Origins and Overview of the Shaped Sonic Boom Demonstration Program
Author:
Affiliation:
1. Northrop Grumman Corporation
2. NASA Langley Research Center
3. Eagle Aeronautics Inc.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2005-5
Reference44 articles.
1. 2Carlson, H. W. "The Lower Bound of Attainable Sonic-Boom Overpressure and Design Methods of Approaching This Limit." NASA TN-D-1494, Oct.1962.
2. Influence of airplane configuration on sonic- boom characteristics
3. 5McLean,F.E."SomeNonasymptoticEffectsontheSonicBoomofLargeAirplanes,"NASATN-D-2877,June1965.
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