A shape optimization methodology for reducing the sonic boom initial pressure rise
Author:
Affiliation:
1. Colorado, Univ., Boulder
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2002-145
Reference21 articles.
1. 1A. Busemann, Aerodynamischer Auftreib bei Ueberschallgeswindigkeit, Proc. Volta Congress, 1935, 315-317.
2. Lower bounds for sonic boom considering the negative overpressure region
3. Optimum configurations for bangless sonic booms
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