On the impact of injection schemes on transition in hypersonic boundary layers

16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference

Volumn , Issue , 2009, Pages

  Leyva, Ivett A ^a   Jewell, Joseph S ^b   Laurence, Stuart ^b,c   Hornung, Hans G ^b   Shepherd, Joseph E ^b  

^a AIR FORCE RESEARCH LABORATORY   (United States)

^b CALIFORNIA INSTITUTE OF TECHNOLOGY   (United States)

^c GERMAN AEROSPACE CENTER DLR   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

CALTECH; FREESTREAM CONDITIONS; HOLE INJECTORS; INJECTION FLOW; INJECTION HOLES; INJECTION SCHEMES; LENGTH TO DIAMETER RATIO; REFLECTED SHOCKS; TRANSITION REYNOLDS NUMBER; TURBULENT HEAT TRANSFER;

GEOMETRY; HYDRAULICS; JET PUMPS; REYNOLDS NUMBER;

HYPERSONIC BOUNDARY LAYERS;

EID: 77958526973     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (14)

1. Berry, S. A., Nowak, R. J., Horvath, T. J., "Boundary Layer Control for Hypersonic Airbreathing Vehicles", AIAA 2004-2246.
2. Bathel, B.F., Danehy, P.M., Inman J.A., Alderfer, D.W., Berry, S.A., "PLIF Visualization of Active Control of Hypersonic Boundary Layers Using Blowing", AIAA 2008-4266.
3. Danehy, P.M., Garcia, A. P., Borg, S., Dyakonov, A.A., Berry, S.A., (Wilkes) Inman, J.A., Alderfer, D.W., "Fluorescence Visualization of Hypersonic Flow Past Triangular and Rectangular Boundary-Layer Trips", AIAA 2007-536.
4. Berry, S.A., Auslender, A.H., Dilley, A.D., Calleja, J.F., "Hypersonic Boundary Layer Development for Hyper-X", J. Spacecraft and Rockets, Vol. 38, No. 6, pp. 853-864, 2001.
5. Holden, M.S., Mundy, E.P., Wadhams, T.P., "A Review of Experimental Studies of Surface Roughness and Blowing on the Heat Transfer and Skin Friction to Nosetips and Slender Cones in High Mach Number Flows", AIAA 2008-3907.
6. Korkegi, R., H., "Transition Studies and Skin-Friction Measurements on an Insulated Flat Plate at a Mach Number of 5.8", J. of the Aeronautical Sciences, Vol. 23, No. 2, February 1956.
7. Coles, D., "Measurements of Turbulent Friction on a Smooth Flat Plate in Supersonic Flow", J. of the Aeronautical Sciences, Vol. 21, No. 7, July 1954.
8. Germain, P., "The Boundary Layer on a Sharp Cone in High-Enthalpy Flow", GALCIT, Caltech, Ph.D. thesis, 1994.
9. Leyva, I.A., Laurence, S. War-Kei Beierholm A., Hornung H.G., Wagnild R., Candler, G., "Transition delay in hypervelocity boundary layers by means of CO2/acoustic instability interactions", AIAA 2009-1287.
10. Hornung, H., Belanger, J., "Role and techniques of ground testing simulation of flows up to orbital speeds", AIAA 90-1377.
11. Hornung, H., "Performance data of the new free-piston shock tunnel at GALCIT", AIAA 92-3943.
12. Sanderson, S., "Shock Wave Interaction in Hypervelocity Flow", GALCIT, Caltech, Ph.D. thesis, 1995.
13. Rowley. C. W., Colonius, T., Basu, A. J., "On self-sustained oscillations in two-dimensional compressible flow over rectangular cavities", J. Fluid Mech., Vol. 455, pp. 315-346, 2002.
14. http://www.mottcorp.com/sitemap/sitemap.htm.