Numerical study on using sulfur hexafluoride as a wind tunnel test gas
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Virginia 23665
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.10856
Reference9 articles.
1. Allied Chemical Corporation, TB524-99-1787-2.
2. Flux-vector splitting for the Euler equations
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