1. Introduction
Turbulent flows of dilute polymeric solutions are fundamentally important in many engineering applications such as turbulent drag reduction (DR), fire fighting and agricultural spraying (Toms Reference Toms1949; Lumley Reference Lumley1969). In canonical channel/pipe flows, it is well established that the addition of a small amount of long-chain polymers leads to remarkable DR (Procaccia, L’vov & Benzi Reference Procaccia, L’vov and Benzi2008; White & Mungal Reference White and Mungal2008; Xi Reference Xi2019; Saeed & Elbing Reference Saeed and Elbing2023). This phenomenon arises from the complex interplay between near-wall small-scale turbulent vortices and mesoscale polymer dynamics. Generally, DR occurs as the polymers stretched by the velocity gradient counteract and suppress streamwise vortices (Kim et al. Reference Kim, Li, Sureshkumar, Balachandar and Adrian2007, Reference Kim, Adrian, Balachandar and Sureshkumar2008), and in the dilute solution limit the extent of DR increases with polymer concentration and/or molecular weight and the commensurate elastic forces (Li, Sureshkumar & Khomami Reference Li, Sureshkumar and Khomami2006). A notable feature of this phenomenon is the existence of an upper bound, known as the maximum drag reduction (MDR) (Virk, Mickley & Smith Reference Virk, Mickley and Smith1970), that is, an asymptotic flow state for which a further increase in elastic forces is culminated to obtain a saturated DR at a fixed Reynolds number (
$ \textit{Re} $
). In wall-bounded unidirectional turbulent shear flows, the DR rate of the MDR state can even saturate at
$-80\,\%$
under optimal conditions (Virk et al. Reference Virk, Merrill, Mickley, Smith and Mollo-Christensen1967).
Despite decades of investigation since its discovery, the underlying mechanisms of the MDR asymptote in channel/pipe flows remain an active area of research. Recent advances have established two distinctive viewpoints for elucidating the physical nature of MDR, namely a hibernating/active picture (Li, Sureshkumar & Khomami Reference Li, Sureshkumar and Khomami2015; Xi Reference Xi2019) and elasto-inertial turbulence (EIT) (Li et al. Reference Li, Sureshkumar and Khomami2015; Dubief, Terrapon & Hof Reference Dubief, Terrapon and Hof2023). Both are closely related to the interaction between polymers and the small-scale structures (SSS) that populate the wall region. Specifically, the hibernating/active perspective characterises MDR as a marginal hibernating turbulent state intrinsic to Newtonian turbulence, where the turbulent vortices are greatly suppressed and only a small population of small-scale hairpin vortices persists (Li et al. Reference Li, Sureshkumar and Khomami2006; Xi & Graham Reference Xi and Graham2010, Reference Xi and Graham2012). This leads to reduced Reynolds stress and flow intermittency, ultimately making weak small-scale vortices unable to adequately stretch polymers for further suppression (Zhu & Xi Reference Zhu, Ostilla-Mónico, Verzicco and Lohse2020, Reference Zhu, Song, Lin, Liu, Lu and Khomami2021). Furthermore, the dominant SSS observed in the hibernating state are still classical streamwise vortices, which are commonly found in Newtonian wall-bounded turbulent flows. An alternative viewpoint regards MDR as a distinct EIT state that is fundamentally different from Newtonian turbulence (Samanta et al. Reference Samanta, Dubief, Holzner, Schäfer, Morozov, Wagner and Hof2013; Choueiri, Lopez & Hof Reference Choueiri, Lopez and Hof2018). This state, sustained by inertial and elastic forces, features small-scale spanwise cylindrical vortices generated by polymer forces, which play a key role in EIT self-sustaining dynamics (Terrapon, Dubief & Soria Reference Terrapon, Dubief and Soria2015; Zhang et al. Reference Zhang, Shao, Li, Ma, Zhang and Li2021b
). In particular, the connection between MDR and EIT is substantiated by the fact that EIT exhibits the characteristic drag level of the MDR asymptote (Choueiri et al. Reference Choueiri, Lopez and Hof2018; Lopez, Choueiri & Hof Reference Lopez, Choueiri and Hof2019) and the SSS of EIT are found in a wide parameter regime, particularly in the MDR limit (Samanta et al. Reference Samanta, Dubief, Holzner, Schäfer, Morozov, Wagner and Hof2013; Zhang et al. Reference Zhang, Zhang, Wang, Li, Yu and Li2022). Despite the essential differences between these two viewpoints, one can transition from one state to another by altering certain key parameters, such as the maximum polymer chain extensibility (Wang et al. Reference Wang, Zhang, Wang, Li, Zhang and Li2023) or by varying
$Re$
.
In curvilinear Taylor–Couette flow (TCF), where fluid flows are confined between two concentric cylinders, the existence of novel polymer-induced drag modification (DM) and associated asymptotic drag modification (ADM) states has been demonstrated in recent years (Song et al. Reference Song, Zhu, Lin, Liu and Khomami2023). Here, DM is obtained as both DR and drag enhancement (DE), depending on the distinct interactions between the stretched polymers and the vortical structures. Specifically, in addition to the SSS that populate the wall region, the centrifugal-force-induced Taylor vortices signify the existence of large-scale structures (LSS) that span the entire gap (Grossmann, Lohse & Sun Reference Grossmann, Lohse and Sun2016). It is important to note that in TCF, SSS consist of hairpin vortices and quasi-streamwise vortices energised by mean flow shear instabilities, as well as inertial Görtler vortices triggered by the curvature-induced Görtler instabilities at high
$Re$
(Barcilon & Brindley Reference Barcilon and Brindley1984; Dong Reference Dong2007).
Previous studies have explored the flow dynamics and asymptotic drag-limiting states for cases where polymers interact separately with LSS or SSS in TCF. For low-curvature TCF (quantified by radius ratio
$\eta =R_i/R_o=0.99$
, where
$R_i$
and
$R_o$
represent the inner and outer cylinder radii, respectively) that is devoid of small-scale Görtler vortices, a novel MDR state sustained by LSS dynamics can be observed. As commonly seen in channel/pipe flows, the addition of polymers to low-curvature TCF also results in suppression of SSS and reduction of Reynolds stress, leading to DR (Lin et al. Reference Lin, Song, Liao, Liu, Lu and Khomami2025). However, when the asymptotic MDR state is realised by gradually enhancing the elastic forces, the SSS can be almost completely eliminated while the LSS persists in the flow field. This is strikingly different from the classical MDR of channel/pipe flows, which are characterised by the sole presence of shear-energised small-scale vortices that include hairpin vortices, quasi-streamwise vortices and spanwise vortices. In turn, the interaction between polymer chains and persistent LSS is found to give rise to significant polymer stress development that partially offsets the magnitude of DR, leading to MDR asymptotes with lower levels of DR (approximately
$\sim -60\,\%$
). Similar findings are experimentally obtained in a TCF with
$\eta =0.714$
, for which the effects of polymers on the LSS are only marginal (Zhang et al. Reference Zhang, Fan, Su, Xi and Sun2025). In particular, the MDR rate at
$\eta =0.714$
is only
$\sim -20\,\%$
, significantly lower than that for
$\eta =0.99$
, indicating that the curvature effect plays a significant role in the determination of polymer-induced DM in TCF. Although we observe these MDR states at relatively high
$Re\gt 1000$
, the spatio-temporal dynamics of the LSS observed are reminiscent of those for a low-
$Re$
elasto-inertial TCF (Boulafentis et al. Reference Boulafentis, Lacassagne, Cagney and Balabani2023; Bai et al. Reference Bai, Latrache, Kelai, Crumeyrolle and Mutabazi2023). In particular, Boulafentis et al. (Reference Boulafentis, Lacassagne, Cagney and Balabani2024) showed that solitary pairs of large-scale vortices form the fundamental structural elements of a variety of intriguing flow patterns: they are stable in diwhirls (Groisman & Steinberg Reference Groisman and Steinberg1997; Lopez Reference Lopez2022), oscillatory in flame patterns (Latrache & Mutabazi Reference Latrache and Mutabazi2021; Latrache et al. Reference Latrache, Kelai, Bai, Crumeyrolle and Mutabazi2025) and chaotic in EIT (Dutcher & Muller Reference Dutcher and Muller2013; Lacassagne et al. Reference Lacassagne, Cagney, Gillissen and Balabani2020). The LSS in MDR of TCF likewise exhibit chaotic dynamics, especially oscillating and meandering in the axial direction (Lin et al. Reference Lin, Song, Liao, Liu, Lu and Khomami2025). Hence, one can speculate that the MDR state is also closely related to the EIT regime in viscoelastic TCF.
In stark contrast, the strong coupling between polymer dynamics and SSS in a high-curvature TCF with
$\eta =0.5$
can lead to dramatically different asymptotic drag-limiting states (Zhu et al. Reference Zhu, Wan, Lin, Liu, Lu and Khomami2023; Lin et al. Reference Lin, Song, Liu, Wan, Lu and Khomami2024b
). Specifically, strong curvature has been shown to intensify the elastic instability driven by the hoop stress that squeezes fluid packages radially inward (Larson, Shaqfeh & Muller Reference Larson, Shaqfeh and Muller1990; Larson Reference Larson1992; Al-Mubaiyedh, Sureshkumar & Khomami Reference Al-Mubaiyedh, Sureshkumar and Khomami2000; Thomas, Sureshkumar & Khomami Reference Thomas, Sureshkumar and Khomami2006; Schäfer et al. Reference Schäfer, Morozov and Wagner2018; Shaqfeh & Khomami Reference Shaqfeh and Khomami2021). This polymer-induced elastic force competes with the outward-pointing centrifugal force, resulting in the breakdown and complete elimination of LSS, as well as the creation of distinctive small-scale elastic Görtler vortices that are triggered by elastic (hoop-stress-induced) Görtler-like instabilities (Liu & Khomami Reference Liu and Khomami2013; Song et al. Reference Song, Lin, Liu, Lu and Khomami2021). Consequently, an SSS-dominated flow state is achieved. In this scenario, a significant reduction in Reynolds stress is also observed as the velocity fluctuations are suppressed by polymer additives. However, a notable DE is achieved due to the efficient incoherent transport of polymer stresses induced by SSS (Song et al. Reference Song, Teng, Liu, Ding, Lu and Khomami2019; Zhu et al. Reference Zhu, Song, Lin, Liu, Lu and Khomami2022). This implies that the DR effect resulting from Reynolds stress reduction is completely counteracted by the development of polymer stress. The degree of DE increases with the enhancement of the elastic forces and, eventually, the turbulent flow drag saturates, demonstrating the existence of a novel asymptotic flow state called maximum drag enhancement (MDE) (Zhu et al. Reference Zhu, Wan, Lin, Liu, Lu and Khomami2023; Lin et al. Reference Lin, Song, Liu, Wan, Lu and Khomami2024b
). The similarities between MDR and MDE have been substantiated in both the TCF and the spanwise rotating plane Couette flow. These include a significant reduction in Reynolds stress, the saturation of flow structures quantified by vorticity fluctuation and a similar interaction between polymers and turbulence in the near-wall region (Li et al. Reference Li, Sureshkumar and Khomami2006; Dubief, Terrapon & Soria Reference Dubief, Terrapon and Soria2013; Li et al. Reference Li, Sureshkumar and Khomami2015). While most previous studies have reported polymer-induced DE based on numerical simulations, experiments in a high-
$Re$
viscoelastic TCF with both cylinders rotating also show significant DE. In particular, Horimoto & Okuyama (Reference Horimoto and Okuyama2025) demonstrated for the first time that the transition from DR to DE occurs when the outer cylinder switches from counter- to co-rotation, which they attributed to the emergence of a solid-body rotational flow structure.
Although the aforementioned studies have demonstrated the existence of distinct MDR and MDE states in TCF, the underlying mechanism connecting them remains unclear. Resolving this issue is crucial for understanding the universality of elastically induced DM asymptotes, namely, whether the asymptotic flow states are an inherent property of viscoelastic wall-bounded turbulent flows. In the end, several fundamental questions need to be addressed: (i) the dynamical connections between MDR and MDE in TCF, that is, whether these states are connected along a continuous transition pathway or are disconnected by barrier flow regimes (Choueiri et al. Reference Choueiri, Lopez and Hof2018; Zhu & Xi Reference Zhu and Xi2021); (ii) the underlying mechanisms responsible for the occurrence of different drag-limiting states and their quantitative dependence on key parameters; (iii) the scale interaction between LSS and SSS in the presence of polymer dynamics, given that previous work has highlighted intriguing connections between LSS and MDR, and between SSS and MDE. The answer to the second question also guides future work that aims to achieve ADM states with different DM rates. In fact, previous studies have documented MDR at
$\eta =0.714$
(Zhang et al. Reference Zhang, Fan, Su, Xi and Sun2025) and MDE at
$0.5$
(Lin et al. Reference Lin, Song, Liu, Wan, Lu and Khomami2024b
), suggesting the potential to realise various DMs at intermediate
$\eta$
values.
In this paper we performed extensive high-fidelity direct numerical simulations (DNS) of TCF in a viscoelastic fluid described by the FENE-P model to explore the polymer-induced ADM states. At fixed
$\eta =0.6$
and
$Re=6000$
, a state transition from MDR to MDE is observed by decreasing the solvent-to-total viscosity ratio
$\beta$
from
$0.99$
to
$0.90$
. To obtain a mechanistic understanding of this ADM state transition, we leverage the capability of DNS to directly resolve polymer stress fields. This allows us to examine the DM characteristics, turbulence dynamics and polymer dynamics for different ADM states in a way that is not feasible experimentally. To this end, the relationship underlying the ADM state transition, structural change and elastic instability is established, which also provides a unified view to elucidate the different DM extents observed in previous studies. That is, varying the control parameter, in fact, changes the strength of the elastic instability, which in turn modulates the flow structures and associated turbulent transport. Furthermore, we underscore an inverse energy cascade in viscoelastic turbulence by examining the scale-decomposed transport equation of turbulent kinetic energy (TKE).
2. Problem formulation and numerical method
2.1. Governing equations
We conducted three-dimensional DNS to investigate the flow dynamics of a turbulent viscoelastic TCF. In our set-up, the inner cylinder rotates at a constant angular velocity
$\omega _i$
, while the outer cylinder remains stationary. To capture the essential rheological response of viscoelastic fluids, the commonly used constitutive equation FENE-P (finitely extensible nonlinear elastic-Peterlin) is chosen to model the polymeric contribution to total stress (Alves, Oliveira & Pinho Reference Alves, Oliveira and Pinho2021; Dubief et al. Reference Dubief, Terrapon and Hof2023; Song et al. Reference Song, Zhu, Lin, Liu and Khomami2023). For dimensionless formulation, we selected the following reference scales: the width of the gap
$d=R_o-R_i$
, the velocity of the inner cylinder
$R_i\omega _i$
, the characteristic pressure
$\rho (R_i\omega _i)^2$
and the stress
$\eta _p R_i\omega _i/d$
. Here,
$\rho$
is the density of the fluid and
$\eta _p$
represents the viscosity of the polymers. Using these scales, we obtained non-dimensional velocity
$\boldsymbol{u}$
, time
$t$
, pressure
$P$
and polymer stress
$\boldsymbol{\tau }$
. The governing equations that describe the turbulent TCF of dilute polymeric solutions are formulated in the following dimensionless form:
and
Here
$\unicode{x1D63E}$
is the positive definite symmetric conformation tensor, which quantifies the local phase average of the product of the end-to-end vector of each polymer molecule. The Reynolds number is defined on the basis of the inner cylinder velocity, i.e.
$Re=\rho R_i\omega _i d/\eta _t$
, where
$\eta _t=\eta _p+\eta _s$
is the total zero-shear solution viscosity with
$\eta _s$
being the solvent viscosity. Hence, the parameter
$\beta =\eta _s/\eta _t$
is the solvent-to-total viscosity ratio (for a Newtonian fluid,
$\beta =1$
). In cylindrical coordinates, the velocity vector
$\boldsymbol{u}$
comprises
$(u_r,u_\theta ,u_z)$
, representing the radial (wall normal), azimuthal (stream) and axial (span) velocities, respectively. For the chosen FENE-P model, the polymer stress tensor
$\boldsymbol{\tau }$
is obtained from the conformation tensor using the following relation:
Here the function
$f(\unicode{x1D63E}\,)=(L^2-3)/[L^2-tr(\unicode{x1D63E}\,)]$
, known as the Peterlin function, limits the maximum extension that a polymer molecule can experience, with
$L$
defining the maximum extensibility of the polymers. Moreover,
$tr(\unicode{x1D63E}\,)=C_{\textit{rr}}+C_{\theta \theta }+C_{\textit{zz}}$
represents the trace of the conformation tensor, and the Weissenberg number is defined as
$Wi=\lambda R_i \omega _i/d$
with
$\lambda$
being the polymer relaxation time.
2.2. Numerical methods and computational settings
The governing equations are solved using an efficient and robust DNS code developed in our previous work, based on the finite difference method. This code has been thoroughly validated in Lin et al. (Reference Lin, Wan, Zhu, Liu, Lu and Khomami2022) and previously used to investigate polymer-induced drag-limiting behaviours in turbulent TCFs (Lin et al. Reference Lin, Song, Liu, Wan, Lu and Khomami2024b , Reference Lin, Song, Liao, Liu, Lu and Khomami2025). Specifically, temporal advancement is computed with a low-storage Runge–Kutta third-order time-stepping scheme (Rai & Moin Reference Rai and Moin1991), in combination with a Crank–Nicolson scheme for the viscous term in (2.2) and the stress relaxation term in the constitutive equation (2.3). This approach allows for the enforcement of the boundedness of the polymer conformation tensor during time integration (Dubief et al. Reference Dubief, Terrapon, White, Shaqfeh, Moin and Lele2005). Furthermore, pressure–velocity coupling is ensured by a fractional step method (Kim & Moin Reference Kim and Moin1985). No-slip boundary conditions are applied to the inner and outer walls of the cylinder, and periodic boundary conditions are applied in the azimuthal and axial directions.
We employ a staggered grid arrangement with uniform grid spacing in the azimuthal and axial directions and non-uniform grid spacing in the radial direction, refining wall grids via a clipped Chebyshev-type clustering method. For spatial discretisation, a well-established second-order energy-conserving central scheme (Verzicco & Orlandi Reference Verzicco and Orlandi1996; van der Poel et al. Reference van der Poel, Ostilla-Mónico, Donners and Verzicco2015) is employed. Special consideration is given to the convection term in the constitutive equation (2.3) due to its hyperbolic nature at high
$Wi$
(Talwar, Ganpule & Khomami Reference Talwar, Ganpule and Khomami1994; Somasi & Khomami Reference Somasi and Khomami2000; Alves et al. Reference Alves, Oliveira and Pinho2021). This term is solved using the method proposed by Vaithianathan et al. (Reference Vaithianathan, Robert, Brasseur and Collins2006), which is based on the shock capture scheme of Kurganov & Tadmor (Reference Kurganov and Tadmor2000) and avoids the introduction of any artificial diffusion. Specifically, this scheme guarantees the symmetric positive definite property of
$\unicode{x1D63E}$
during time integration with an appropriately small time step by monitoring the eigenvalues of the conformation tensor for all points on the grid. In our present simulations, this method was found to provide second-order accuracy at more than 95 % of all grid points.
A series of simulations are conducted for a three-dimensional TCF of moderate curvature, i.e. a radius ratio
$\eta =0.6$
, where large-scale Taylor vortices coexist with small-scale vortices (Bilson & Bremhorst Reference Bilson and Bremhorst2007). The axial length of the computational domain is set as
$L_z/d=2\pi$
. As shown in § 3, this choice of
$L_z/d$
allows for at least two pairs of large-scale Taylor vortices, demonstrating that the flow structures exhibit reasonable axial wavelengths and ensuring the reliability of the turbulence statistics (Martínez-Arias et al. Reference Martínez-Arias, Peixinho, Crumeyrolle and Mutabazi2014; Ostilla-Mónico et al. Reference Ostilla-Mónico, Verzicco and Lohse2015, Reference Ostilla-Mónico, Lohse and Verzicco2016). To maintain a fixed inertial effect, a typical
$Re=6000$
is chosen that is commonly used in the existing literature (Dubief et al. Reference Dubief, Terrapon and Soria2013; Song et al. Reference Song, Teng, Liu, Ding, Lu and Khomami2019; Wang et al. Reference Wang, Zhang, Wang, Li, Zhang and Li2023). For the current TCF set-up, this
$Re$
corresponds to a turbulent Taylor vortices state for the Newtonian base flow (Andereck, Liu & Swinney Reference Andereck, Liu and Swinney1986), with a frictional Reynolds number of
$Re_\tau = \rho u_\tau d/\eta _t = 325.2$
on the inner cylinder wall. Here,
$u_\tau =\sqrt {\tau _w/\rho }$
is the friction velocity with
$\tau _w$
being the total wall stress, i.e. the sum of viscous and polymer stresses.
The viscosity ratio
$\beta$
, known as a measure of polymer concentration in the experimental study (Lopez et al. Reference Lopez, Choueiri and Hof2019), has been shown to play a critical role in flow dynamics. For example, a change in
$\beta$
can significantly alter the viscoelastic instability (Khalid, Shankar & Subramanian Reference Khalid, Shankar and Subramanian2021) and the transition pathway to turbulence (Ibarra & Park Reference Ibarra and Park2023). To this end, this work focuses on the asymptotic flow states realised in a range of
$0.90\leqslant \beta \leqslant 0.99$
, corresponding to polymer solutions that fall into the dilute regimes. We use a large value of
$L=100$
to ensure the dilute polymeric solution shear viscosity is nearly shear rate independent and a significant elongational viscosity that scales with
$L^2$
. This value of
$L$
is frequently adopted in previous studies on ADM states (Wang et al. Reference Wang, Zhang, Wang, Li, Zhang and Li2023; Lin et al. Reference Lin, Song, Liu, Wan, Lu and Khomami2024b
, Reference Lin, Song, Liao, Liu, Lu and Khomami2025), enabling a reasonable comparative study. For each given value
$\beta$
, we vary
$Wi$
from
$10$
to
$150$
to systematically examine polymer-induced drag-limiting behaviours. This simulation protocol for attaining asymptotic flow states is widely adopted in previous numerical studies (Xi Reference Xi2019), contrasting with conventional experimental approaches where MDR is typically achieved by increasing the polymer concentration at a fixed
$Re$
(Procaccia et al. Reference Procaccia, L’vov and Benzi2008; Zhang et al. Reference Zhang, Fan, Su, Xi and Sun2025). The latter simultaneously decreases
$\beta$
and increases
$Wi$
in experiments, leading to a strong coupling between these two parameters that complicates the interpretation of MDR observations. To experimentally replicate the simulation protocol, temperature-mediated modulation of polymer relaxation time, along with adjustments to the inner cylinder’s rotational speed to counteract the viscosity changes induced by temperature and maintain a constant
$Re$
, offers a viable pathway (Groisman & Steinberg Reference Groisman and Steinberg1996). All simulations are conducted using a structured cylindrical grid system consisting of
$N_r\times N_\theta \times N_z = 256\times 256\times 448$
grid points in the radial, azimuthal and axial directions, respectively. Evidently, the results reported based on the implemented grid sizes are accurate, as demonstrated by the extensive grid convergence studies reported in Appendix A. The time step was set as sufficiently small
$\Delta t=0.002$
to resolve turbulent time scales and polymer relaxation dynamics. For each setting of
$(\beta , Wi)$
, long-time simulation is performed on
$500T$
, where
$T=d/R_i\omega _i$
is the convective time unit, to ensure statistical convergence. Ensemble averaging is performed for time periods of
$400T$
to reliably evaluate the turbulence statistics.
3. Results and discussions
3.1. Drag modification characteristics and mechanisms
Polymer additives significantly modify turbulent drag in TCF (Song et al. Reference Song, Zhu, Lin, Liu and Khomami2023). This modification is quantified by variations in the global response of the flow system, i.e. the pseudo-Nusselt number
$Nu_\omega$
, which quantifies the overall transport of angular momentum and has been used in experiments to examine the torque scaling of viscoelastic TCF (Moazzen et al. Reference Moazzen, Lacassagne, Thomy and Bahrani2023). Specifically, we define
$Nu_\omega$
as
$J^\omega /J^{\omega }_{lam}$
(Lathrop et al. Reference Lathrop, Fineberg and Swinney1992a
,
Reference Lathrop, Fineberg and Swinneyb
; Lewis & Swinney Reference Lewis and Swinney1999). Here,
$J^\omega$
is the conserved angular momentum flux, analogous to the heat flux in Rayleigh–Bénard convection, with its definition given by
where
$\omega =u_\theta /r$
and
$\langle \boldsymbol{\cdot }\rangle =\langle \langle \langle \boldsymbol{\cdot }\rangle _{\theta }\rangle _z\rangle _t$
denotes the averaging in the
$\theta$
and
$z$
directions and in time. In addition, the laminar value of
$J^{\omega }$
is calculated as
$J^{\omega }_{lam}=2\omega _i R_i^2 R_o^2/Re(R_o^2 -R_i^2)$
. We define the extent of DM as
$DM=(Nu_{\omega } - Nu_{\omega }^{N})/Nu_{\omega }^{N}$
, where
$Nu_{\omega }^{N}$
is the Newtonian value at
$Re=6000$
. Figure 1(a) shows a complete diagram of the ADM states, where an intriguing DM phenomenon is observed as
$\beta$
and
$Wi$
vary, that is, asymptotic flow states of MDR and MDE are realised. Specifically, continuously increasing
$Wi$
at higher
$\beta \geqslant 0.98$
leads to MDR, while MDE is achieved at lower
$\beta \leqslant 0.97$
. For a given
$\beta$
,
$DM$
monotonically changes with increasing
$Wi$
, except for lower
$Wi=10$
at
$\beta =0.98$
and
$0.97$
. Note that
$DM$
becomes almost saturated at sufficiently high
$Wi\geqslant 100$
, indicating the realisation of asymptotic flow states. It should be noted that different
$\beta$
leads to asymptotic flow states to varying degrees of
$DM$
. For example, an MDR state with
$DM=-11.7\,\%$
is observed at
$\beta =0.99$
, which is comparable to recent experimental findings in viscoelastic TCF with
$\eta =0.714$
and
$Re=1.3\times 10^4$
(Zhang et al. Reference Zhang, Fan, Su, Xi and Sun2025). This observed MDR value is considerably lower than that typically found in the channel/pipe flow (which is typically around
$DM\sim -70\,\%$
) (Procaccia et al. Reference Procaccia, L’vov and Benzi2008; White & Mungal Reference White and Mungal2008). In contrast, at the smallest
$\beta =0.90$
considered, an MDE state with
$DM=34.6\,\%$
is realised. This clearly highlights a continuous state transition pathway from MDR to MDE as
$\beta$
decreases. In particular, the transition threshold is approximately
$\beta =0.98$
, for which a nearly zero
$DM$
(
$-2.4\,\%$
) is observed. This suggests that in TCF, the appropriate selection of
$\beta$
(corresponding to the polymer concentration in experiments) can lead to ineffective drag modulation by polymer addition.
(
$a$
) Global response
$Nu_{\omega }$
versus
$Wi$
at various
$\beta$
. The extent of DM for the highest
$Wi=150$
realised in our simulations is reported. To distinguish MDR and MDE states, a horizontal reference line corresponding to
$Nu_{\omega }$
of the Newtonian flow is depicted. (
$b$
) Dynamical evolution cycles of a rescaled system response
$4Nu_{\omega }/(1+\eta )^2$
versus total dissipation
$\varepsilon _v + \varepsilon _p$
for different ADM states (
$Wi=150$
) at various
$\beta$
. Here,
$\varepsilon _v = \langle (\partial _i u_j + \partial _j u_i)^2 \rangle _V /2$
and
$\varepsilon _p = \langle \tau _{\textit{ij}} \partial _j u_i \rangle _V$
are the viscous and elastic dissipation rates, respectively, with
$\langle \boldsymbol{\cdot } \rangle _V$
denoting the volume average. The result of Newtonian flow is plotted for comparison. The dashed line in panel (
$b$
) corresponds to the exact relation
$\varepsilon _v+\varepsilon _p=4Nu_\omega /(1+\eta )^2$
.

We further illustrate this
$\beta$
-dependent state transition pathway in figure 1(
$b$
) by plotting the dynamical evolution cycles for different ADM states with
$Wi=150$
. Specifically, we examine the exact relation
$\varepsilon _v+\varepsilon _p=4Nu_\omega /(1+\eta )^2$
(Lin et al. Reference Lin, Song, Liu, Liu, Lu and Khomami2024a
), using both sides as axes to explore the property of dynamical evolution. This choice is based on the fact that the left-hand side characterises energy dissipation, while the right-hand side represents angular momentum transport. In fact, the latter corresponds directly to the rate of energy input through the rotating cylinder wall (Eckhardt, Grossmann & Lohse Reference Eckhardt, Grossmann and Lohse2007). As shown in figure 1(
$b$
), the dynamical evolution of ADM states traces elliptical-like envelopes whose principal axes align with the exact relation. This alignment confirms that statistically converged states are achieved, signifying a balance between energy input and dissipation. The continuous state transition is evident as the evolution cycle of the ADM states gradually shifts to encompass that of the Newtonian flow as
$\beta$
decreases. Intriguingly, while the evolution cycle at
$\beta =0.98$
overlaps greatly with that of the Newtonian fluid (consistent with their comparable
$Nu_\omega$
values), the shapes of their elliptical-like envelopes exhibit distinct topological characteristics. Specifically, the evolution cycle at
$\beta =0.98$
occupies a smaller area, which can be attributed to the polymer-induced suppression of turbulent motions, i.e. weakened fluctuations in energy dissipation and angular momentum transport (Dallas, Vassilicos & Hewitt Reference Dallas, Vassilicos and Hewitt2010; Zhang et al. Reference Zhang, Fan, Su, Xi and Sun2025).
It is important to note that, although various DM phenomena have been observed, the transition path from MDR to MDE has been reported for the first time. Figure 2 summarises the DM studied to date in high-
$Re$
(
${\gt } 1000$
) viscoelastic TCFs, highlighting the significance and novelty of our present findings. As illustrated, the wide parameter space, encompassing variations in
$Re$
,
$\eta$
,
$Wi$
,
$\beta$
, and the presence of rotation of the outer cylinder, captures the intriguing phenomena of DM, covering a wide range of DR and DE. At comparable
$Re$
and
$\eta$
values, we find good agreement between numerical data (Lin et al. Reference Lin, Wan, Zhu, Liu, Lu and Khomami2022) and experimental data (Zhang et al. Reference Zhang, Fan, Su, Xi and Sun2025), which demonstrates the effectiveness of the FENE-P model and our numerical method in faithfully predicting polymer-induced DM in viscoelastic TCF. Although asymptotic flow states have also been identified numerically in Lin et al. (Reference Lin, Song, Liu, Wan, Lu and Khomami2024b
, Reference Lin, Song, Liao, Liu, Lu and Khomami2025) and experimentally in Zhang et al. (Reference Zhang, Fan, Su, Xi and Sun2025), these previous studies observed MDR or MDE separately. As figure 2 shows, two critical considerations contribute to the transition of the ADM state observed in our study: (i) we chose a moderate curvature with
$\eta =0.6$
, which is weaker than that leading to the MDE state (at
$\eta =0.5$
) but stronger than the value leading to the MDR state (at
$\eta =0.99,0.714$
); (ii) we consider a wide range of values of
$\beta$
, allowing an extensive examination of elastic effects. We will discuss later how these considerations lead to a subtle competition between elastic and inertial forces, which, in turn, modifies angular momentum transport and flow structures. A recent experiment on TCF of a dilute surfactant solution observed a transition from DE to DR by increasing
$Re$
or switching the outer cylinder rotation from co-rotating to counter-rotating (Horimoto & Okuyama Reference Horimoto and Okuyama2025). However, they did not achieve an asymptotic flow state, and the physical mechanisms for the DM transition in their experiments remain unclear, as the direct measurement of polymer stress is experimentally intractable. Our numerical approach overcomes this limitation by directly resolving the stress fields to uncover the underlying physics.
A summary of the DM induced by the elastic effect in high-
$Re$
viscoelastic TCF. For consistency, here the definition of DM is based on the friction factor
$C_f$
, namely,
$DM^*=C_f/C_f^N-1$
, with
$C_f^N$
being the value for the corresponding Newtonian flow. For TCF,
$C_f$
is calculated as
$[(1-\eta )^2/\pi ]G/Re^2$
, with
$G$
being the dimensionless torque (Lathrop et al. Reference Lathrop, Fineberg and Swinney1992a
,
Reference Lathrop, Fineberg and Swinneyb
; Grossmann et al. Reference Grossmann, Lohse and Sun2016). Both experimental data (Exp.) and numerical data (Num.) are shown. In addition to
$Re$
, another remarkable difference between these studies is the curvature effect:
$\eta =0.5$
for Rajappan & McKinley (Reference Rajappan and McKinley2020) and Lin et al. (Reference Lin, Wan, Zhu, Liu, Lu and Khomami2022, Reference Lin, Song, Liu, Wan, Lu and Khomami2024b
);
$\eta =0.6$
for the present study;
$\eta =0.714$
for Zhang et al. (Reference Zhang, Fan, Su, Xi and Sun2025);
$\eta =0.731$
for Horimoto & Okuyama (Reference Horimoto and Okuyama2025);
$\eta =0.95$
for Barbosa et al. (Reference Barbosa, Cussuol, Soares, Andrade and Khalil2022);
$\eta =0.99$
for Lin et al. (Reference Lin, Song, Liao, Liu, Lu and Khomami2025). For Barbosa et al. (Reference Barbosa, Cussuol, Soares, Andrade and Khalil2022), only data obtained with polyacrylamide polymers are shown here, as they exhibit the most pronounced DR. Data obtained from Zhang et al. (Reference Zhang, Fan, Su, Xi and Sun2025) correspond to polyacrylamide polymers with two different molecular weights. Moreover, only Horimoto & Okuyama (Reference Horimoto and Okuyama2025) have considered the outer cylinder rotation, and all the other studies are focused on TCF of a purely inner cylinder rotation.

Figure 3 illustrates how the mean velocity profile
$u_\theta ^+$
responds to increments in
$Wi$
. We present results of two representative values of
$\beta$
:
$\beta =0.99$
for MDR states and
$\beta =0.90$
for MDE states. For higher
$\beta =0.99$
, the
$u_\theta ^+$
profiles immediately collapse onto a single curve at low
$Wi=10$
. The introduction of polymers leads to a boost of
$u_\theta ^+$
in the core region, a common observation in polymer drag-reducing flows (Li et al. Reference Li, Sureshkumar and Khomami2006; White & Mungal Reference White and Mungal2008). Interestingly, the
$u_\theta ^+$
profile for the MDR state exhibits a von Kármán-like logarithmic law for
$r^+\gt 30$
, closely following
$u_\theta ^+=(1/\kappa ) \text{ln} r^+ + C$
with
$\kappa = 1.06, C=7.6$
(see figure 3
$a$
). Similarly to the observations in Zhang et al. (Reference Zhang, Fan, Su, Xi and Sun2025),
$\kappa$
is not significantly modified compared with its Newtonian counterpart (
$\kappa =0.94$
). In contrast, the
$u_\theta ^+$
profile in
$\beta =0.90$
demonstrates a more pronounced variation due to the stronger elastic effect. Specifically, an increase in
$Wi$
within the range of
$10{\sim}80$
leads to a gradual decrease in
$u_\theta ^+$
in the core region, consistent with the increase in DE reported in figure 1. As the MDE state is realised for
$Wi\geqslant 100$
, the
$u_\theta ^+$
profile shows a very weak dependence on further increases in
$Wi$
. For the MDE state at
$\beta =0.90$
, we obtain
$\kappa =1.85$
, which clearly deviates from its Newtonian counterpart.
The log plots of mean velocity profile
$u_\theta ^+$
in the inner half of the gap versus wall-normal distance
$r^+$
for (
$a$
)
$\beta =0.99$
and (
$b$
)
$\beta =0.90$
. Here,
$u_\theta ^+$
and
$r^+$
are calculated as
$(1-\langle u_\theta \rangle )/u_\tau$
and
$(r-R_i)/(u_{\tau }\eta _t/\rho )$
, respectively. The log law plot of
$u_\theta ^+=(1/\kappa ) \text{ln} r^+ + C$
is obtained by fitting the mean velocity profile at
$Wi=150$
in the region
$r^+ \geqslant 30$
. Here
$\kappa =1.06, C=7.6$
for the MDR state at
$\beta =0.99$
, and
$\kappa =1.85, C=8.1$
for the MDE state at
$\beta =0.90$
.

(
$a$
) Comparison of the mean velocity profile
$u_\theta ^+$
for different ADM states in viscoelastic TCF. The present data show
$u_\theta ^+$
of drag-limiting states at
$Wi=150$
with various
$\beta$
. Available numerical and experimental data are plotted for comparison:
$\eta =0.5,Re=5000$
, Lin et al. (Reference Lin, Song, Liu, Wan, Lu and Khomami2024b
);
$\eta =0.714,Re=1.3\times 10^4$
, Zhang et al. (Reference Zhang, Fan, Su, Xi and Sun2025);
$\eta =0.99,Re=5000$
, Lin et al. (Reference Lin, Song, Liao, Liu, Lu and Khomami2025). The grey dashed line corresponds to the Virk law in the MDR state of parallel shear turbulent flows, namely,
$u_\theta ^+=(1/\kappa ) \text{ln} r^+ + C$
with
$\kappa =1/11.7, C=-17$
(Virk et al. Reference Virk, Mickley and Smith1970). (
$b$
) The diagnostic function
$r^+ \text{d}u_\theta ^+/\text{d}r^+$
for the ADM states achieved in this study. The inset shows the change of
$\kappa$
in ADM states with increasing
$1-\beta$
.

To further highlight the properties of the mean velocity profile, figure 4(
$a$
) shows
$u_\theta ^+$
as a function of
$r^+$
for various ADM states realised in this study. Data available from previous studies are also added for comparison (Virk et al. Reference Virk, Mickley and Smith1970; Lin et al. Reference Lin, Song, Liu, Wan, Lu and Khomami2024b
, Reference Lin, Song, Liao, Liu, Lu and Khomami2025; Zhang et al. Reference Zhang, Fan, Su, Xi and Sun2025). Evidently, the transition to the ADM state is accompanied by a corresponding transition in the
$u_\theta ^+$
profile. Specifically, as
$\beta$
decreases, the asymptotic flow state transitions from MDR to MDE, and the corresponding profile
$u_\theta ^+$
decreases in the core region. It is also found that, although the ADM state at
$\beta =0.98$
exhibits a turbulent flow drag similar to its Newtonian counterpart (see figure 1
$a$
), their
$u_\theta ^+$
profiles are not identical, indicating significant modifications introduced by polymers. Interestingly, comparing the present results with previous data also reveals an ADM state transition driven by decreasing
$\eta$
. To highlight this, table 1 summarises the corresponding degree of DM for the
$u_\theta ^+$
profile depicted in figure 4 (
$a$
). Specifically, a gradual increase in the curvature effect (corresponding to a decrease in
$\eta$
) leads to a sequence of transitions in the ADM state: from the classical MDR state (
$\eta \to \infty$
) to MDR states with significantly lower DR rates (
$\eta =0.99, 0.95, 0.714$
), followed by the MDR/MDE states with low/moderate DR/DE observed in this study (
$\eta =0.6$
), and eventually to the MDE state with significantly enhanced DE (
$\eta =0.5$
). This confirms our earlier argument that the observed state transition is a result of the appropriate choice of
$\eta$
and
$\beta$
in this study. In fact, the curvature effect is closely related to elastic forces and instabilities (Larson et al. Reference Larson, Shaqfeh and Muller1990; Shaqfeh & Khomami Reference Shaqfeh and Khomami2021; Datta et al. Reference Datta2022), which, as we show later, are critical in determining the flow dynamics of the ADM states.
The extent of DM corresponding to the
$u_\theta ^+$
profile shown in figure 4(
$a$
). Here, the parallel shear (channel/pipe) flow is presented as a curvature-free case, in which exceedingly high DR can be achieved (Procaccia et al. Reference Procaccia, L’vov and Benzi2008; White & Mungal Reference White and Mungal2008; Xi Reference Xi2019). The MDR rate for Zhang et al. (Reference Zhang, Fan, Su, Xi and Sun2025) is experimentally obtained by increasing the polymer concentration at
$Re=1.3\times 10^4$
using polyacrylamide solutions. Moreover, the MDR state at comparable
$Re=6200$
, realised in Barbosa et al. (Reference Barbosa, Cussuol, Soares, Andrade and Khalil2022) using 500 ppm polyacrylamide solutions, is also included for comparison. The geometric curvature
$\epsilon =d/R_i$
is provided to clearly illustrate the variations in curvature effects.

We have also examined the logarithmic dependence of the
$u_\theta ^+$
profiles for the ADM states achieved in this study. As shown in figure 4(
$b$
), the diagnostic function indicates a clear logarithmic behaviour, especially for the MDR state realised at higher
$\beta$
. This observation aligns with the clear logarithmic law reported for the MDR state in Zhang et al. (Reference Zhang, Fan, Su, Xi and Sun2025). The transition of the ADM state is accompanied by a change in
$\kappa$
. Specifically,
$\kappa =0.94$
is obtained for the Newtonian flow, which is significantly larger than
$\kappa =0.4$
obtained for canonical pipe and channel flows (Marusic et al. Reference Marusic, Monty, Hultmark and Smits2013). This discrepancy is attributed to the boundary layer of the non-zero pressure gradient in the TCF (Ostilla-Mónico et al. Reference Ostilla-Mónico, Van Der Poel, Verzicco, Grossmann and Lohse2014b
). Decreasing
$\beta$
results in a gradual increase in
$\kappa$
, as shown by the inset in figure 4(
$b$
). For
$\beta \geqslant 0.95$
, a plateau is found in
$\kappa$
, for which the underlying mechanisms are unclear. Further exploration of the
$\kappa$
dependence on the ADM states would be an interesting question for future study.
As mentioned previously, the ADM state transition stems from a subtle competition between the inertial and elastic forces, which can be closely examined by the Reynolds and polymer stresses. As illustrated in figure 5(
$a$
), the ADM states always have a reduced Reynolds stress compared with their Newtonian counterpart, regardless of the extent of DM. This observation suggests a universal nature of polymer-induced suppression of velocity fluctuations in wall-bounded turbulent flows. Furthermore, Reynolds stress monotonically decreases with decreasing
$\beta$
, due to the enhanced elastic effect. For a detailed examination of the Reynolds stress in ADM states for TCF, we compared our current data with the previously available results. For
$\eta =0.5$
and
$0.6$
, the maximum value of
$\langle u'_r u'_\theta \rangle$
occurs in the inner wall region. This has been attributed to the ‘elastic Görtler vortices’ that induce intense azimuthal velocity fluctuations (Bilson & Bremhorst Reference Bilson and Bremhorst2007; Lin et al. Reference Lin, Song, Liu, Wan, Lu and Khomami2024b
). In contrast, the radial distributions of
$\langle u^{\prime}_r u^{\prime}_\theta \rangle$
depict a qualitative difference for the MDR states realised at
$\eta =0.99,0.714$
, where the peak value occurs in the core region. This, in contrast, is attributed to the large-scale Taylor vortices that persist in asymptotic flow states, inducing intense radial velocity in the bulk region (Lin et al. Reference Lin, Song, Liao, Liu, Lu and Khomami2025; Zhang et al. Reference Zhang, Fan, Su, Xi and Sun2025). These intriguing structural changes and their correspondence to the ADM state transition will be detailed in § 3.2. To accurately evaluate the influence of polymer stress on flow dynamics, we calculated the rescaled polymer stress
$-(1-\beta )\langle \tau _{r\theta }\rangle /Re$
, allowing for a direct comparison with Reynolds stress. Figure 5(
$b$
) delineates a monotonic increase in the magnitude of rescaled polymer stress as the MDR state gradually transitions to the MDE state. In a commensurate manner, the contribution of polymer stress to angular momentum transport (turbulent flow drag) becomes more significant. This argument is further confirmed by the large polymer stress obtained at
$\eta =0.5$
(Lin et al. Reference Lin, Song, Liu, Wan, Lu and Khomami2024b
), which facilitates an MDE state with a dramatic DE of
${\sim}73.8\,\%$
(see table 1).
Radial distribution of (
$a$
) Reynolds stress and (
$b$
) rescaled polymer stress for different ADM states in viscoelastic TCF. The present data correspond to the drag-limiting states at
$Wi=150$
with various
$\beta$
. Previous numerical data (Lin et al. Reference Lin, Song, Liu, Wan, Lu and Khomami2024b
, Reference Lin, Song, Liao, Liu, Lu and Khomami2025) and experimental data (Zhang et al. Reference Zhang, Fan, Su, Xi and Sun2025) at different
$\eta$
are added for comparison. Note that Zhang et al. (Reference Zhang, Fan, Su, Xi and Sun2025) did not provide the polymer stress due to the lack of experimental techniques for characterising polymer deformation.

(
$a$
) Competition of the convective and elastic contributions to the angular momentum transport. Only four typical values of
$\beta$
are shown for simplicity. (
$b$
) The contributions of diffusive (
$J_d^v$
), convective (
$J_c^v$
) and elastic (
$J_p^v$
) fluxes to the angular momentum transport at various
$\beta$
. The values have been scaled by the angular momentum flux in the Newtonian flow state. The superscript ‘
$v$
’ denotes the volume average calculated by the integral across the gap, e.g.
$J_{c}^{v}=({1}/{d})\int _{R_i}^{R_o}{ J_{c}^{\omega } {\textrm{d}}r}$
.

Evidently, the competition between the reduction of Reynolds stress and the development of polymer stress gives rise to the observed ADM state transition. To highlight this, we examine the contribution of convective fluxes (
$J_c^\omega$
) and elastic (
$J_p^\omega$
) fluxes to angular momentum transport that correspond to Reynolds and polymer stresses, respectively. As depicted in (3.1), these fluxes are calculated as
$J^{\omega }_c=r^3\langle u_r\omega \rangle$
and
$J^{\omega }_p= -r^2( 1-\beta )\langle \tau _{r\theta }\rangle /Re$
. The remaining part of (3.1) represents the diffusive flux
$J_d^\omega$
. To illustrate the general contribution of different angular momentum fluxes, we present in figure 6 the volume-averaged values of
$J_c^\omega$
,
$J_p^\omega$
and
$J_d^\omega$
. Clearly, the ADM state is realised as a consequence of the saturation of different angular momentum transport mechanisms (see figure 6
$a$
), consistent with our previous observations (Zhu et al. Reference Zhu, Wan, Lin, Liu, Lu and Khomami2023; Lin et al. Reference Lin, Song, Liu, Wan, Lu and Khomami2024b
, Reference Lin, Song, Liao, Liu, Lu and Khomami2025). Furthermore, the underlying mechanism for the occurrence of the ADM state transition is substantiated by the competition of
$J_c^v$
reduction and
$J_p^v$
development illustrated in figure 6(
$b$
). Specifically, the addition of polymers to the turbulent TCF inevitably leads to the suppressed Reynolds stress and to the introduction of polymer stress. In the ADM state at
$\beta =0.98$
, the reduction
$J_c^v$
is perfectly compensated by the development
$J_p^v$
, leading to an asymptotic drag-limiting state of nearly zero DM extent. The
$J_c^v$
–
$J_p^v$
competition in TCF drastically differs from observations in parallel shear turbulent flow, where the Reynolds stress nearly vanishes as turbulent motions are greatly suppressed (Warholic, Massah & Hanratty Reference Warholic, Massah and Hanratty1999; Li et al. Reference Li, Sureshkumar and Khomami2006; Wang et al. Reference Wang, Zhang, Wang, Li, Zhang and Li2023), but the polymer stress remains small because the weak and few turbulent vortices cannot stretch polymers sufficiently (Xi Reference Xi2019; Zhu & Xi Reference Zhu and Xi2021; Lin et al. Reference Lin, Song, Liao, Liu, Lu and Khomami2025). This is analogous to a large reduction
$J_c^v$
and a small development
$J_p^v$
, which explains why only the MDR state is observed for channel/pipe flows. The above argument regarding the competition between
$J_c^v$
reduction and
$J_p^v$
development also provides a consistent view to understand the intriguing DM phenomena in viscoelastic TCF (see figure 2). That is, variations in
$Re,\eta ,Wi,\beta$
result in varying degrees of reduction in
$J_c^v$
and
$J_p^v$
growth, leading to different degrees of DM.
In general, the above findings provide clear answers to the questions posed in the introduction. That is, direct transition paths exist between MDR and MDE, while they each represent distinctive regimes in the phase space of various ADM states. To achieve this state transition pathway, our study highlights two critical parameters, namely
$\eta$
and
$\beta$
, which quantify the curvature effect and polymer concentration, respectively. We speculate that varying other parameters that can effectively manipulate the
$J_c^v$
–
$J_p^v$
competition may also lead to a similar transition pathway from MDR to MDE. In fact, in the following section we demonstrate that changes in control parameters indeed modify the elastic instabilities, which in turn result in structural changes and corresponding turbulent transport modifications.
3.2. Flow structures and regime identification
An overview of the flow structures for various ADM states is depicted by the space–time plots in figure 7. As
$\beta$
decreases, the dominant flow structure in the asymptotic drag-limiting flow state undergoes a structural change. At
$\beta =0.99$
, the highly intermittent inflow/outflow streaks signify the persistence of large-scale Taylor vortices in the flow field (Dutcher & Muller Reference Dutcher and Muller2009), whereas the strong SSS characteristic of Newtonian TCF are markedly suppressed. This is consistent with previous numerical and experimental observations in the MDR state with a weaker curvature effect
$\eta =0.714,0.99$
(Zhang et al. Reference Zhang, Fan, Su, Xi and Sun2025; Lin et al. Reference Lin, Song, Liao, Liu, Lu and Khomami2025). In contrast, the MDE state at
$\beta =0.90$
is populated by small-scale flow structures, which manifest themselves as random inflow/outflow spots in the space–time plot (see figure 7
$f$
). Interestingly, for intermediate
$\beta$
values, a transition of flow structures is observed in the ADM state. In particular, transitional flow patterns are attained for the ADM states at
$\beta =0.98,0.97$
, for which only a slight DM rate is achieved (see figure 1
$a$
). As shown in figure 7(
$b,\!c$
), although stronger randomness has been excited, the imprints of LSS can still be discerned within these transitional flow patterns.
Space–time plots of radial velocity
$u_r$
along the axial sampling line at the middle of the gap (
$\tilde {r}=0.5$
) for the ADM states (
$Wi=150$
) at (
$a$
)
$\beta =0.99$
, (
$b$
)
$\beta =0.98$
, (
$c$
)
$\beta =0.97$
, (
$d$
)
$\beta =0.95$
, (
$e$
)
$\beta =0.93$
and (
$f$
)
$\beta =0.90$
.

In contrast to the classical MDR in parallel shear channel/pipe flows, here the MDR states at higher
$\beta$
do not exhibit hibernating/active behaviours. This is due to the persistence of centrifugal-force-induced LSS, which contribute significantly to global angular momentum transport (Zhang et al. Reference Zhang, Fan, Su, Xi and Sun2025). It is also worth noting that the flow structures observed in the ADM states are consistent with previous findings in the EIT or elastically dominated turbulence (EDT) regime of viscoelastic TCF. Specifically, the LSS at higher
$\beta$
are reminiscent of the lower-
$Re$
solitary pairs of vortices (Boulafentis et al. Reference Boulafentis, Lacassagne, Cagney and Balabani2024), which display chaotic merging and splitting dynamics (Lacassagne et al. Reference Lacassagne, Cagney, Gillissen and Balabani2020). By contrast, the SSS observed in the MDE at lower
$\beta$
correspond to similar structures documented in the EDT regime (Song et al. Reference Song, Lin, Liu, Lu and Khomami2021), highlighting the relevance of EIT/EDT to ADM states. Overall, the above observation demonstrates that the extent of DM for an ADM state is closely related to its dominant flow structure. That is, ADM states exhibiting a stronger dominance of small-scale flow structures are more likely to experience higher turbulent flow drag, underscoring the intriguing competition between large- and small-scale flow structures in the ADM state transition.
Although the SSS are present in both Newtonian flow and the MDE state, their generation mechanisms are strikingly different. This is demonstrated by scrutinising the budget equation for streamwise enstrophy
$\langle \omega _\theta ^2 \rangle$
(detailed descriptions are given in Appendix B) (Kim et al. Reference Kim, Li, Sureshkumar, Balachandar and Adrian2007). Two key production terms are examined: (i) the elastic production term
$W_p$
, which represents the work performed by the polymer-induced torque; and (ii) the inertial production term
$W_c$
, which combines the contribution of stretching, tilting and twisting of vortical structures (Zhu et al. Reference Zhu, Song, Lin, Liu, Lu and Khomami2022). Figure 8 demonstrates the mechanistic differences in the generation of SSS between Newtonian flow and polymer-induced ADM states. Specifically,
$W_c$
, which drives the formation of inertial Görtler vortices, is greatly suppressed in the ADM states. This finding is consistent with experimental observations that polymer additives effectively inhibit the generation of inertial Görtler vortices (Lee, Sengupta & Wei Reference Lee, Sengupta and Wei1995). On the other hand,
$W_p$
increases monotonically with decreasing
$\beta$
, and at
$\beta =0.98$
it becomes greater than
$W_c$
in its Newtonian counterpart. This demonstrates the emergence of distinctive SSS, which have been referred to as elastic Görtler vortices due to their elastically driven nature (Song et al. Reference Song, Teng, Liu, Ding, Lu and Khomami2019, Reference Song, Lin, Liu, Lu and Khomami2021). In particular, the positive
$W_p$
observed presents a striking contrast to the negative
$W_p$
reported in viscoelastic channel flow (Kim et al. Reference Kim, Li, Sureshkumar, Balachandar and Adrian2007), where the effects of polymer-induced torque were shown to suppress shear-energised vortices.
The generation mechanism for the SSS in the near inner wall region for the ADM states (
$Wi=150$
) at various
$\beta$
, which is quantified as the competition between the combined inertial production term
$W_c$
and the work done by the polymer-induced torque
$W_p$
.

One-dimensional spanwise spectra of the TKE (
$\langle \boldsymbol{u}' \boldsymbol{\cdot }\boldsymbol{u}' \rangle /2$
) at the middle of the gap (
$\tilde {r}=0.5$
) for the ADM states (
$Wi=150$
) achieved in this study. For a more reasonable comparison, the values have been scaled by the corresponding
$u_\tau ^2$
at various
$\beta$
. The decaying law
$k_z^{-2.6}$
is obtained by fitting the spectral curve at
$\beta =0.90$
in the
$8\leqslant k_z\leqslant 40$
regime (Boulafentis et al. Reference Boulafentis, Lacassagne, Cagney and Balabani2024). The classical decaying laws for Newtonian turbulence
$k_z^{-5/3}$
and for MDR in parallel shear turbulent flows
$k_z^{-14/3}$
(Dubief et al. Reference Dubief, Terrapon and Soria2013) are added for comparison. The vertical dashed line indicates the wavenumber corresponding to the gap width, namely,
$k_z^d=2\pi /d\approx 6$
.

To examine the interaction between these flow structures and polymers, we analyse the spectral properties of the ADM states first, which also allows for a quantitative characterisation of the polymer-induced modification on LSS. As depicted in figure 9, varying
$\beta$
significantly modulates the spectral characteristics of the TKE, especially in the large-scale regime. Specifically, the appearance of the spectral peak shifts from
$k_z=3$
for Newtonian flow to
$k_z=2$
for
$\beta =0.99$
. The dominance of large-scale modes gradually decreases as
$\beta$
is decreased, and eventually no obvious spectral peak can be seen for MDE states at lower
$\beta$
. This provides direct evidence for our observation depicted in figure 7, namely, the decrease of
$\beta$
gradually modifies the LSS in the ADM states. In the following, we quantitatively demonstrate that these modifications lead to a smaller portion of large-scale TKE; equivalently, to a larger portion of small-scale TKE. However, the power-law decay for small-scale TKE of ADM states is not significantly altered, as demonstrated by the spectral curves that obey the scaling
$-2.6$
in the
$8\leqslant k_z \leqslant 40$
regime. This scaling exponent exhibits remarkable agreement with the experimental findings reported by Boulafentis et al. (Reference Boulafentis, Lacassagne, Cagney and Balabani2024) in the EIT regime of viscoelastic TCF. Additionally, Boulafentis et al. (Reference Boulafentis, Lacassagne, Cagney and Balabani2024) showed that this decay exponent is independent of fluid elasticity (
$Wi/Re$
). In the present case, it is also independent of
$\beta$
, indicating that the scaling
$k_z^{-2.6}$
may be unaffected by fluid rheology and flow parameter (Yamani et al. Reference Yamani, Keshavarz, Raj, Zaki, McKinley and Bischofberger2021). The power-law decay
$k_z^{-14/3}$
, commonly observed in the EIT of channel flow (Dubief et al. Reference Dubief, Terrapon and Soria2013; Wang et al. Reference Wang, Zhang, Wang, Li, Zhang and Li2023), has also been added for comparison. The TKE spectrum deviates from
$k_z^{-14/3}$
(for a more rigorous examination, see Appendix C), indicating the distinctive polymer-induced dynamics for viscoelastic TCF. It is important to note that, due to the wide parameter space involved, different decay exponents for the spatial spectra have been reported (Latrache et al. Reference Latrache, Kelai, Bai, Crumeyrolle and Mutabazi2025). For example, experimental findings have reported values of
$-7/3$
(Moazzen et al. Reference Moazzen, Lacassagne, Thomy and Bahrani2023) and
$-2.6$
(Boulafentis et al. Reference Boulafentis, Lacassagne, Cagney and Balabani2024), while
$-3$
(Lopez Reference Lopez2022) or
$\lt -3$
(Song et al. Reference Song, Zhu, Lin, Liu and Khomami2023; Lin et al. Reference Lin, Song, Liao, Liu, Lu and Khomami2025) are found in numerical simulations. This highlights the need for a thorough investigation to ascertain the intriguing dependence of spectral characteristics for viscoelastic TCF across different parameter regimes.
Given the substantial modification of the flow structures during the transition from MDR to MDE of the ADM state, an important question arises: How do these structural changes influence polymer-flow interactions? To answer this question and illustrate the relevant polymer dynamics, we examined the polymer stretch for different ADM states. As shown in figure 10(
$a$
), all ADM states exhibit large polymer stretch (
$\langle \textrm{tr}(\unicode{x1D63E}\,)\rangle /L^2\gt 0.8$
) across the gap. This is in stark contrast to the small polymer stretch (e.g.
$\langle \textrm{tr}(\unicode{x1D63E}\,)\rangle /L^2\lt 0.1$
for
$L=120$
) typically observed in classical MDR for channel/pipe flows (Li et al. Reference Li, Sureshkumar and Khomami2006; Dallas et al. Reference Dallas, Vassilicos and Hewitt2010). This observation is consistent with the significant polymer stress development shown in figures 5(
$b$
) and 6, which facilitates the occurrence of MDE or low-DR MDR states. Comparison of different ADM states reveals a smaller and more asymmetric polymer stretch for smaller
$\beta$
, particularly in the bulk region. However, a larger polymer stretch at larger
$\beta$
does not necessarily guarantee larger effective elastic contributions to angular momentum transport (see the rescaled polymer stress in figures 5 and 6), which takes into account the factor
$(1-\beta )$
in the definition of
$J_p^\omega$
in (3.1).
(
$a$
) Ensemble-averaged polymer chain extension rate
$\langle {\textrm {tr}}(\unicode{x1D63E}\,)\rangle / L^2$
and (
$b$
) interaction between polymers and vortical structures for the ADM states (
$Wi=150$
) at various
$\beta$
. In panel (
$b$
) the contour plots illustrate the fluctuations of polymer chain extension, quantified as the r.m.s. values of
$\textrm{tr}(\unicode{x1D63E}\,)$
, and the superimposed solid and dashed lines respectively represent the positive and negative ensemble-averaged streamwise vorticity
$\langle \omega _\theta \rangle$
.

As clearly captured in figure 10(
$b$
), distinct radial distributions of polymer stretch in various
$\beta$
suggest unique polymer dynamics induced by different flow structures in ADM states. Specifically, we observe a strong correlation between the fluctuating polymer stretch and vortical structures. In fact, the pattern of polymer stretch changes as the ADM state transitions from MDR to MDE. For MDRs with higher
$\beta$
, polymers exhibit a high fluctuating stretch in the core region of large-scale Taylor vortices; that is, the stretch and relaxation of polymers are mainly confined within LSS. This feature is still discernible for the transitional
$\beta =0.98,0.97$
, where remnants of large-scale Taylor vortices persist in these two ADM states. The polymer dynamics induced by LSS occupying the entire gap also explain the relatively stronger symmetry of
$\langle \textrm{tr}(\unicode{x1D63E}\,)\rangle /L^2$
at
$\beta =0.99$
(see figure 10
$a$
), where the LSS result in more uniform polymer stretch in the bulk region. As
$\beta$
further decreased, the irregular pattern of
$\langle \omega _\theta \rangle$
demonstrates that in the ADM states the SSS are dominant (see figure 7). In this case, strong fluctuations of polymer stretch occur in the near-wall region where elastic Görtler vortices are most intense (Song et al. Reference Song, Lin, Liu, Lu and Khomami2021; Lin et al. Reference Lin, Song, Liu, Wan, Lu and Khomami2024b
). Such correlations between polymers and small-scale vortical structures are also highlighted in the wall-mode-dominated EIT of channel flows, for which pronounced polymer stretch correlates with shear-energised spanwise vortices in the near-wall regions (Dubief et al. Reference Dubief, Terrapon and Soria2013; Zhang et al. Reference Zhang, Shao, Li, Ma, Zhang and Li2021b
). Moreover, the polymer stretch fluctuations become stronger for smaller
$\beta$
, as indicated by the higher values of
$\textrm{tr}(\unicode{x1D63E}\,)'_{rms}/L^2$
in
$\beta =0.90$
. This underscores the increasingly dominant role of polymer dynamics and associated elastic effects on the transition path from MDR to MDE.
To quantify the strength of the elastic effect at various
$\beta$
and
$Wi$
, we evaluated the Pakdel–McKinley (PM) criterion, which was originally proposed to identify the primary elastic instability in curvilinear flows (McKinley, Pakdel & Öztekin Reference McKinley, Pakdel and Öztekin1996; Pakdel & McKinley Reference Pakdel and McKinley1996; Schäfer et al. Reference Schäfer, Morozov and Wagner2018). Specifically, motivated by the fact that elastic forces are closely related to the curvature of streamlines and polymer hoop stresses, McKinley et al. (Reference McKinley, Pakdel and Öztekin1996) proposed the following formulation for the onset of an elastic instability:
\begin{equation} M=\sqrt {Wi^{\textit{eff}}\epsilon \frac {N_1}{\varSigma _{r\theta }}}. \end{equation}
Here
$Wi^{\textit{eff}}$
is the effective Weissenberg number,
$N_1=\langle (1-\beta )(\tau _{\theta \theta }-\tau _{\textit{rr}})/Re\rangle$
is the first normal stress difference and
$\varSigma _{r\theta }$
is the total shear stress. As this study focuses on the viscoelastic TCF of the FENE-P fluid, the effective Weissenberg number is calculated as
$Wi^{\textit{eff}}=Wi[1-\textrm{tr}(\unicode{x1D63E}\,)/L^2]$
to account for the finite extensibility of the polymer chain (Li et al. Reference Li, Sureshkumar and Khomami2015). In general, the parameter
$M$
can be viewed as a viscoelastic Görtler number (Pakdel & McKinley Reference Pakdel and McKinley1996), which combines dimensionless measures of the radius of curvature and elasticity of the fluid. Evidently,
$Wi^{\textit{eff}}$
,
$N_1$
and
$\varSigma _{r\theta }$
depend on the flow conditions; therefore,
$M$
is a dynamic measure of the strength of elastic instability. We note that More et al. (Reference More, Patterson, Pashkovski and McKinley2024) recently proposed a unified PM criterion to predict the onset of elasto-inertial instability and validated it in a cone-plate geometry. Here, we do not choose this form, as we focus on the primary elastic instability resulting in small-scale elastic Görtler vortices observed at smaller
$\beta$
. In fact, the mechanism for the generation of these vortices is of elastic (instead of elasto-inertial) origin, as demonstrated in figure 8.
Figure 11(
$a$
) illustrates the radial dependence of
$M$
as the flow reaches the ADM state at
$\beta =0.99$
. For all
$Wi$
considered, two local maxima of
$M$
are observed in the regions near the wall. This results from the pronounced polymer stretch and the associated substantial
$N_1$
generated in the high-shear wall regions (see figure 10
$a$
). Although the polymer stretch is slightly larger in the near inner wall region, the implementation of
$Wi^{\textit{eff}}$
yields a larger local maximum of
$M$
in the near outer wall region. In general, the magnitude of
$M$
exhibits a monotonic increase across the entire gap as
$Wi$
increases, demonstrating the progressive enhancement of the elastic instability. This growth, however, diminishes at sufficiently high
$Wi$
, indicating imbibition of elastic instabilities at a given
$\beta$
. To quantify the variation in the strength of elastic instability, we have extracted the maximum value of
$M$
(the one near the outer wall) for each (
$\beta , Wi$
). Figure 11(
$b$
) reveals that elastic instabilities intensify with decreasing
$\beta$
and increasing
$Wi$
. In particular,
$M_{\textit{max}}$
exhibits a saturating trend with increasing
$Wi$
, consistent with the trend observed in
$Nu_\omega$
(see figure 1
$a$
). This correspondence underscores that asymptotic saturation of turbulent DM is fundamentally related to the imbibition of elastic instability, implying the elastically driven nature of drag-limiting states (Zhu et al. Reference Zhu, Wan, Lin, Liu, Lu and Khomami2023; Lin et al. Reference Lin, Song, Liu, Wan, Lu and Khomami2024b
). The higher values of
$M$
are obtained in the smaller
$\beta$
, demonstrating that decreasing
$\beta$
is obviously an efficient way to enhance the elastic instability.
(
$a$
) Radial distribution of the parameter
$M$
obtained from the Pakdel–McKinley criterion for various
$Wi$
at
$\beta =0.99$
. The radial dependence of
$M$
for other
$\beta$
exhibits similar behaviour, and thus, is not shown here. (
$b$
) The maximum value of
$M$
as a function of
$Wi$
at various
$\beta$
.

(
$a$
) Percentage of large-scale TKE (
${\textit{TKE}}^L$
) to total TKE for each pair of (
$\beta , Wi$
). Three regimes are roughly identified: LSS-dominated regime I,
$55\,\% \leqslant {\textit{TKE}^L}$
; transitional regime II,
$45\,\%\lt {\textit{TKE}^L}\lt 55\,\%$
; SSS-dominated regime III,
${\textit{TKE}^L}\leqslant 45\,\%$
. (
$b$
) Phase map based on the percentage of
${\textit{TKE}^L}$
. Hollow, half-filled and solid stars represent regimes I, II and III, respectively. In panel (
$b$
) the colour illustrates the
$M_{\textit{max}}$
obtained in figure 11(
$b$
). The dashed line indicates a contour line corresponding to
$M_{\textit{max}}=6.8$
(at
$\beta =0.97, Wi=150$
) with the grey shaded region showing a
$10\,\%$
deviation, i.e.
$M_{\textit{max}}=6.8\pm 0.68$
.

In fact, the elastic instability modulates the ADM states by suppressing large-scale Taylor vortices while promoting the formation of small-scale elastic Görtler vortices. To establish this relationship, we quantify the relative contributions of LSS and SSS in different ADM states by calculating the fraction of large-scale TKE (
${\textit{TKE}^L}$
) in the total TKE. Specifically, we define LSS as flow structures with an axial length scale comparable to the width of the gap, such as Taylor vortices (Barcilon & Brindley Reference Barcilon and Brindley1984; Dong Reference Dong2007). This criterion corresponds to a cutoff wavenumber of
$k_z^d=2\pi /d\approx 6$
as the spectral demarcation between large and small scales (see figure 9). Consequently,
${\textit{TKE}}^L$
is evaluated by integrating the TKE in all spatial modes that satisfy
$k_z\leqslant k_z^d$
, while the remainder is the small-scale contribution. As shown in figure 12(
$a$
), the energy fraction
${\textit{TKE}^L}$
varies significantly with both
$\beta$
and
$Wi$
. At low
$Wi$
, this fraction decreases significantly, consistent with the known polymer-induced suppression and stabilisation of LSS (Lin et al. Reference Lin, Song, Liao, Liu, Lu and Khomami2025; Zhang et al. Reference Zhang, Fan, Su, Xi and Sun2025). As
$Wi$
increases further,
${\textit{TKE}^L}$
approaches a fluctuating plateau, indicating that the ADM states are closely related to the saturation of energy at either large or small scales. Based on this energy fraction, we quantitatively classify the flow into three regimes: an LSS-dominated regime for
$55\,\% \leqslant {\textit{TKE}^L}$
, a transitional regime for
$45\,\%\lt {\textit{TKE}^L}\lt 55\,\%$
and an SSS-dominated regime for
${\textit{TKE}^L}\leqslant 45\,\%$
. This classification reveals that decreasing
$\beta$
drives the flow state from an LSS-dominated MDR to an SSS-dominated MDE, corroborating the observations in figure 7. Although the precise demarcations of flow regimes may depend on specific threshold values, the fundamental physics governing the transition in the dominant flow structure as
$\beta$
decreases is insensitive to threshold choice.
Figure 12(
$b$
) illustrates the relationship between elastic instability and the dominant flow structure in viscoelastic TCF. At lower values of
$M_{\textit{max}}$
(corresponding to low
$Wi$
and high
$\beta$
), the weak elastic instability is insufficient to destroy Taylor vortices (Liu & Khomami Reference Liu and Khomami2013), so the flow state is dominated by LSS. As
$M_{\textit{max}}$
increases, the flow enters the transitional regime dominated by LSS and SSS. In particular, this transition regime approximates the grey-shaded region,
$M_{\textit{max}}=6.8\pm 0.68$
, indicating that this value may be taken as a reasonable critical threshold for the transition of predominance between LSS and SSS. In fact,
$M_{\textit{max}}=6.8$
corresponds to the state of the ADM in
$\beta =0.97, Wi=150$
, where
${\textit{TKE}^L}$
is approximately
$50\,\%$
(see figure 12
$a$
). For comparison, Schäfer et al. (Reference Schäfer, Morozov and Wagner2018) reported a significantly lower critical elastic instability threshold of
$M=1.8\pm 0.3$
in a purely elastic (
$Re\to 0$
) TCF. This discrepancy is attributed to the following two factors. (i) In this study, conducted at the Reynolds number of
$Re=6000$
, stronger elastic forces (higher
$M$
) are required to overcome inertial stabilisation and excite different elastic structures. This is supported by previous findings that fluid inertia monotonically suppresses elasticity-driven flow modifications (Song et al. Reference Song, Lin, Liu, Lu and Khomami2021). (ii) The nature of the elastic instability differs between the purely elastic and EIT regimes. Whereas Schäfer et al. (Reference Schäfer, Morozov and Wagner2018) observed flow patterns reminiscent of large-scale diwhirls, our study reveals small-scale vortical structures, indicating a distinct instability mechanism.
At sufficiently large
$M_{\textit{max}}$
, the flow becomes SSS dominated, as shown by the solid stars in figure 12(
$b$
). The phase map demonstrates that a stronger elastic instability promotes the SSS dominance; for example,
$M_{\textit{max}} \approx 10$
for the ADM state at
$\beta =0.90, Wi=150$
leads to a
${\textit{TKE}^L}$
of merely
$40\,\%$
. Thus, these enhanced elastic Görtler vortices facilitate incoherent mixing of polymer stress, which, in turn, leads to efficient angular momentum transport and significant DE. This correlation between flow structures and elastic instability also explains the underlying mechanisms of the ADM state transition pathway with varying geometric curvature (see table 1). According to the PM criterion (3.2), a lower curvature effect results in a lower value of
$M$
and, thus, weaker elastic instability. In low-curvature TCF (
$\eta =0.99,0.714$
), the instability is too weak to generate elastic Görtler vortices, while polymer additives still suppress the inertial Taylor vortices, resulting in an asymptotic MDR state (Lin et al. Reference Lin, Song, Liao, Liu, Lu and Khomami2025; Zhang et al. Reference Zhang, Fan, Su, Xi and Sun2025). In contrast, the stronger elastic instability in the high-curvature case (
$\eta =0.5$
) easily eliminates Taylor vortices and generates elastic Görtler vortices, driving the flow to an asymptotic MDE state (Lin et al. Reference Lin, Song, Liao, Liu, Lu and Khomami2024b
). These findings suggest a promising strategy for control of the flow structure in TCF, namely, by tuning the elastic effects and their associated instabilities, one can control the balance between LSS/SSS to manipulate turbulent transport, as indicated by Xu et al. (Reference Xu, Liu, Li and Xia2025). Moreover, our findings highlight the enhancement of elastic instability as
$\beta$
decreases (i.e. as concentration increases), which may induce a degree of shear thinning in real polymer solutions. Previous experimental studies (Cagney, Lacassagne & Balabani Reference Cagney, Lacassagne and Balabani2020; Lacassagne, Cagney & Balabani Reference Lacassagne, Cagney and Balabani2021) have demonstrated that significant shear thinning can suppress or even completely eliminate viscoelastic instabilities. However, within the range of
$\beta$
values considered in this study, the selected value of
$L=100$
is sufficiently large such that shear-thinning effects are minimal in our simulations, as demonstrated in Appendix D. Based on these prior experiments, it is anticipated that, if significant shear thinning occurs, it could inhibit the onset of the MDE state, as the elastic instability responsible for the formation of elastic Görtler vortices will be suppressed.
By further considering the elastic instabilities in different parameter spaces, we summarise the mechanism governing the ADM state transition as follows. At high values of
$\beta$
(e.g. 0.99), weak elastic effects suppress but do not eliminate Taylor vortices, resulting in a significant reduction of Reynolds stress and, hence, an asymptotic MDR state. As
$\beta$
decreases, the enhanced elastic forces and instabilities promote the formation and progressive increase of elastic Görtler vortices. The incoherent transport driven by these SSS leads to efficient mixing and a significant development of polymer stress, ultimately establishing an asymptotic MDE state. In fact, elastic effects and associated instabilities depend on multiple key parameters, including
$Re,\beta ,\eta ,L,Wi$
. This dependence underscores the potential for the realisation of diverse ADM transition pathways and points to the existence of distinct phase diagrams of ADM states with varying degrees of DM.
3.3. Energy transfers and scale interactions
The intriguing competition between LSS and SSS in the ADM states of viscoelastic TCF motivates fundamental questions regarding the mechanisms of TKE production at different scales and the process of interscale energy transfer. To investigate these interscale interactions, we derive and examine the scale-decomposed TKE transport equation for viscoelastic TCF, following the methodology proposed by Kawata & Alfredsson (Reference Kawata and Alfredsson2018). Specifically, the fluctuating velocity and polymer stress fields, denoted by
$\phi '$
, are decomposed into large-scale (
$\phi '_L$
) and small-scale (
$\phi '_S$
) components by spatial filtering at an axial cutoff wavenumber,
$k_z^{\textit{filter}}$
, such that
$\phi '=\phi '_L+\phi '_S$
. Because this spatial filtering is based on an orthogonal-mode (Fourier-mode) decomposition, cross-correlation terms between the large- and small-scale quantities vanish. This property enables a direct decomposition of the TKE transport equation into large- and small-scale budgets:
Basically, the scale-decomposed transport equation of TKE has a similar form to the transport equation of the total TKE (Bilson & Bremhorst Reference Bilson and Bremhorst2007; Song et al. Reference Song, Lin, Liu, Lu and Khomami2021). Using (3.3) as an example, the left-hand side is merely the total time derivative of large-scale TKE
$e_L$
following a mean flow fluid parcel, while the terms on the right-hand side represent the various large-scale mechanisms that produce, dissipate or transport large-scale TKE. Specifically,
$P_{t}^{L}$
is the turbulence shear production term that arises due to the interaction of mean flow shear and large-scale Reynolds stress, and
$P_{e}^{L}$
represents the production of TKE associated with polymer stretch. As the primary TKE generation terms, they will be examined in detail. The terms
$D_{p}^{L}$
,
$D_{t}^{L}$
,
$D_{d}^{L}$
and
$D_{e}^{L}$
denote the transport and redistribution of large-scale TKE caused by pressure, turbulent stress, viscous diffusion and polymer stress, respectively. Here
$\varepsilon _t^{L}$
represents the direct viscous dissipation of large-scale TKE through its conversion to heat. A key difference from the total TKE budget is the term
$T_r$
, which represents the turbulent interscale transport of TKE arising from the nonlinear interaction between the large- and small-scale parts of the velocity field (Kawata & Alfredsson Reference Kawata and Alfredsson2018, Reference Kawata and Alfredsson2019; Kawata & Tsukahara Reference Kawata and Tsukahara2021). A positive
$T_r$
indicates an interscale energy flux from large to small scales along the cutoff wavenumber
$k_z^{filter}$
, and vice versa. A detailed description of the scale-decomposed transport equation of TKE is given in Appendix E.
Following our earlier definition of LSS, we set the filter scale at
$k_z^{filter} = k_z^d$
to scrutinise the transport and generation of TKEs within large- and small-scale regimes. To highlight polymer-induced modifications, we analyse the AMD state that corresponds to the largest elastic effect (
$\beta =0.90, Wi=150$
). The transport budgets illustrated in figure 13 show good total balances for (3.3) and (3.4), confirming the reliability of the analytical derivation of budget equations and numerical solution to obtain the data set. A key finding is that in both budgets, TKE redistribution is overwhelmingly dominated by the polymer stress term (
$D_e^{L},D_e^{S}$
), whereas in the Newtonian counterpart, pressure and turbulent stress transport are the primary mechanisms (Bilson & Bremhorst Reference Bilson and Bremhorst2007). The viscous transport term (
$D_d^{L},D_d^{S}$
) is significant only near the walls. This dominance of polymer stress transport is consistent with the efficient angular momentum transport observed for the MDE state in figure 6.
The transport budgets for (
$a$
) large-scale and (
$b$
) small-scale TKE of the ADM state at
$\beta =0.90, Wi=150$
. Here, only the inner half of the gap is presented for clarity. The values have been scaled by
$u_{\tau }^4/\nu$
(Teng et al. Reference Teng, Liu, Lu and Khomami2018). We implement a filtered scale of
$k_z^{filter}=k_z^d$
, corresponding to the gap width.

The radial distributions of scale-decomposed (
$a$
) inertial and (
$b$
) elastic production terms in various flow states. The values have been scaled by
$u_{\tau }^4/\nu$
. For different ADM states, the same filtered scale of
$k_z^{filter}=k_z^d$
is implemented.

To further investigate the mechanisms of TKE generation in large- and small-scale regimes, we delve into the inertial and elastic production terms. Figure 14 compares
$P_t^{L},P_t^{S}$
and
$P_e^{L},P_e^{S}$
in various
$\beta$
to highlight the differences in TKE production for various ADM states. Evidently,
$P_t^{L}$
and
$P_t^{S}$
are positive across the gap, with their peaks occurring in the near-wall region, for example,
$r^+=10$
for
$P_t^S$
and
$r^+=14$
for
$P_t^L$
at
$\beta =0.99$
. This behaviour can be attributed to the significant mean flow shear (see figures 3 and 4). As the ADM state transitions from MDR to MDE, these peaks are slightly away from the walls, indicating enlargement of the buffer layer (White & Mungal Reference White and Mungal2008; Xi Reference Xi2019). Based on the values of
$P_e^{L}$
and
$P_e^{S}$
, the radial distributions of
$P_e^{L}$
and
$P_e^{S}$
demonstrate three typical energy exchange regions (Dallas et al. Reference Dallas, Vassilicos and Hewitt2010; Tsukahara et al. Reference Tsukahara, Ishigami, Yu and Kawaguchi2011; Teng et al. Reference Teng, Liu, Lu and Khomami2018) for elastic TKE production at large and small scales (see figure 14
$b$
), indicating that the universal mechanism of polymer–turbulence interaction remains valid in a scale-decomposed framework. Specifically, in the vicinity of the wall and in the core regions, the negative values of
$P_e^{L}$
and
$P_e^{S}$
signify that the kinetic energy carried by fluctuating large- and small-scale motions is absorbed and stored as elastic potential energy in the stretched polymer chains. In contrast, the positive values of
$P_e^{L}$
and
$P_e^{S}$
in the near-wall region indicate that elastic potential energy is released from the stretched polymer chains back to turbulent flow. As the ADM state transitions with decreasing
$\beta$
, we observe a weakening of inertial production and an increase of elastic production, consistent with the progressive enhancement of elastic instability depicted in figure 11. Nevertheless, the inertial production does not vanish at
$\beta =0.90$
, and turbulent motion arises from both inertial and elastic forces in various
$\beta$
. Hence, the ADM states observed in this study are in the EIT/EDT regime (Zhu et al. Reference Zhu, Wan, Lin, Liu, Lu and Khomami2023; Lin et al. Reference Lin, Song, Liu, Wan, Lu and Khomami2024b
).
Although the ADM state at higher
$\beta$
possesses a larger fraction of large-scale TKE (see figure 12
$a$
), the production of TKE arises primarily from SSS, as evidenced by the higher values of
$P_t^S$
and
$P_e^S$
(see figure 14). This observation is physically reasonable because the TKE generated by the small-scale dynamics can still be transferred to the large-scale regime through the interaction between LSS and SSS, which can be quantified by examining the interscale energy transport term
$T_r$
. In figure 15(
$a$
), pronounced negative values of
$T_r$
, which signify the inverse energy transfer from small to large scales, are observed in the near-wall region (around
$r^+=10$
). This finding is consistent with observations in Newtonian channel flow, where the inverse energy cascade occurs in the buffer layer (
$6\lt y^+\lt 37$
, where
$y^+$
is the wall distance at the inner scale in channel flow) (Saikrishnan et al. Reference Saikrishnan, De Angelis, Longmire, Marusic, Casciola and Piva2012). As the ADM state transitions from MDR to MDE, the magnitude of
$T_r$
decreases, indicating weak-scale interactions for the transfer of TKE. This reduction is attributed to the polymer-induced suppression of velocity fluctuations (see figure 5
$a$
), which facilitates smaller Reynolds stresses on large and small scales (see (E6)). The introduction of polymer additives produces a striking difference in energy transfer in the core region. Although Newtonian flow exhibits a classical forward energy transfer (positive
$T_r$
) from larger to smaller scales in
$r^+\gt 20$
, the inverse energy cascade persists for the asymptotic ADM states at various
$\beta$
, as highlighted in the inset of figure 15(
$a$
).
(
$a$
) The radial distribution of interscale transfer term
$T_r$
at the filter scale
$k_z^{filter}=k_z^d$
for various ADM states. The inset depicts a zoom in of the core region. (
$b$
) Space–wavelength diagrams of
$T_r$
in the Newtonian flow state (left), MDR state at
$\beta =0.99, Wi=150$
(middle) and MDE state at
$\beta =0.90, Wi=150$
(right). The horizontal dashed line indicates the filter scale
$k_z^{filter}=k_z^d$
, corresponding to the radial distribution in panel (
$a$
). Following the same style in figure 13, the values are also scaled by
$u_{\tau }^{4}/\nu$
.

It should be noted that the above discussions are based on energy transfer on the cutoff scale
$k_z^{filter}=k_z^d$
. To provide a more comprehensive picture of the energy transfer at different scales, we examine the space–wavelength diagrams of
$T_r$
for three typical cases: Newtonian flow, MDR at
$\beta =0.99$
and MDE at
$\beta =0.90$
. As depicted in figure 15(
$b$
), for the Newtonian flow, the interscale flux mostly indicates energy transfer from larger to smaller scales, while inverse energy transfer is only observed in the near-wall regions for relatively larger scales (
$\lambda _z \gt 0.3d$
). Of interest, Kawata & Alfredsson (Reference Kawata and Alfredsson2019) reported a similar space–wavelength diagram for the interscale flux of wall-normal velocity fluctuations in turbulent plane Couette flow under strong rotation (cf. figure 7 in their paper). This underscores the similarity of flow dynamics between TCF and the rotating plane Couette flow (Brauckmann, Salewski & Eckhardt Reference Brauckmann, Salewski and Eckhardt2016). In contrast, for the polymer-induced ADM states, striking differences emerge in the core region, consistent with the observation in figure 15(
$a$
). Specifically, while
$T_r$
in the near-wall region exhibits a behaviour similar to its Newtonian counterpart, negative values of
$T_r$
are observed across a wide range of
$\lambda _z$
for the core region (
$0.2\lt \tilde {r}\lt 0.8$
). To the best of our knowledge, such inverse TKE transfer in wall-bounded viscoelastic turbulent flows has not been previously reported. The underlying mechanism for the inverse TKE transfer is related to the distinctive polymer dynamics, which we discuss in detail through the following scale-by-scale analysis.
To further examine how TKE is generated and transferred between different scales in the ADM states, we examine the scale-by-scale production and interscale transport of TKE. Specifically, differentiating (3.3) with respect to
$k_z$
produces the scale-by-scale transport equation of the TKE (Kawata & Alfredsson Reference Kawata and Alfredsson2018). We focus in particular on scale-by-scale inertial production
$p_t$
, elastic production
$p_e$
and interscale transport
$t_r$
. A detailed description of these terms is provided in Appendix E. Here, positive and negative values of
$p_t$
,
$p_e$
,
$t_r$
represent the local gain and loss of TKE on scale
$k_z$
, respectively. Given that the above discussions have highlighted the occurrence of inverse energy transfer in the core region, we specifically inspect the scale-by-scale TKE production and transfer in the middle of the gap (
$\tilde {r}=0.5$
).
Figure 16(
$a$
) shows the premultiplied scale-by-scale inertial production
$k_z p_t$
. For Newtonian flow,
$k_z p_t$
exhibits two local maxima, one at
$\lambda _z=2.09d$
corresponding to the axial length of Taylor vortices of a large scale (see figure 9), and another at a relatively smaller scale
$\lambda _z=0.7d$
, demonstrating that mean flow shear generates TKE across a wide range of scales (Kawata & Alfredsson Reference Kawata and Alfredsson2019). Consistent with previous observations (figure 14), the addition of polymers results in the suppression of inertial production at different scales, with the suppression effect becoming more significant as
$\beta$
decreases. For the ADM state at
$\beta =0.99$
, a pronounced local maximum at
$\lambda _z=3.14d$
remains observable in the large-scale regime, as turbulent motions of persistent LSS contribute to TKE production. However, this peak disappears as
$\beta$
decreases, because the enhanced elastic forces have broken the regular pattern of LSS and reinforced the dominance of SSS. These findings align with the structural changes shown in figure 7.
Profiles at the middle of the gap of the premultiplied scale-by-scale (
$a$
) inertial production
$k_z p_t$
, (
$b$
) elastic production
$k_z p_e$
, and (
$c$
) interscale transport
$k_z t_r$
for the TKE of various flow states. The values have been scaled by
$u_{\tau }^{3}/d$
, and the vertical dashed line indicates the filtered scale implemented in figure 13. Here, positive and negative values represent the local gain and loss of TKE at scale
$\lambda _z$
, respectively.

The premultiplied scale-by-scale elastic production
$k_z p_e$
in the middle of the gap is depicted in figure 16(
$b$
). As polymers can absorb energy from turbulent motions through their extensions,
$k_z p_e$
has negative values in the core region. Based on the value of
$k_z p_e$
, two distinct regimes are identified: polymers extract TKE on relatively larger scales (around
$\lambda =d$
) and release energy to turbulent motion on small scales. Thus, the effect of polymers on turbulent fluctuations is a redistribution of energy among different scales. Interestingly, this can be viewed as an effective polymer-induced energy cascade, in which the elastic energy flux plays a significant role (Xi, Bodenschatz & Xu Reference Xi, Bodenschatz and Xu2013; Zhang et al. Reference Zhang, Bodenschatz, Xu and Xi2021a
). This scenario is consistent with the early cascade picture proposed by Tabor & de Gennes (Reference Tabor and de Gennes1986), wherein polymer elasticity reshapes turbulent interscale energy transfer. Similar findings have been observed in viscoelastic homogeneous isotropic turbulence (Valente, Da Silva & Pinho Reference Valente, Da Silva and Pinho2014), where polymers can remove more energy from the large scales than they can dissipate and transfer the excess energy to turbulent dissipative scales. As polymers continuously pump energy to small scales, the following mechanism emerges: if the accumulated energy on the small scales cannot be dissipated directly into heat, it would be transferred back to the large-scale regime via the interaction between large- and small-scale velocity fluctuations (i.e. term
$T_r$
), causing the inverse energy transfer observed in the core region. A recent observation in Newtonian TCF has confirmed this postulated mechanism: Zhou et al. (Reference Zhou, Dou, Niu and Xu2025) found that small-scale vortices with high turbulent energy coexist with large-scale vortices and cannot be dissipated by low shear stress, resulting in an inverse energy cascade.
The premultiplied interscale transport scale-by-scale
$k_z t_r$
is shown in figure 16(
$c$
), further highlighting the distinction between the scale interactions in Newtonian and viscoelastic flows. For Newtonian flow,
$t_r$
transfers energy from large scales to smaller scales, consistent with the classical view of the turbulent energy cascade. In contrast,
$t_r$
in viscoelastic flow exhibits an opposite trend due to the polymer-induced energy redistribution discussed above among different scales. That is, positive and negative values of
$t_r$
are observed in the large- and small-scale regimes, respectively, demonstrating that the interaction between large- and small-scale turbulent motions results in inverse energy transfer. Exploring whether such a reverse energy cascade exists in other viscoelastic flows and its correlation with the asymptotic saturation flow states represent intriguing topics for future research.
4. Conclusions
In this work, extensive DNS of a moderate-curvature (
$\eta =0.6$
) TCF at
$Re=6000$
have been performed to explore polymer-induced asymptotic flow states with saturated DM. By gradually increasing
$Wi$
from 10 to 150, it is found that ADM states are achieved at different solvent-to-total viscosity ratios. As
$\beta$
decreases from 0.99 to 0.90, corresponding to dilute polymer solutions, a continuous transition pathway from MDR to MDE is reported for the first time. Specifically, a gradual reduction of
$\beta$
leads to a sequence of ADM state transitions: from an MDR state with low DR
$\sim -11.7\,\%$
at
$\beta =0.99$
to an ADM state with nearly zero DM at
$\beta =0.98$
, followed by an MDE state with slight DE
$\sim 6.0\,\%$
at
$\beta =0.97$
. The degree of DE in MDE states increases monotonously to
$34.6\,\%$
after further decreasing
$\beta$
to 0.90. This flow state transition is accompanied by modifications in the mean streamwise velocity profiles, namely, the parameter
$\kappa$
of the von Kármán-like logarithmic law increases as the ADM state transitions from MDR to MDE. Through examination of angular momentum fluxes, it is demonstrated that the ADM state transition stems from the competition between Reynolds stress reduction and polymer stress development, namely, a mechanistic change in angular momentum transport.
A careful analysis of flow structures for different ADM states demonstrates a structural transition from LSS-dominated to SSS-dominated flow states as
$\beta$
gradually decreases. In LSS-dominated MDR, intense polymer stretch fluctuations are confined in the core region of large-scale Taylor vortices, whereas they are concentrated in the near-wall regions for the SSS-dominated MDE. These intriguing polymer dynamics underscore the differences in the elastic driving forces for different ADM states, which are further quantified by the PM criterion. To this end, the relationship between ADM state transition, structural change and elastic instability is established: decreasing
$\beta$
effectively enhances elastic instability, which eliminates Taylor vortices on a large scale and gives rise to the small-scale elastic Görtler vortices; the enhanced dominance of SSS results in stronger incoherent transport that facilitates efficient mixing and significant development of polymer stress, leading to the ADM state transition. These findings present a unified perspective for determining the underlying mechanisms of DM in viscoelastic TCF. That is, elastic forces and associated instabilities determine the flow structures, thereby modulating turbulent transport and resulting in DM. This perspective is further supported by previous observations that different ADM states can be realised in TCFs with varying geometric curvature.
Given that the observed ADM state transition presents the competition between LSS and SSS, we further derive and examine the scale-decomposed transport equations of TKE to better understand the mechanisms governing energy transfer and scale interaction. In both large- and small-scale regimes, decreasing
$\beta$
leads to suppression and enhancement of inertial and elastic TKE productions, respectively, signifying a transition from elasto-inertial to elastically driven turbulence. The universal mechanism of the polymer–turbulence interaction remains valid in a decomposed framework at both large and small scales. Overall, polymers absorb TKE from fluctuating motions in the vicinity of the wall and the core region and subsequently release the stored elastic energy back to the flow as the chains relax in the buffer layer. Examination of interscale transport demonstrates a striking difference at the centre of the gap between viscoelastic flow and its Newtonian counterpart. Specifically, while the Newtonian flow exhibits a classical forward energy transfer from larger to smaller scales, the addition of polymers leads to an inverse energy cascade where velocity fluctuation interactions move energy from smaller to larger scales. The occurrence of the inverse energy cascade is attributed to the polymer-induced energy redistribution. In the core region, polymers extract more energy from the large scales than they can dissipate. Hence, excess energy is redirected to smaller scales. The energy accumulating on smaller scales can not be immediately dissipated as heat. Therefore, it is transferred back to the large-scale regime via nonlinear-scale interactions. This mechanism sustains a novel polymer-mediated cycle of energy transport between large and small scales.
In summary, present DNS results demonstrate for the first time a continuous ADM state transition pathway from MDR to MDE in viscoelastic TCF, captured in the full phase diagram of the ADM state. This provides concrete evidence for the universality of polymer-induced asymptotic drag-limiting states in wall-bounded turbulent flows. The challenging question regarding how distinct ADM states emerge and their dynamical connections is resolved by a comprehensive examination of turbulence and polymer dynamics, which reveals the close relation between elastic instability, vortical structure and turbulent transport. These findings pave the way for coordinated experimental, simulation and theoretical studies of transition pathways to the desired ADM states.
Acknowledgements
The calculations were performed in the Supercomputing Center at the University of Science and Technology of China and the Hefei Advanced Computing Center.
Funding
This work was supported by the National Natural Science Foundation of China through grants numbers 12388101, 12402257, 12172353, 92252202; the Science Challenge Project, No. TZ2025016; the CPSF Postdoctoral Fellowship Program under grant number GZC20232551.
Declaration of interests
The authors report no conflict of interest.
Appendix A. Grid resolution test and convergence criterion
To validate the reliability of our simulations, we conduct comprehensive tests of grid resolution and, consequently, establish convergence criteria for viscoelastic TCF. Accurate simulation of viscoelastic turbulent flows requires high grid resolution to capture sharp gradients in
$\unicode{x1D63E}$
and
$\boldsymbol{\tau }$
that develop with increasing
$Wi$
(Alves et al. Reference Alves, Oliveira and Pinho2021; Dubief et al. Reference Dubief, Terrapon and Hof2023). This challenge is further exacerbated by the high computational cost of resolving the constitutive equation (2.3), which requires computational power typically of an order of magnitude greater than its Newtonian counterpart (Dallas et al. Reference Dallas, Vassilicos and Hewitt2010; Lin et al. Reference Lin, Wan, Zhu, Liu, Lu and Khomami2022). Therefore, a rigorous grid convergence criterion is crucial to ensure flow solution accuracy while mitigating computational expenses. For EIT in viscoelastic channel flows, extensive studies have identified three key resolution parameters: overall grid points, the size of the cell on the wall (
$\varDelta _{\textit{min}}$
) and the Schmidt number (when an artificial diffusion is implemented) (Sid, Terrapon & Dubief Reference Sid, Terrapon and Dubief2018; Gupta & Vincenzi Reference Gupta and Vincenzi2019; Dubief et al. Reference Dubief, Page, Kerswell, Terrapon and Steinberg2022). These investigations have successfully established quantitative thresholds, that is,
$\varDelta _{\textit{min}}\leqslant 10^{-4}$
is necessary to resolve the intense polymer stress gradients in low-
$Re$
chaotic EIT regimes. However, similar convergence criteria have yet to be developed for viscoelastic TCF, for which additional complexities arising from curvature effects and rotational dynamics may impose more stringent resolution requirements.
Following the methodology established for Newtonian TCF by Ostilla-Mónico et al. (Reference Ostilla-Mónico, Stevens, Grossmann, Verzicco and Lohse2013), we examine the grid convergence criteria for viscoelastic TCF based on numerical precision in maintaining the key dynamical properties of the flow system. Specifically, for TCF, which is considered as a closed system, an exact global balance relation between the driving force and dissipation can be derived (Eckhardt et al. Reference Eckhardt, Grossmann and Lohse2007; Grossmann et al. Reference Grossmann, Lohse and Sun2016). In our recent work (Lin et al. Reference Lin, Song, Liu, Liu, Lu and Khomami2024a ), this relation was extended to viscoelastic TCF, which produced
The definitions of each term in (A1) are provided in the main text. Moreover, TCF should preserve a constant angular momentum flux
$J^{\omega }$
across the gap in a statistically stationary state. In viscoelastic TCF (Song et al. Reference Song, Teng, Liu, Ding, Lu and Khomami2019; Lopez Reference Lopez2022), angular momentum transport takes into account the contribution of polymer stress, and we rewrite
$J^\omega$
as follows for completeness:
Theoretically,
$J^\omega$
is a quantity independent of
$r$
, representing the conserved transverse current of azimuthal motion that transports
$\omega$
in the radial direction.
Numerical errors commonly lead to the violation of (A1) and the radial dependence of (A2) (Stevens, Verzicco & Lohse Reference Stevens, Verzicco and Lohse2010; Ostilla-Mónico et al. Reference Ostilla-Mónico, Stevens, Grossmann, Verzicco and Lohse2013, Reference Ostilla-Mónico, Huisman, Jannink, Van Gils, Verzicco, Grossmann, Sun and Lohse2014a
; Zhu et al. Reference Zhu, Ostilla-Mónico, Verzicco and Lohse2016). To this end, two quantities have been proposed in the following to evaluate the precision of the flow solution: (i)
$\varDelta _\varepsilon$
, measuring the relative difference between the two sides of (A1),
and (ii)
$\varDelta _J$
, measuring the radial variation of
$J^\omega$
,
As mentioned,
$\varDelta _\varepsilon$
and
$\varDelta _J$
are theoretically zero but will deviate when obtained by numerical simulations. In a Newtonian TCF, Ostilla-Mónico et al. (Reference Ostilla-Mónico, Stevens, Grossmann, Verzicco and Lohse2013) has demonstrated that reliable simulation results require sufficiently small values of
$\varDelta _\omega$
and
$\varDelta _J$
, typically less than
$1\,\%$
. However, the validity of these criteria in viscoelastic TCF remains unknown because additional elastic dissipation and polymer stress are at play. This will be the primary goal in the following grid resolution test.
To provide preliminary information for the examination of
$\varDelta _\varepsilon$
and
$\varDelta _J$
, we first conducted a grid convergence study using the parameter set corresponding to flows with the largest elastic effect, i.e.
$\beta =0.90, Wi=150$
. Given that the production grid resolution introduced in § 2.2 already involves a sufficiently large number of overall grid points, we implemented two coarser mesh sizes for test simulations:
$N_r\times N_\theta \times N_z =96\times 128 \times 256$
(mesh 1) and
$160\times 256\times 384$
(mesh 2). The resolution of the production grid,
$256\times 256\times 448$
, is denoted as mesh 3. All three simulations are performed using a time step
$\varDelta t =0.002$
. Considering that higher-order turbulent statistics are more difficult to converge on, we examined the root mean square (r.m.s.) values of
$\boldsymbol{u}$
and
$\boldsymbol{\tau }$
. As depicted in figure 17, both velocity and polymer stress fields show no significant qualitative differences with increasing grid resolution, and the sharp gradients of
$\boldsymbol{\tau }$
in the near-wall regions are faithfully captured (Dubief et al. Reference Dubief, Page, Kerswell, Terrapon and Steinberg2022; Lin et al. Reference Lin, Song, Liao, Liu, Lu and Khomami2024b
). Interestingly, the profiles of the r.m.s. values for the two finer grids collapse onto a single curve, which is particularly evident for the
$\tau '_{\theta \theta \ rms}$
profile. This shows that mesh 2 and mesh 3 represent spatially converged cases (Ostilla-Mónico et al. Reference Ostilla-Mónico, Verzicco and Lohse2015), thus serving as reliable references to calculate
$\varDelta _\varepsilon$
and
$\varDelta _J$
.
Profiles of r.m.s. values of (
$a$
) velocity components and (
$b$
) polymer stresses at
$\beta =0.90, Wi=150$
with various mesh sizes. The fluctuating part of the variable
$\phi$
is evaluated as
$\phi '=\phi -\langle \phi \rangle$
. Hereafter,
$\tilde {r}=(r-R_i)/d$
represents the dimensionless distance to the inner cylinder wall.

(
$a$
) Radial dependence of
$Nu_{\omega }(r)$
for three different grid resolutions in the simulations of
$\beta =0.90, Wi=150$
. The inset depicts the corresponding variations of
$\varDelta _J$
and
$\varDelta _{\varepsilon }$
as a function of grid resolutions. (
$b$
) The
$\varDelta _J$
for each pair of
$(\beta ,Wi)$
calculated by using mesh 3 (
$N_r\times N_{\theta } \times N_z = 256\times 256\times 448$
). The horizontal dashed line indicates a
$1\,\%$
error for reference.

The radial distribution of
$Nu_\omega$
shown in figure 18(
$a$
) confirms a visible radial dependence of the angular momentum flux in our simulations, especially for the under-resolved mesh 1 case. The behaviour of
$Nu_\omega$
is similar to that observed in a Newtonian TCF, where under-resolution leads to large oscillations in the near-wall regions. These oscillations, likely artefacts of unresolved boundary layer dynamics rather than a systematic bias of the solver (Ostilla-Mónico et al. Reference Ostilla-Mónico, Stevens, Grossmann, Verzicco and Lohse2013), can be suppressed with grid refinement. We demonstrated this by calculating
$\varDelta _J$
for various grid resolutions. As depicted in the inset of figure 18(
$a$
),
$\varDelta _J$
gradually decreases with increasing grid resolution, and a sufficiently small value (approximately
$\sim 1\,\%$
) is achieved with mesh 2, consistent with the grid convergence study depicted in figure 17. Hence, the convergence criterion
$\varDelta _J\leqslant 1\,\%$
can still be used safely for viscoelastic TCF, as the additional errors induced by the polymer stress field have been considered in the definition of
$\varDelta _J$
((A2) and (A4)). Similarly,
$\varDelta _\varepsilon$
exhibits a comparable convergence behaviour, reaching a sufficiently small value with mesh 2. These observations demonstrate that, in future studies, the proper grid resolution for viscoelastic TCF simulations can be guaranteed by examining
$\varDelta _\varepsilon$
and
$\varDelta _J$
, instead of performing successive grid refinement test simulations. In figure 18(
$b$
) we compute
$\varDelta _J$
for each pair of
$(\beta ,Wi)$
considered under the production grid resolution
$256\times 256\times 448$
. Evidently, the accuracy of our simulations is guaranteed by meeting the criterion
$\varDelta _J\leqslant 1\,\%$
(several cases have exceeded
$1\,\%$
, but very slightly).
An additional critical consideration in the simulation of viscoelastic turbulent flow is that insufficient grid resolution can introduce numerical diffusion into the polymer constitutive equation. This may trigger the so-called polymer diffusive instability (PDI), whose physical origin remains under debate (Beneitez, Page & Kerswell Reference Beneitez, Page and Kerswell2023, Reference Beneitez, Page, Dubief and Kerswell2024b
). We note that the flow dynamics discussed in this study do not suffer from PDI, based on the following two aspects: (i) the above extensive tests of grid resolution have demonstrated grid convergence, which can alleviate non-physical flow instability (Zhang et al. Reference Zhang, Cheng, Wang, Zhang, Li and Li2024); (ii) the PDI is relevant in two-dimensional planar viscoelastic TCF (Beneitez, Mrini & Kerswell Reference Beneitez, Mrini and Kerswell2025) and in three-dimensional TCF at low
$\beta \lt 0.8$
(Surya Phani Tej, Kumar Mohanty & Shankar Reference Surya Phani Tej, Kumar Mohanty and Shankar2025), whereas in the parameter regime considered here the dominant instability is associated with hoop stresses (Larson et al. Reference Larson, Shaqfeh and Muller1990; Datta et al. Reference Datta2022).
Appendix B. Budget equation for the streamwise enstrophy
The vorticity equation of an incompressible viscoelastic fluid can be written as
where
$\boldsymbol{\Omega} = \boldsymbol{\nabla } \times \boldsymbol{u}$
. The polymer stress tensor yields a supplementary contribution to the vorticity generation. Multiplying the equation of the
$\theta$
component of (B1) by
$\omega _\theta$
and performing the ensemble average, we obtain the budget equation for the streamwise enstrophy as
\begin{align} & \frac {1}{2}\frac {D\langle {\omega ^{2}_\theta }\rangle }{Dt} = {\underbrace {\left\langle {\omega _\theta \left(\frac {\partial f_r}{\partial z}-\frac {\partial f_z}{\partial r}\right)}\right\rangle }_{W_{\textit{p}}}} + \left\langle {\omega _{\theta }\frac {\beta }{\textit{Re}}\boldsymbol{\nabla} ^{2}\omega _{\theta }}\right\rangle \nonumber \\& \quad +\, {\underbrace {\left\langle {\omega ^{2}_{\theta}\left(\frac {u_r}{r}+\frac {1}{r}\frac {\partial u_{\theta }}{\partial \theta }\right)}\right\rangle - \left\langle {\omega _{\theta} \left(\frac {1}{r}\frac {\partial u_r}{\partial \theta }-\frac {u_{\theta }}{r}\right)\frac {\partial u_{\theta }}{\partial z}}\right \rangle + \left \langle {\omega _{\theta }\frac {1}{r}\frac {\partial u_z}{\partial \theta }\frac {\partial u_{\theta }}{\partial r}}\right \rangle }_{W_{\textit{c}}}}, \end{align}
where
$f_i = (1-\beta )(\partial \tau _{\textit{ik}}/\partial x_k)/Re$
denotes the force of the polymer body and
$W_{\!p}$
represents the correlation between the stream vorticity and the polymer-induced torque (Kim et al. Reference Kim, Li, Sureshkumar, Balachandar and Adrian2007; Zhu et al. Reference Zhu, Song, Lin, Liu, Lu and Khomami2022). Here
$W_c$
is the combined term of inertial production for streamwise enstrophy, comprising three distinct contributions that arise from the stretching, tilting and twisting of vortical structures.
Compensated one-dimensional spanwise TKE spectra of various ADM states for the power-law decaying exponents: (
$a$
)
$k_z^{-2.6}$
and (
$b$
)
$k_z^{-14/3}$
.

Appendix C. Examination of the scaling exponents in the TKE spectra
We demonstrate the validity of the
$k_z^{-2.6}$
decay in the ADM states across a range of
$\beta$
(see figure 9) by examining the compensated TKE spectra. As shown in figure 19, the spectra exhibit a clear plateau when compensated by
$k_z^{2.6}$
, whereas one only sees a narrow plateau when compensated by
$k_z^{14/3}$
. This indicates that our results are consistent with the experimental findings of Boulafentis et al. (Reference Boulafentis, Lacassagne, Cagney and Balabani2024), while also showing that the TKE spectra in viscoelastic TCF do not strictly follow the
$k_z^{-14/3}$
scaling commonly reported for EIT states in channel and pipe flows (Dubief et al. Reference Dubief, Terrapon and Soria2013; Wang et al. Reference Wang, Zhang, Wang, Li, Zhang and Li2023).
Appendix D. Characterisation of the shear-thinning behaviour in FENE-P fluids
Increasing polymer concentration results in shear thinning in real fluids. As our focus is on the ADM state transition induced by varying
$\beta$
, one might question the extent of shear thinning within the explored
$\beta$
range. Here, we demonstrate that the shear thinning is minor for the chosen
$L=100$
and the dilute
$\beta$
range. To this end, we have examined the rheological response of FENE-P fluids in simple shear flow (Purnode & Crochet Reference Purnode and Crochet1998; Ghanbari & Khomami Reference Ghanbari and Khomami2014; Yamani & McKinley Reference Yamani and McKinley2023). Specifically, for steady shear flow, the expression below depicts the relationship between shear viscosity and shear rate
$\dot {\gamma }$
:
\begin{equation} \eta _{shear} =\eta _s+\eta _p\left ( \frac {L^6}{4\lambda ^2\dot {\gamma }^2\left ( L^2-3 \right ) ^2} \right ) ^{1/3}\left ( \varDelta _{1}^{1/3}+\varDelta _{2}^{1/3} \right ). \end{equation}
Here
\begin{equation} \varDelta _1=1+\sqrt {1+\frac {2L^6}{27\lambda ^2\dot {\gamma }^2\left ( L^2-3 \right ) ^2}},\ \varDelta _2=1-\sqrt {1+\frac {2L^6}{27\lambda ^2\dot {\gamma }^2\left ( L^2-3 \right ) ^2}}. \end{equation}
For
$L=100$
, figure 20 shows the shear-thinning behaviour predicted by the FENE-P model. Even for the most concentrated polymer solution (
$\beta = 0.90$
) with the highest
$Wi_s = 150$
, the shear-thinning effect remains minimal, approximately
$0.95\eta _t$
(where
$\eta _t$
denotes the zero-shear solution viscosity). Therefore, the shear-thinning behaviour does not significantly impact the reported results.
Shear viscosity versus shear rate (defined as
$Wi_s=\lambda \dot {\gamma }$
) for a dilute solution (
$\beta =0.99\sim 0.90$
) of FENE-P dumbbells with
$L=100$
in simple shear flow. The vertical dashed line marks
$Wi_s=150$
for reference.

Appendix E. Derivation of the scale-decomposed transport equations of TKE
To derive the scale-decomposed transport equations of TKE, one can first consider the transport equations of large-scale (
$u^{\prime}_{i,L}$
) and small-scale (
$u^{\prime}_{i,S}$
) velocity fluctuations, which are obtained by filtering the governing equation of fluctuating velocity
$u^{\prime}_i$
(Kawata & Alfredsson Reference Kawata and Alfredsson2019; Kawata & Tsukahara Reference Kawata and Tsukahara2021). After choosing a filter scale, these equations are written as
\begin{align} \frac {\partial u^{\prime}_{i,L}}{\partial t}& +\langle u_k \rangle \frac {\partial u^{\prime}_{i,L}}{\partial x_k}+u^{\prime}_{k,L}\frac {\partial \left \langle u_i \right \rangle }{\partial x_k}+\left ( u^{\prime}_k\frac {\partial u^{\prime}_i}{\partial x_k} \right ) _L-\frac {\partial \left \langle u^{\prime}_iu^{\prime}_k \right \rangle }{\partial x_k}=-\frac {\partial p'_L}{\partial x_i}+\frac {\beta }{\textit{Re}}\frac {\partial ^2u^{\prime}_{i,L}}{\partial x_{k}^{2}} \nonumber\\ & +\, \frac {1-\beta }{\textit{Re}}\frac {\partial \tau '_{ik,L}}{\partial x_k}, \end{align}
\begin{align} \frac {\partial u^{\prime}_{i,S}}{\partial t} & +\langle u_k \rangle \frac {\partial u^{\prime}_{i,S}}{\partial x_k}+u^{\prime}_{k,S}\frac {\partial \left \langle u_i \right \rangle }{\partial x_k}+\left ( u^{\prime}_k\frac {\partial u^{\prime}_i}{\partial x_k} \right ) _S=-\frac {\partial p'_S}{\partial x_i}+\frac {\beta }{\textit{Re}}\frac {\partial ^2u^{\prime}_{i,S}}{\partial x_{k}^{2}} \nonumber\\ & +\, \frac {1-\beta }{\textit{Re}}\frac {\partial \tau '_{ik,S}}{\partial x_k}. \end{align}
The Reynolds stress term
$\partial \langle u^{\prime}_i u^{\prime}_j\rangle /\partial x_k$
appears in the transport equation of the large-scale velocity (E1) because the Reynolds stress is a mean quantity. Similarly to the derivation of the transport equation of the full TKE, and recalling that the cross-correlation between the large- and small-scale parts is zero for any combination of velocity components, we can obtain the scale-decomposed transport equations of TKE (3.3) and (3.4). For completeness, we rewrite them as follows:
Note that here the ensemble average has been performed. The physical meanings of each term have been interpreted in the main text. Moreover, the interscale transport term
$T_r$
has opposite signs in the large- and small-scale TKE budget equations, signifying the opposite direction of energy flux. It can be seen that the sum of (E3) and (E4) yields the transport equation of the full TKE. In cylindrical coordinates, the inertial production, interscale transport and elastic production terms on the right-hand side of (E3) are defined respectively as
\begin{align} T_r^L &= \left \langle u^{\prime}_{r,L}u^{\prime}_{r,L}\frac {\partial u_{r,S}^{\prime}}{\partial r}\right \rangle + \left \langle \frac {1}{r}u^{\prime}_{r,L}u_{\theta ,L}^{\prime}\frac {\partial u_{r,S}^{\prime}}{\partial \theta }\right \rangle + \left \langle u^{\prime}_{r,L}u_{z,L}^{\prime}\frac {\partial u_{r,S}^{\prime}}{\partial z} \right \rangle \notag \\ & - \left \langle u_{r,S}^{\prime}u_{r,S}^{\prime}\frac {\partial u^{\prime}_{r,L}}{\partial r}\right \rangle - \left\langle \frac {1}{r}u_{r,S}^{\prime}u_{\theta ,S}^{\prime}\frac {\partial u^{\prime}_{r,L}}{\partial \theta }\right \rangle - \left\langle u_{r,S}^{\prime}u_{z,S}^{\prime}\frac {\partial u^{\prime}_{r,L}}{\partial z}\right \rangle \notag \notag \\ &+ \left \langle u^{\prime}_{r,L}u_{\theta ,L}^{\prime}\frac {\partial u_{\theta ,S}^{\prime}}{\partial r}\right \rangle + \left \langle \frac {1}{r}u_{\theta ,L}^{\prime}u_{\theta ,L}^{\prime}\frac {\partial u_{\theta ,S}^{\prime}}{\partial \theta }\right \rangle + \left\langle u_{z,L}^{\prime}u_{\theta ,L}^{\prime}\frac {\partial u_{\theta ,S}^{\prime}}{\partial z}\right \rangle \notag \\ &- \left\langle u_{r,S}^{\prime}u_{\theta ,S}^{\prime}\frac {\partial u_{\theta ,L}^{\prime}}{\partial r}\right \rangle - \left \langle \frac {1}{r}u_{\theta ,S}^{\prime}u_{\theta ,S}^{\prime}\frac {\partial u_{\theta ,L}^{\prime}}{\partial \theta }\right \rangle - \left \langle u_{z,S}^{\prime}u_{\theta ,S}^{\prime}\frac {\partial u_{\theta ,L}^{\prime}}{\partial z}\right \rangle \notag \notag \\ &+ \left\langle u^{\prime}_{r,L}u_{z,L}^{\prime}\frac {\partial u_{z,S}^{\prime}}{\partial r}\right \rangle + \left \langle \frac {1}{r}u_{\theta ,L}^{\prime}u_{z,L}^{\prime}\frac {\partial u_{z,S}^{\prime}}{\partial \theta }\right \rangle + \left \langle u_{z,L}^{\prime}u_{z,L}^{\prime}\frac {\partial u_{z,S}^{\prime}}{\partial z} \right \rangle \notag \\ &- \left\langle u_{r,S}^{\prime}u_{z,S}^{\prime}\frac {\partial u_{z,L}^{\prime}}{\partial r} \right \rangle - \left \langle \frac {1}{r}u_{\theta ,S}^{\prime}u_{z,S}^{\prime}\frac {\partial u_{z,L}^{\prime}}{\partial \theta }\right \rangle - \left \langle u_{z,S}^{\prime}u_{z,S}^{\prime}\frac {\partial u_{z,L}^{\prime}}{\partial z} \right \rangle , \end{align}
\begin{align} P_{e}^{L}&=-\frac {1-\beta }{\textit{Re}}\bigg (\left \langle \tau _{rr,L}^{\prime}\frac {\partial u^{\prime}_{r,L}}{\partial r}\right \rangle + \left \langle \tau _{r\theta ,L}^{\prime} \left[ \frac {1}{r} \left(\frac {\partial u^{\prime}_{r,L}}{\partial \theta }-u_{\theta ,L}^{\prime} \right) +\frac {\partial u_{\theta ,L}^{\prime}}{\partial r} \right]\right \rangle \notag \\ & +\, \left \langle \tau _{rz,L}^{\prime} \left[ \frac {\partial u^{\prime}_{r,L}}{\partial z}+\frac {\partial u_{z,L}^{\prime}}{\partial r} \right]\right \rangle + \left \langle \tau _{\theta z,L}^{\prime} \left[ \frac {\partial u_{\theta ,L}^{\prime}}{\partial z}+\frac {1}{r}\frac {\partial u_{z,L}^{\prime}}{\partial \theta } \right]\right \rangle \notag \\ & + \, \left \langle \tau _{\theta \theta ,L}^{\prime} \left[ \frac {1}{r} \left(\frac {\partial u_{\theta ,L}^{\prime}}{\partial \theta }+u^{\prime}_{r,L} \right)\right]\right \rangle + \left\langle \tau _{zz,L}^{\prime}\frac {\partial u_{z,L}^{\prime}}{\partial z} \right\rangle \bigg ) . \end{align}
The other terms follow formulations analogous to the full TKE transport equation (Bilson & Bremhorst Reference Bilson and Bremhorst2007; Song et al. Reference Song, Lin, Liu, Lu and Khomami2021), but are not presented here for simplicity. The corresponding terms in (E4) are those with the subscript
$_L$
interchanged with
$_S$
. Interestingly,
$T_r$
has a form similar to the inertial production term
$P_t$
, that is, they are both products of the second moment of velocity fluctuations and velocity gradient. Hence, for the right-hand side of (E6), one can interpret that the terms that have a negative sign indicate the energy transfer from the larger to smaller scales, whereas the others represent the transfer in the other direction (Kawata & Alfredsson Reference Kawata and Alfredsson2018).
We follow the same procedure as Kawata & Tsukahara (Reference Kawata and Tsukahara2021) to evaluate the scale-by-scale terms shown in figure 16. Specifically, the filtered turbulent stresses
$\langle u^{\prime}_{i,L}u^{\prime}_{j,L}\rangle$
are related to their corresponding one-dimensional spanwise spectra as
$E_{\textit{ij}}=\partial \langle u^{\prime}_{i,L}u^{\prime}_{j,L}\rangle / \partial k_z =-\partial \langle u^{\prime}_{i,S}u^{\prime}_{j,S}\rangle / \partial k_z$
. Hence, the scale-by-scale transport equation of TKE is derived by differentiating (E3) with respect to
$k_z$
, i.e.
where the terms on the right-hand side are the
$k_z$
derivatives of the corresponding terms of (E3). To evaluate
$t_r$
, we use finite differentiation (more details can be found in Kawata & Tsukahara Reference Kawata and Tsukahara2021). On the other hand, since the averaged quantities are only functions of
$r$
in TCF, the scale-by-scale inertial production
$p_t$
can be evaluated as
where
$E_{r\theta }$
is the spectrum of Reynolds shear stress. Moreover, the elastic production term is expressed in the form of polymer stress–velocity gradient cospectra, i.e.
where
$T_{\textit{ij}}$
and
$S_{\textit{ij}}$
are the spectra of the polymer stress and the velocity gradient, respectively. In viscoelastic channel flow, this analysis has been used to examine the scales at which polymers gain energy from the flow and vice versa (Dubief et al. Reference Dubief, Page, Kerswell, Terrapon and Steinberg2022; Beneitez et al. Reference Beneitez, Page, Dubief and Kerswell2024a
).













































































































































































































