Euler code prediction of near-field to midfield sonic boom pressure signatures
Author:
Affiliation:
1. Grumman Corporate Research Center, Bethpage, New York 11714
2. 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/10.2514/3.46434
Reference16 articles.
1. The flow pattern of a supersonic projectile
2. The Shock Pattern of a Wing-Body Combination, Far from the Flight Path
3. 4Siclari, M. J. "Nonlinear Analysis of Sonic Booms," Ph.D. Dissertation,New York Univ., New York, Jan. 1974.
4. Sonic boom analysis for high altitude flight at high Mach number
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