Application of Finite-Element Theory to Airplane Configurations
Author:
Affiliation:
1. General Dynamics Corporation, Fort Worth, Texas
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.59116
Reference13 articles.
1. Analysis and design of wing-body combinations at subsonic and supersonic speeds.
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1. Simplified Solution of the Compressible Lifting Surface Problem;AIAA Journal;1982-05
2. Simplified solution of the compressible lifting surface problem;18th Aerospace Sciences Meeting;1980-01-14
3. Vortex shedding from circular and noncircular bodies at high angles of attack;17th Aerospace Sciences Meeting;1979-01-15
4. Rolling stabilization through gyroscopically actuated ailerons;Journal of the Chinese Institute of Engineers;1978-01
5. Image system solution for store aerodynamics with interference. I;Journal of Aircraft;1975-03
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