Abstract
Research within the past five years (e.g., References 1 to 5) identified a multitude of mechanisms whereby shock interactions can affect turbulence. These mechanisms include: (1) direct vorticity amplification, (2) production of vorticity from incident sound and entropy modes, (3) bulk compression and (4) shock-induced streamline curvature as “extra rates of strain,” (5) instantaneous shock focusing, and (6) direct effects of shock motion/dynamics/instability. The present paper addresses three facets of this last issue, the effects of shock motion upon turbulence/“unsteady vorticity.”
Research was supported by the National Aeronautics and Space Administration under NASA Contract No. NAS1-17170 while this author was in residence at ICASE, NASA Langley Research Center, Hampton, VA 23665. This work is declared to be a product of U.S. Government research and therefore in the public domain.
This is a preview of subscription content, log in via an institution to check access.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
Preview
Unable to display preview. Download preview PDF.
References
Delery, J.M.: Experimental investigation of turbulence properties in transonic shock/boundary layer interactions. AIAA J., Vol. 21 (1983), pp. 180–185.
Anyiwo, J.C. and D.M. Bushneil: Turbulence amplification in shock wave boundary layer interactions. AIAA J. Vol. 20 (1982), pp. 893–899.
Zang, T.A., M.Y. Hussaini, and D.M. Bushneil: Numerical computations of turbulence amplification in shock wave interactions. AIAA Paper No. 82-D293, AIAA 20th Aerospace Sciences Meeting, January 11–14, 1982, Orlando, Florida. Also AIAA J., Vol. 22 (1984), pp. 13–21.
Hayakawa, K., Smits, A.J., and Bogdonoff, S.M.: Hotwire investigation of an unseparated shock wave-turbulent boundary layer interaction. AIAA Paper No. 82-0985, 1982.
Parthasarathy, S.P., Harstad, K., and Massier, P.F.: Jet oscillations caused by vorticity interactions with shock waves. Presented at the AIAA 7th Aeroacoustics Conference, Octo’ber 5–7, 1981, Palo Alto, California. AIAA Paper No. 81–1974.
Jungowski, W.M.: Some self-induced supersonic flow oscillations. Progress Aerospace Sciences, Vol. 18, No. 1978, pp. 151–15.
Majda, Andrew: The stability of multi-dimensional shock fronts. Memoirs of the American Mathematical Society, Number 275. American Mathematical Society, January 1983, Vol. 41.
Plotkin, Kenneth J.: Shock wave oscillation driven by turbulent boundary-layer fluctuations. AIAA J., Vol. 13, August 1975, pp. 1036–1040.
Grande, E. and Oates, G.C.: Unsteady flow generated by shock-turbuelnt boundary layer interactions. Presented at the AIAA 11th Aerospace Sciences Meeting, Washington, D.C., January 10–12, 1973. AIAA Paper No. 73–168.
Whitham, G.B.: A new approach to problems of shock dynamics. Part 1 — Two-dimensional problems. J. Fluid Mech., Vol. 2, 1957, pp. 145–171.
Carrier, G.F.: The oscillating wedge in supersonic stream. J. Aero. Sci., Vol. 16, 1949, pp. 150–152.
Van Dyke, Milton D.: On supersonic flow past an oscillating wedge. Quart. Appl. Math., Vol. XI, No. 3, 1953, pp. 360–363.
Oh, Y. H.: Analysis of two-dimensional free turbulent mixing. Presented at the AIAA 7th Fluid and Plasma Dynamics Conference, Palo Alto, California, June 17–19, 1974. AIAA Paper No. 74–594.
Birch, Stanley F. and Eggers, James M.: A critical review of the experimental data for developed free turbulent shear layers. Free Turbulent Shear Flows, Vol. 1, Conference Proceedings, NASA SP-321, 1972.
Wagner, Richard D.: Mean flow and turbulence measurements in a mach 5 shear layer. Part II — Hot-wire measurements of the mean flow and turbulence intensities. Fluid Mechanics of Mixing ASME, 1973.
Morrisette, E. Leon and Birch, Stanley F.: Mean flow and turbulence measurements in a mach 5 shear layer. Part I — The development and spreading of the mean flow. Fluid Mechanics of Mixing ASME, 1973.
The 1980-81 AFOSR-HTTM-Stanford Conference on Complex Turbulent Flows: Comparison of Computation and Experiment, Vol. II, Taxonomies, Reporters’ Summaries, Evaluation, and Conclusions. Proceedings of the 1981 Conference, Stanford University, Stanford, California, September 14–18, 1981, pp. 814-836.
Dosanjh, D.S. and Hamernik, R.P.: Interaction of an advancing shock front with a concentrated heat (entropy) source. Phys. Fluids, Supp. I, 1969, pp. 1136–1139.
Picone, J. M., Oran, E. S., Boris, J. P., and Young Jr., T. R., Theory of vorticity generation by shock wave and flame interactions in Dynamics of Shock Waves, Explosions, and Detonations, J. R. Bowen, N. Manson, A. K. Oppenheim, and R. I. Soloukhin (eds.), Vol. 94, Progress in Astronautics and Areonautics.
Swan, G.W. and Fowles, G.R.: Shock wave stability. Phys. Fluids, Vol. 18, No. 1, January 1975, pp. 28–35.
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
Hussaini, M.Y., Collier, F., Bushnell, D.M. (1986). Turbulence Alteration due to Shock Motion. 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_29
Download citation
DOI: https://doi.org/10.1007/978-3-642-82770-9_29
Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-642-82772-3
Online ISBN: 978-3-642-82770-9
eBook Packages: Springer Book Archive