CFD prediction of the near-field sonic boom environment for two low boom HSCT configurations
Author:
Affiliation:
1. Grumman Corporate Research Center, Bethpage, NY
2. NASA, Langley Research Center, Hampton, VA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1991-1631
Reference18 articles.
1. High Speed Civil Tranport Study, NASA CR 4234. 1989.
2. The Shock Pattern of a Wing-Body Combination, Far from the Flight Path
3. W 0.800 -
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