Boundary layer transition results from STS-114

Collection of Technical Papers - 9th AIAA/ASME Joint Thermophysics and Heat Transfer Conference Proceedings

Volumn 1, Issue , 2006, Pages 177-189

  Berry, Scott A ^a,d   Horvath, Thomas J ^a,d   Cassady, Amy M ^b,e   Kirk, Benjamin S ^b,e   Wang, K C ^c,f   Hyatt, Andrew J ^c,f  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b NASA JOHNSON SPACE CENTER   (United States)

^c BOEING COMPANY   (United States)

^d Research and Technology Directorate   (United States)

^e CFD Branch

^f Orbiter Aeroheating ^*

Author keywords

[No Author keywords available]

Indexed keywords

AEROTHERMODYNAMIC ENVIRONMENT; THERMAL PROTECTION SYSTEMS;

COMPUTATION THEORY; REPAIR; SPACE RESEARCH; SPACE SHUTTLES; STRESS ANALYSIS; THERMAL STRESS;

BOUNDARY LAYERS;

EID: 33845595923     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (12)

1. Columbia Accident Investigation Board Final Reports, Vols. I-VI [online resource], URL: http://caib.nasa.gov/ [cited Aug and Oct 2003].
2. Campbell, C. H., Bourland, G., Bouslog, S. A., Horvath, T. J., Berry, S. A., Gnoffo, P. A., Reuther, J., Chao, D., Anderson, B., and Picetti, D., "Orbiter Return-To-Flight Entry Aeroheating," AIAA Paper-2006-2917, June 2006.
3. Berry, S. A., Horvath, T. J., Greene, F, Kinder, G., and Wang, K. C., "Overview of Boundary Layer Transition Research in Support of Orbiter Return to Flight," AIAA Paper-2006-2918, June 2006.
4. Horvath, T. J., Berry, S. A., Merski, N. R., Berger, K. T., Liechty, D. S., and Schneider, S. P., "Disposition of Shuttle Thermal Protection System Damage / Repair From the Perspective of Hypersonic Boundary Layer Transition," AIAA Paper-2006-2919, June 2006.
5. Greene, F., and Hamilton, H., "Development of a Boundary Layer Properties Interpolation Tool in Support of Orbiter Return-To-Flight," AIAA Paper-2006-2920, June 2006.
6. McGinley, C., Berry, S. A., Kinder, G., Barnwell, M., and Wang, K. C., "Review of Orbiter Flight Boundary Layer Transition Data," AIAA Paper-2006-2921, June 2006.
7. Haney, J. W., "Orbiter (Pre STS-1) Aeroheating Design Data Base Development Methodology: Comparison of Wind Tunnel and Flight Test Data," NASA CP-3248, Orbiter Experiments (OEX) Aerothermodynamics Symposium, April 1995, pp. 607-675.
8. Green, M. J., Budnick, M. P., Yang, L., and Chiasson, M. P., "Supporting Flight Data Analysis for Space Shuttle Orbiter Experiments at NASA Ames Research Center," AIAA Paper 83-1532, June 1983.
9. Blanchard, R. C., Wilmoth, R. C., Glass, C. E., Merski, N. R., Berry, S. A., Bozung, T. J., Tietjen, A., Wendt, J., Dawson, D., "Infrared Sensing Aeroheating Flight Experiment: STS-96 Flight Results," Journal of Spacecraft and Rockets, Vol. 38, No. 4, 2001, pp. 465-472.
10. Blanchard, R. C., Anderson, B. P., Welch, S. S., Glass, C. E., Berry, S. A., Merski, N. R., Banks, D. W., Tietjen, A., Lovern, M., "Shuttle Orbiter Fuselage Global Temperature Measurements from Infrared Images at Hypersonic Speeds," AIAA Paper 2002-4702, Aug. 2002.
11. Berry, S. A.; Merski, N. R.; and Blanchard, R. C.: "Wind Tunnel Measurements of Shuttle Orbiter Global Heating With Comparison to Flight," AIAA Paper 2002-4701, Aug. 2002.
12. Smolinski, G. J., Hubner, J. P., and Holden, M. S., "Risk Mitigation Study for Instrumentation Layout Along Wing Leading Edge of a 1.8%-Scale Space Shuttle Model Using TSP," AIAA 2005-478, Jan. 2005.