Verification of the Heat-Field Concept for Sonic-Boom Alleviation
Author:
Affiliation:
1. The Aerospace Corporation, El Segundo, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.59803
Reference17 articles.
1. Alleviation of the Sonic Boom by Thermal Means
2. Sonic‐Boom Minimization
3. Optimum configurations for bangless sonic booms
4. Sonic boom minimization including both front and rear shocks
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1. Sonic Boom Alleviation Using Keel Configurations;Journal of Aircraft;2003-03
2. Minimization of Sonic Boom with Genetic Algorithms;41st Aerospace Sciences Meeting and Exhibit;2003-01-06
3. Minimization of Sonic Boom on Supersonic Aircraft Using an Evolutionary Algorithm;Genetic and Evolutionary Computation — GECCO 2003;2003
4. Boom alleviation using keel configurations;40th AIAA Aerospace Sciences Meeting & Exhibit;2002-01-14
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