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Supersonic flow over three dimensional cavities

Published online by Cambridge University Press:  27 January 2016

R. Das and
J. Kurian
J. Kurian*
Affiliation:
Indian Institute of Technology, Madras, Chennai, India
*
kurian@iitm.ac.in
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Abstract

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This work presents a study of acoustic oscillations generated and the wave structure associated with supersonic flow past wall mounted 3D open cavities of varying length-to-width (L/W) ratio. Experiments were conducted to investigate the acoustic signature generated by the cavities at freestream Mach number of 1·7. The effect of L/W ratio of the cavity on the dominant modes of the acoustic signature registered on different walls of the cavities is investigated for an L/W range of 0·83-4. Shift in the dominant acoustic mode is observed as L/W ratio changes from 3 to 4. Statistical analysis of pressure data showed existence of acoustic waves and spreading of acoustic energy over different modes with change in cavity width. Time averaged schlieren visualisation indicated variation of shock and shear layer structure in the mainstream for the different cavities. Acoustic waves generated by the presence of the cavity and the dynamic behaviour of the shear layer were observed during instantaneous shadowgraph visualisation. Numerical simulation was done to make a prior assessment of the flow structure and the results are in good agreement with those from experiments. Ratio of mass exchange between cavity and mainflow and the cavity volume was observed to have profound effect on the magnitude of pressure oscillations generated by the cavities.

Information

Type
Research Article
Information
The Aeronautical Journal , Volume 117 , Issue 1188 , February 2013, pp. 175 - 192
Copyright
Copyright © Royal Aeronautical Society 2013 

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