Boundary Layer Transition Results from STS-114
Author:
Affiliation:
1. NASA Langley Research Center
2. NASA Johnson Space Center
3. The Boeing Company
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2006-2922
Reference12 articles.
1. 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. "OrbiterReturn-To-FlightEntry Aeroheating," AIAA Paper-2006-2917,June2006.
2. Berry, S. A., Horvath, T. J., Greene, F, Kinder, G., and Wang, K. C. "Overview of Boundary Layer Transition Research in SupportofOrbiter Return to Flight," AIAA Paper-2006-2918,June2006.
3. 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,June2006.
4. Greene, F., and Hamilton, H. "Development of a Boundary Layer Properties Interpolation Tool in Support of Orbiter Return-To-Flight," AIAA Paper-2006-2920,June2006.
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