PIV experiments on a rough-wall hypersonic turbulent boundary layer

40th AIAA Fluid Dynamics Conference

Volumn , Issue , 2010, Pages

  Sahoo, Dipankar ^a   Papageorge, Michael ^a   Smits, Alexander J ^a  

^a PRINCETON UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPRESSIBILITY EFFECTS; DIFFERENT HEIGHTS; FLAT PLATE; HIGH MACH NUMBER; LOW REYNOLDS NUMBER; MEAN VELOCITY PROFILES; MESH ELEMENTS; PARTICLE IMAGE VELOCIMETRIES; REYNOLDS SHEAR STRESS; ROUGHNESS DENSITY; ROUGHNESS ELEMENTS; SIZE AND SHAPE; SQUARE BAR; TURBULENT BOUNDARY LAYERS; VELOCITY PROFILES;

ATMOSPHERIC THERMODYNAMICS; BOUNDARY CONDITIONS; FLOW VISUALIZATION; FLUID DYNAMICS; HYPERSONIC AERODYNAMICS; HYPERSONIC VEHICLES; MACH NUMBER; QUAY WALLS; REYNOLDS NUMBER; SURFACE PROPERTIES; SURFACE ROUGHNESS; TURBULENCE; VELOCITY MEASUREMENT;

HYPERSONIC BOUNDARY LAYERS;

EID: 78649484664     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (20)

1. Berg, D. E. 1977. Surface roughness effects on the hypersonic turbulent boundary layer. Ph.D. Thesis, Calif. Inst. Technol., Pasadena (Univ. Microfilms 77-17260)
2. Baumgartner, M.L. 1997. Turbulence Structure in a Hypersonic Boundary Layer. Ph.D. Thesis, Princeton University.
3. Etz, M.R. 1998. The Effects of Transverse Sonic Gas Injection on a Hypersonic Boundary Layer. MSE Thesis, Princeton University.
4. Ekoto, I.W., Bowersox, R., Beutner, T., and Goss, L. 2008. Supersonic boundary layers with periodic surface roughness. AIAA Journal. 46(2), 486-497, 2008
5. Humble, R.A. 2009. Unsteady Flow Organization of a Shock Wave/Boundary Layer Interaction. Ph.D. Thesis, Delft University, The Netherlands.
6. Magruder, T.D. 1997. An Experimental Study of Shock/Shock and Shock/Boundary Layer Interactions on Double-Cone Geometries in Hypersonic Flow. MSE Thesis, Princeton University.
7. McGinley, C.B., Spina, E.F. and Sheplak, M. 1994 Turbulence measurements in a Mach 11 helium turbulent boundary layer. AIAA Paper 94-2364.
8. Mikulla, V. and Horstman, C. C. 1976. Turbulence measurements in hypersonic shock-wave boundary-layer interaction flows. AIAA J., 14(5) 568-575.
9. Morkovin, M. 1961. Effects of compressibility on turbulent flows. International Symposium on the mechanics of turbulence, Paris.
10. Perry, A.E. and Joubert, P.N. 1963. Rough wall boundary layers in adverse pressure gradients. Journal of Fluid Mechanics, 17, 193-211, 1963.
11. Perry, A.E., Schofield, W.H., and Joubert, P.N. 1969. Rough wall turbulent boundary layers. Journal of Fluid Mechanics, 37, 383, 1969.
12. Owen, F. K. and Horstman, C. C. 1972. On the structure of hypersonic turbulent boundary layers. J. Fluid Mech., 53 611-636.
13. Owen, F. K. and Horstman, C. C. 1972. Turbulent properties of a compressible boundary layer. AIAA J, 10(1) 1418-1424.
14. Owen, F. K., Horstman, C. C. and Kussoy, M. I. 1975. Mean and fluctuating flow measurements on a fully-developed non-adiabatic hypersonic boundary layer. J. Fluid Mech., 70 393 - 413.
15. Sahoo, D., Ringuette, M.J., and Smits, A.J. 2009. Experimental investigation of a hypersonic turbulent boundary layer. AIAA Paper, 2009-0780.
16. Sahoo, D., Schultze, M., and Smits, A.J. 2009. Effects of roughness on a turbulent boundary layer in hypersonic flow. AIAA Paper, 2009-3678.
17. Schultze, M. 2009. Experiments on roughness in hypersonic boundary layers at a DNS accessible Reynolds number. MSE Thesis, University of Stuttgart, 2009.
18. Smits A. J. and Dussauge J.-P. 2005 Turbulent Shear Layers In Supersonic Flow. Springer-Verlag New York Inc., 2005.
19. Spina, E.F., Smits, A.J. and Robinson, S.K. 1994. The physics of supersonic turbulent boundary layers. Annual Review of Fluid Mechanics, 26, 287-319, 1994.
20. Van Driest, E.R. 1951. Turbulent boundary layer in compressible fluids. J. of Aeronautical Science, 18(3), 145-160, March 1951.