Numerical and Experimental Characterization of High Enthalpy Flow in an Expansion Tunnel Facility
Author:
Affiliation:
1. CUBRC
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2010-1562
Reference38 articles.
1. 2Holden, M.S.; Wadhams, T.P.; and Candler, G.V. "Experimental Studies in the LENS Shock Tunnel and Expansion Tunnel to Examine Real-Gas Effects in Hypervelocity Flows". AIAA Paper 2004-0916. January 2004.
2. 4MacLean, M.; Candler, G.; and Holden, M. "Numerical Evaluation of Flow Conditions in the LENS Reflected Shock-Tunnel Facilities". AIAA Paper 2005-0903. 43RDAerospaceSciencesMeeting&Exhibit.Reno,NV:10-13January2005.
3. 5Dufrene, A.; Sharma, M.; and Austin, J.M. "Design and Characterization of a Hypervelocity Expansion Tube Facility," AIAA Paper 2007-1327. 45THAerospaceSciencesMeeting&Exhibit.Reno,NV:8-11January2007.
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