HIFiRE-1 boundary layer transition experiment design

Collection of Technical Papers - 45th AIAA Aerospace Sciences Meeting

Volumn 9, Issue , 2007, Pages 6450-6462

  Kimmel, Roger L ^a   Adamczak, David ^a   Gaitonde, Datta ^a   Rougeux, Albert ^a   Hayes, James R ^a  

^a AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

FLIGHT DYNAMICS; HYPERSONIC AERODYNAMICS; SPACECRAFT INSTRUMENTS; TEMPERATURE MEASUREMENT; TRANSDUCERS;

BOUNDARY LAYER TRANSITION; INSTRUMENTATION PERFORMANCE; PAYLOADS;

BOUNDARY LAYERS;

EID: 34250863288     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2007-534     Document Type: Conference Paper

References (19)

1. Schneider, S. P., "Flight Data for Boundary-Layer Transition at Hypersonic and Supersonic Speeds," Journal of Spacecraft and Rockets, vol. 36, no. 1, January-February 1999.
2. Stetson, K. F., and Kimmel, R. L., "On Hypersonic Boundary-Layer Stability," AIAA-92-0737, January 1992.
3. Kontis, K. and Stollery, J. L., "Incipient separation on flared bodies at hypersonic speeds," The Aeronautical Journal, vol. 103, no. 1027, September 1999, pp. 405-414.
4. Smart, M. K., Hass, N. E., and Paull, A., "Flight Data Analysis of the HyShot 2 Scramjet Flight Experiment," AIAA Journal, vol. 44, no. 10, October 2006.
5. Mack, L. M., "Boundary-Layer Stability Theory," Special Course on Stability and Transition of Laminar Flow, edited by R. Michel, AGARD Report No. 709, pp. 3-1 to 3-81, 1984.
6. Stetson, K. F., "Nosetip Bluntntess Effects on Cone Frustum Boundary-layer Transition in Hypersonic Flow," AIAA paper 83-1763, July 1983.
7. Stetson, K. F., Thompson, E. R., Donaldson, J. C., and Siler, L. G., "Laminar Boundary Layer Stability Experiments on a Cone at Mach 8, Part 2: Blunt Cone" AIAA paper 84-0006, January 1984.
8. Holden, M., and Wadham, T., Calspan University of Buffalo Research Center, personal communication.
9. Bertin, J. J., Stetson, K. F., "The Effect of Surface Roughness on Shuttle Orbiter Boundary-Layer Transition," NASA report JSC-27358, January 1996.
10. Johnson, H. B., and Candler, G. V., "Hypersonic Boundary Layer Stability Analysis Using PSE-Chem," AIAA paper 2005-5023, June 2005.
11. Reda, D. C., "Roughness-Dominated Transition on Nosetips, Attachment Lines and Lifting-Entry Vehicles," AIAA paper 2001-0205, January 2001.
12. Boudreau, A. H. "Correlation of Artificially Induced Boundary-Layer Transition Data at Hypersonic Speeds," AIAA Journal of Spacecraft, vol. 18, no. 2, March- April 1981.
13. Stetson, K. F., "Nosetip Bluntntess Effects on Cone Frustum Boundary Layer Transition in Hypersonic Flow," AIAA paper 83-1763, July 1983.
14. Schneider, S. P., "Design of a Mach-6 Quiet-Flow Wind-Tunnel Nozzle using the e**N Method for Transition Estimation," AIAA paper 1998-0547.
15. Beckwith, I. E., Chen, F.-J., and Malik, M. R., "Design and Fabrication Requirements for Low Noise Supersonic / Hypersonic Wind-Tunnels," AIAA paper 1988-0143, January 1988.
16. Beckwith, I., Chen, F.., Wilkinson, S. Malik, M. and Tuttle, D., "Design and Operational Features of Low-Disturbance Wind Tunnels at NASA Langley for Mach Numbers from 3.5 to 18," AIAA paper 1990-1391, June 1990.
17. Schneider, S. P., private communication, 2 June 2006.
18. Beckwith, I. E., Chen, F.-J., and Creel, Jr., T. R., "Design Requirements for the NASA Langley Supersonic Low-Disturbance Wind Tunnel," AIAA paper 86-0763, March 1986.
19. Berry, S. A., Bouslog, S. A., Brauckmann, G. J., and Caram, J. M., "Shuttle Orbiter Experimental Boundary-Layer Transition Results with Isolated Roughness," AIAA journal of Spacecraft and Rockets, vol. 35, no. 3, May-June 1998, pp. 241-248.