Global Heat-Transfer Measurements on the NASA Crew Exploration Vehicle at AEDC Tunnel 9
Author:
Affiliation:
1. University of Maryland
2. LeaTech LLC
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2008-3947
Reference7 articles.
1. Ragsdale,W.C.andBoyd,C.F.,HypervelocityWindTunnel9FacilityHandbook,ThirdEdition,NAVSWCTR91-616,Silver Spring,MD, July1993.
2. Liu,T.,Sullivan,J.P.,PressureandTemperatureSensitivePaints,Springer,NewYork,2005.
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1. Temperature Sensitive Paint Response to Fluctuating/Decreasing Heating Loads in AEDC Tunnel 9;AIAA Scitech 2019 Forum;2019-01-06
2. The Hypervelocity Wind Tunnel No. 9; Continued Excellence Through Improvement and Modernization;53rd AIAA Aerospace Sciences Meeting;2015-01-03
3. Temperature-Sensitive Paint Calibration Methodology Developed at AEDC Tunnel 9;49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2011-01-04
4. Aerothermal Testing for Project Orion Crew Exploration Vehicle;41st AIAA Thermophysics Conference;2009-06-14
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