Summary
A combined experimental and computational investigation of an axisymmetric turbulent shock-wave boundary-layer interaction flow is presented. Experimental measurements include both mean and fluctuating data obtained by LDV techniques and identify large scale unsteady motions associated with shock induced separation. Computations using the compressible Navier-Stokes equations, and a two-equation turbulence model are in relatively good agreement with experimental measurements. It is found that the large scale unsteady motions do not appear to have a critical impact on the ability to compute the mean properties of the flows investigated in this paper.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
Preview
Unable to display preview. Download preview PDF.
Similar content being viewed by others
References
Ardonceau, P.L.: The structure of turbulence in a supersonic shock wave/boundary layer interaction. AIAA Journal, Vol. 22, (1984) 1254–1262.
Settles, G.S.; Fitzpatrick, T.J.; and Bogdonoff, S.M.: Detailed study of attached and separated compression corner flow fields in high Reynolds number supersonic flow. AIAA Journal, Vol. 17 (1975) 573–585.
Dussauge, J.P.; Gaviglio, J.: Bulk dilatation effects on Reynolds stresses in the rapid expansion of a turbulent boundary layer at supersonic speeds. Third Symposium on Turbulent Shear Flows. Univ. of Calif., Davis, California, (1981).
Dolling, D.S.; Or, C.T.: Unsteadiness of the shock wave structure in attached and separated compression ramp flow fields. AIAA Paper 83–1715 (1983).
Marvin, J.G.: Turbulence modeling for computational aerodynamics. AIAA Journal, Vol. 21, No. 7, pp. 941–955 (1983).
Dunnagan, S.E.; Brown, J.L.; Miles, J. B.: A holographic interferometric study of an axisymmetric shock-wave boundary-layer strong interaction flow. AIAA Paper 85–1564 (1985).
Brown, J. L.; Viswanath, P. R.: An experimental study of a supercritical trailing-edge flow. AIAA Paper 84–2187 (1984).
Coakley, T. J.: A compressible Navier-Stokes code for turbulent flow modeling. NASA TM 85899 (1984).
Coakley, T. J.; Hsieh, T.: A comparison between implicit and hybrid methods for the calculation of steady and unsteady inlet flows. AIAA Paper 85–1125 (1985).
Author information
Authors and Affiliations
Editor information
Editors and Affiliations
Rights and permissions
Copyright information
© 1986 Springer-Verlag Berlin, Heidelberg
About this paper
Cite this paper
Brown, J.L., Kussoy, M.I., Coakley, T.J. (1986). Turbulent Properties of Axisymmetric Shock-Wave/Boundary-Layer Interaction Flows. In: Délery, J. (eds) Turbulent Shear-Layer/Shock-Wave Interactions. International Union of Theoretical and Applied Mechanics. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-82770-9_12
Download citation
DOI: https://doi.org/10.1007/978-3-642-82770-9_12
Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-642-82772-3
Online ISBN: 978-3-642-82770-9
eBook Packages: Springer Book Archive