Experimental Studies of Space Shuttle Orbiter Boundary Layer Transition with Flight Representative Protuberances-Reference-Cited by-同舟云学术

Experimental Studies of Space Shuttle Orbiter Boundary Layer Transition with Flight Representative Protuberances

Published:2011-06-14 Issue: Volume: Page:
ISSN:
Container-title:42nd AIAA Thermophysics Conference
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Author:

Wadhams Timothy¹,Holden Michael¹,MacLean Matthew¹,Campbell Charles²,Anderson Brian²,Berger Karen³,Rufer Shann³,Berry Scott³

Affiliation:

1. CUBRC

2. NASA Johnson Space Center

3. NASA Langley Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2011-3328

Reference34 articles.

1. Orbiter Entry Boundary Layer Flight Testing

2. Horvath, T., Berry, S., Splinter, S., Daryabeigi, K., Wood, W., Schwartz, R., Ross, M. "Assessment and Mission Planning Capability for Quantitative Aerothermodynamic Flight Measurements Using Remote Imaging," AIAA2008-4022,40thThermophysicsComference,Seattle,Was,June23-26,2008.

3. Experimental Space Shuttle Orbiter Studies to Acquire Data for Code and Flight Heating Model Validation

4. Vidal, R.J. "Model Instrumentation Techniques for Heat Transfer and Force Measurements in a Hypersonic ShockTunnel,' CornellAeronauticalLaboratoryReportAD-917-A-1,Feb.1956.

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