Problems in high speed flow prediction relevant to control

2nd AIAA, Theoretical Fluid Mechanics Meeting

Volumn , Issue , 1998, Pages

  Malmuth, N ^a,b,c,d   Fedorov, A ^a,b,c,d   Shalaev, V ^a,b,c,d   Cole, J ^a,b,c,d   Khokhlov, A ^a,b,c,d   Hites, M ^a,b,c,d   Williams, D ^a,b,c,d  

^a ROCKWELL SCIENCE CENTER   (United States)

^b MOSCOW INSTITUTE OF PHYSICS AND TECHNOLOGY   (Russian Federation)

^c RENSSELAER POLYTECHNIC INSTITUTE   (United States)

^d ILLINOIS INSTITUTE OF TECHNOLOGY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYERS; FLOW CONTROL; FLUID MECHANICS; HYPERSONIC FLOW;

BOUNDARY LAYER TRANSITIONS; COMPUTATIONAL MODEL; DROP EXPERIMENTS; FLOW STABILIZATION; HIGH SPEED FLOWS; SEMI-TRANSPARENT; STORE SEPARATION; VELOCITY PROFILES;

SHEAR FLOW;

EID: 84884802983     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (13)

1. Bush, W.B., "Hypersonic Strong Interaction Similarity Solutions for Flow Over a Flat Plate," J. Fluid Mech. 251, pp. 51-64, 1966.
2. Cheng, H.K., Hall, J.G., Golian, T.C., and Hertzberg, A., "Boundary Layer Displacement and Leading Edge Bluntness Effects in High- Temperature Hypersonic Flow," J. Aerospace Sciences, 28, pp. 353 - 410, 1961.
3. Cole, J.D., "Newtonian Flow Over Slender Bodies,"J. Aero Sciences, pp. 448 - 455 June, 1957.
4. Lee, R. and Cheng, H.K., "On the Outer Edge Problem of a Hypersonic Boundary Layer," J. Fluid Mech. 38 l, pp. 161 - 179, 1969.
5. Lees, L., "On the Boundary Layer Equations of Hypersonic Flow and Their Approximate Solutions," J. Aero. Sciences, pp. 143 - 145, 1953.
6. Malmuth, N.D., "Inviscid Instability of Hypersonic Strong Interaction Flow Over a Flat Plate," Instability, Transition and Turbulence, M.Y. Hussaini, A. Kumar, and C.L. Street, eds., Springer-Verlag, pp. 107 - 126, 1992.
7. Malmuth, N.D., "Stability of the Inviscid Shock Layer in Strong Interaction Flow Over a Hypersonic Flat Plate," in Instabilities and Turbulence in Engineering Flows, D.E. Ashpis, T.B. Gatski, and R. Hirsh, eds., Kluwer, pp. 189 - 224, 1993.
8. Stewartson, K., The Theory of Laminar Boundary Layers in Compressible Flow, Oxford, London, 1964.
9. Van Dyke, M.D., "A Study of Hypersonic Small Disturbance Theory," NACA TN 3173, May, 1954.
10. Mack, L.M., "Boundary Layer Linear Stability Theory," AGARD Rep. No. 709, pp. 3-81,1984.
11. Anyiwo, J.C., and Bushnell, D.M., "Turbulence Amplification in Shock Wave/Boundary Layer Interaction," AIAA Journal 20, p. 893, 1982
12. Meadows, K.R., Kumar, A., and Hussaini, M.Y., "A Computational Study on the Interaction Between a Vortex and a Shock Wave," AIAA Journal 29, p. 174, 1991.
13. Hayes, W.D., and Probstein, R.F., Hypersonic Flow Theory, Academic Press, N.Y, 1959.