Subsonic Steady and Oscillatory Aerodynamics for Multiple Interfering Wings and Bodies
Author:
Affiliation:
1. Douglas Aircraft Company, McDonnell Douglas Corporation, Long Beach, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.59066
Reference36 articles.
1. Giesing, J. P. "Lifting Surface Theory for Wing-Fuselage Combinations," Report DAC-67212, Aug. 1968, McDonnell Douglas Corp., Long Beach,Calif.
2. Analysis and design of wing-body combinations at subsonic and supersonic speeds.
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