An experiment of two dimensional roughness effect on hypersonic boundary-layer transition

43rd AIAA Aerospace Sciences Meeting and Exhibit - Meeting Papers

Volumn , Issue , 2005, Pages 3419-3430

  Fujii, Keisuke ^a,b,c  

^a JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

^b Wind Tunnel Technology Center   (Japan)

^c AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; BOUNDARY LAYERS; NUMBER THEORY; SURFACE ROUGHNESS; WIND TUNNELS;

HYPERSONIC BOUNDARY LAYER; MACH NUMBER;

HYPERSONIC AERODYNAMICS;

EID: 30744469392     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2005-891     Document Type: Conference Paper

References (9)

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2. Berry, S., Bouslong, S., Brauckmann, G., and Caram, J., "Shuttle Oribter Experimental Boundary-Layer Transition Results with Isolated Roughness," Journal of Spacecraft and Rockets, Vol. 35, No. 5, 1998, pp. 241-248.
3. Berry, S., Auslender, A., Dilley, A., and Calleja, J., "Hypersonic Boundary-Layer Trip Development for Hyper-X," Journal of Spacecraft and Rockets, Vol. 38, No. 6, 2001, pp. 853-864.
4. Stetson, K., "Hypersonic Boundary-Layer Transition," Advances in Hypnrsonics: Volume I. Defining the Environment, edited by J. Bertin, J. Periaux, and J. Ballmann, Birkhäuser Boston, 1992, pp. 324-417.
5. van Driest, E. and Blumer, C., "Boundary-Layer Transition at Supersonic Speeds: Roughness Effects with Heat Transfer," AIAA Journal, Vol. 6, No. 4, 1968, pp. 603-607.
6. Schultz, D. and Jones, T., "Heat Transfer Measurements in Short Duration Hypersonic Facilities," Tech. Rep. AG-165, AGARD, 1973.
7. Mateer, G. and Larson, H., "Unusual Boundary-Layer Transition Results on Cones in Hypersonic Flow," AIAA Journal, Vol. 7, No. 4, 1969, pp. 660-664.
8. Stainback, P., "Some Effects of Roughness and Variable. Entropy on Transition at a Mach Number of 8," 1967.
9. Saric, W., Carrillo, R., and Reibert, M., "Leading-Edge Roughness as a Transition Control Mechanism," AIAA Paper 98-0781, 1998.