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The high-speed submerged hydrofoil

Published online by Cambridge University Press:  09 January 2023

J.S. Marshall*
Affiliation:
Department of Mathematics, University College London, London WC1E 6BT, UK
E.R. Johnson
Affiliation:
Department of Mathematics, University College London, London WC1E 6BT, UK
*
†Email address for correspondence: j.marshall@ucl.ac.uk

Abstract

This paper gives, in the limit of large Froude number, a closed-form, analytical solution for steady, two-dimensional, inviscid, free-surface attached flow over a submerged planar hydrofoil for arbitrary angles of attack and depths of submergence. The doubly connected flow domain is conformally mapped to a concentric annulus in an auxiliary plane. The complex flow potential and its derivative, the complex velocity, are obtained in the auxiliary plane by considering their form at known special points in the flow, and the required conformal mapping is determined by explicit integration. The four real solution parameters are determined as the simultaneous roots of four real nonlinear algebraic equations arising from the flow normalisation. The explicit form allows accurate evaluation of various flow quantities, including the lift on the foil, and these are related to the large-Froude-number results in recent numerical solutions.

Information

Type
JFM Papers
Creative Commons
Creative Common License - CCCreative Common License - BY
This is an Open Access article, distributed under the terms of the Creative Commons Attribution licence (http://creativecommons.org/licenses/by/4.0/), which permits unrestricted re-use, distribution and reproduction, provided the original article is properly cited.
Copyright
© The Author(s), 2023. Published by Cambridge University Press
Figure 0

Figure 1.Sketch of the flow domain $D$ for a free-surface flow past a submerged hydrofoil. Here, $\partial D_0$ denotes the free surface (in blue) while $\partial D_1$ denotes the hydrofoil (red). Also, $z_1=0$ and $z_2=\mathrm {e}^{\mathrm {i}\alpha }$ denote, respectively, the leading and trailing edges of the hydrofoil, so $-\alpha$ gives the angle of attack, and $z_3$ denotes a stagnation point – this lies on the leading face of the hydrofoil.

Figure 1

Figure 2.Sketch of the pre-image domain $D_{\zeta }$ for our conformal parametrisation of the flow domain $D$ as in figure 1. Here, $D$ is the image of $D_{\zeta }$ under a conformal map $z(\zeta )$.

Figure 2

Figure 3.The annuli appearing in the analysis: $D_{\zeta }^{-1}$ (light grey) is the reflection of the pre-image domain $D_{\zeta }$ (turquoise) of figure 2 in the unit circle $C_0$ (dotted blue). The union of $\overline {D_{\zeta }}$ and $D_{\zeta }^{-1}$ forms the fundamental region $F$ of (3.4) for the group $\varTheta$. The union of $\bar {F}$ and the reflection of $F$ (dark grey) in the circle $C_1$ (dotted red) forms the fundamental region $\hat {F}$ of (3.13) for the group $\hat {\varTheta }$. The complex velocity $W'(\zeta )$ has double poles (blue crosses) at $\zeta =-\mathrm {i}$ and $-\mathrm {i}q^2$, and simple zeros (blue circles) at $\zeta =\zeta _2$, $-\overline {\zeta _2}$, $1/\overline {\zeta _2}$ and $-1/\zeta _2$. The mapped complex velocity $\varOmega (\zeta )$ has simple poles (red crosses) at $\zeta =\zeta _1$ and $-1/\zeta _2$ (coinciding with a zero of $W'(\zeta )$), and simple zeros (red discs) at $\zeta =1/\overline {\zeta _1}$ and $-\overline {\zeta _2}$ (also coinciding with a zero of $W'(\zeta )$).

Figure 3

Figure 4.Illustrations of the solution components for a typical solution (namely, that which is illustrated in figure 6(b) below). Here, $\alpha =-{\rm \pi} /4$ and $y_c=0.3$ (see (3.51)). (a) Contours of $\mathrm {Im}\{W(\zeta )\}$ as given by (3.19), giving the flow streamlines in the pre-image domain $D_{\zeta }$ with a dipole at $\zeta =\mathrm {-i}$ (which corresponds to the point at infinity in $D$), stagnation points symmetrically at $\zeta =\zeta _2$ (the trailing edge in $D$) and $-\overline {\zeta _2}$ (on the leading face in $D$), and tangential flow along $C_0$ (the free surface in $D$) and $C_1$ (the foil). (b) Isotachs, contours of $|\varOmega (\zeta )|$ as given by (3.34), the flow speed mapped to the pre-image domain $D_{\zeta }$, with infinite speed at $\zeta _1$ (the leading edge in $D$), a single stagnation point at $\zeta =-\overline {\zeta _2}$ (on the leading face in $D$), and constant speed along $C_0$ (the free surface in $D$), with no stagnation point at $\zeta =\zeta _2$ (the trailing edge in $D$) where the speed is finite.

Figure 4

Figure 5.Free surface profiles (blue) for flow past a hydrofoil (red) for various angles of attack $-\alpha$ and leading-edge submergence $y_c$: (a) $\alpha =-{\rm \pi} /4$, $y_c=0.01, 0.05$ and $0.1, 0.2, 0.3,\dots$; and (b) $\alpha ={\rm \pi} /3$, $y_c=0.28, 0.8$ and $1.2, 1.4, 1.6, \ldots$. Lengths here and in subsequent figures are normalised on the length of the foil.

Figure 5

Figure 6.Streamlines (turquoise) for free-surface flow past a hydrofoil for various angles of attack $-\alpha$ and leading-edge submergence $y_c$: (a) $\alpha =-{\rm \pi} /4$, $y_c=1.5$; (b) $\alpha =-{\rm \pi} /4$, $y_c=0.3$; (c) $\alpha ={\rm \pi} /3$, $y_c=1.4$; and (d) $\alpha ={\rm \pi} /3$, $y_c=0.28$. (e) A detail of part (d) near the stagnation point.

Figure 6

Figure 7.The lift coefficient $C_L$ as a function of the leading-edge submergence $y_c$ for the angles of attack of figure 6: (a) ${\rm \pi} /4$ ($\alpha =-{\rm \pi} /4$); (b) $-{\rm \pi} /3$ ($\alpha ={\rm \pi} /3$). The dashed line gives the limiting value for $y_c\to \infty$ from (6.1).

Figure 7

Figure 8.(a) The lift coefficient $C_L$ as a function of the angle of attack $-\alpha$ for three depths $h$ of the midpoint of the hydrofoil. (b) The rate of change of $C_L$ with respect to angle of attack $-\alpha$ at $\alpha =0$, as a function of $h$. The dashed line gives the infinite depth asymptote $(\mathrm{d}C_L/\mathrm{d}(-\alpha))|_{\alpha=0}=2{\rm \pi}$ from (6.1).

Figure 8

Figure 9.(a) The pressure coefficient $C_p$ for a foil at angle of attack $5^{\circ }$ at selected depths $h$ of midpoint submergence as a function of distance $\hat {x}$ along the foil from the midpoint. The upper curves correspond to the lower side of the foil, and the lower curves correspond to the upper side. (b) The lift coefficient $C_L$ (yellow) as a function of the midpoint submergence $h$ compared with the values of $C_L$ in SW20 for flow past the NACA0012 hydrofoil at Froude numbers $ {\textit {Fr}}=5$ (blue) and $ {\textit {Fr}}=10$ (red). The dashed line gives the infinite depth asymptote from (6.1).