Boundary layer transition experiments in support of the hypersonics program

Collection of Technical Papers - 39th AIAA Thermophysics Conference

Volumn 2, Issue , 2007, Pages 957-970

  Berry, Scott A ^a,c,d   Chen, Fang Jenq ^a,d,e   Wilder, Michael C ^b,d,f   Reda, Daniel C ^b,d,g  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b NASA AMES RESEARCH CENTER   (United States)

^c Aerothermodynamics Branch

^d AIAA   (United States)

^e Flow Physics and Control Branch   (United States)

^f Reacting Flow Environments Branch   (United States)

^g MS 229 3 ^*  (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BALLISTIC RANGE EFFORT; BOUNDARY LAYER TRANSITION; HIGH-SPEED FLOWS; HYBOLT FLIGHT;

BALLISTICS; COMPUTER SIMULATION; DATA FLOW ANALYSIS; DATABASE SYSTEMS; HYPERSONIC FLOW;

BOUNDARY LAYERS;

EID: 35748962009     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (20)

1. th Annual AIAA Aerospace Sciences Meeting, Jan. 2007.
2. Mansour, N., Pittman, J., and Olsen, L., "Fundamental Aeronautics Hypersonics Project at NASA: Overview," AIAA Paper 2007-4263, June 2007.
3. Salas, M. D., "A Review of Hypersonics Aerodynamics, Aerothermodynammics, and Plasmadynamics Activities Within NASA's Fundamental Aeronautics Program," AIAA Paper 2007-4264, June 2007.
4. Wurster, K. E., Riley, C. J., and Zoby, E. V., "Engineering Aerothermal Analysis for X-34 Thermal Protection System Design," Journal of Spacecraft and Rockets, Vol.36, No.2, March-April 1999, pp. 216-228.
5. Reshotko, E., "Boundary Layer Stability and Transition," Annual Review of Fluid Mechanics, Vol. 8, pp. 311-349, 1976.
6. Malik, M. R., Li, F., Choudhari, M. M., and Chang, C. L., "Secondary instability of crossflow vortices and swept-wing boundary-layer transition", J. Fluid Mechanics, Vol. 399, pp. 85-115, 1999.
7. Malik, M. R., "Prediction and Control of Transition in Supersonic and Hypersonic Boundary Layers," AIAA Journal, Vol. 27, No. 11, pp. 1487-1493, 1989.
8. Reshotko, E., "Transition Issues for Atmospheric Entry," AIAA Paper 2007-0304, Jan. 2007.
9. Berry, S. A., Horvath, T. J., Greene, F. A., Kinder, G. R., and Wang, K. C, "Overview of Boundary Layer Transition Research in Support of Orbiter Return To Flight," AIAA-2006-2918, June 2006.
10. Campbell, C., Anderson, B., Bourland, G., Bouslog, S., Cassady, A., Horvath, T., Berry, S., Gnoffo, P., Wood, B., Reuther, J., Driver, D., Chao, D., and Picetti, D., "Orbiter Return To Flight Entry Aeroheating," AIAA-2006-2917, June 2006.
11. Greene, F. A., and Hamilton, H., "Development of a Boundary Layer Properties Interpolation Tool in Support of Orbiter Return-To-Flight," AIAA-2006-2920, June 2006.
12. McGinley, C., Berry, S. A., Kinder, G. R., Barnwell, M., Wang, K. C., and Kirk, B. S., "Review of Orbiter Flight Boundary Layer Transition Data," AIAA-2006-2921, June 2006.
13. Berry, S. A., Horvath, T. J., Cassady, A. M., Kirk, B. S., Wang, K.C., and Hyatt, A. J., "Boundary Layer Transition Results From STS-114," AIAA-2006-2922, June 2006.
14. N Code for Three-Dimensional Flow over Finite-Swept Wings," High Technology report No. HTC-9502 (version 2), April 1995.
15. Horvath, T. J., Berry, S. A., Merski, N. R., Berger, K T., Liechty, D. S., Buck, G. M., and Schneider, S. P., "Shuttle Damage/Repair From the Perspective of Hypersonic Boundary Layer Transition - Experimental Results," AIAA-2006-2918, June 2006.
16. Strawa, A.W., Chapman, G.T., Canning, T.N., and Arnold, J.O., "The Ballistic Range and Aerothermodynamic Testing," AIAA 88-2015, 15th Aerodynamic Testing Conference, San Diego, CA, May 18-20, 1988.
17. th AIAA Thermophysics Conference, June 25-28, 2007.
18. Reda, D. C., "Review and Synthesis of Roughness-Dominated Transition Correlations for Reentry Applications," Journal of Spacecraft and Rockets, Vol. 39, No. 2, March-April 2002, pp. 161-167.
19. Reda, D. C., Wilder, M. C., Bogdanoff, D. W, and Prabhu, D., "Transition Experiments on Blunt Bodies with Distributed Roughness in Hypersonic Free Flight," AIAA 2007-306, 45th AIAA Aerospace Sciences Meeting and Exhibit Jan. 8-11, 2007.
20. Hill, P. R., Adamson, D., Foland, D. H., and Bressette, W. E., "High-temperature oxidation and ignition of metals," NACA-RM-L55L23b, March 26, 1956.