A Recurrence Matrix Solution for the Dynamic Response of Elastic Aircraft
Author:
Affiliation:
1. Lang ley Aeronautical Laboratory, N.A.C.A.,
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Link
http://arc.aiaa.org/doi/pdf/10.2514/8.1722
Reference19 articles.
1. Fluids, Proc. 5th Volta Congress, Rome, pp.255-264, 1935. Vol.40, pp. 279-313, 1932.
2. Effect of Variable Viscosity on Boundary Layers, With a Discussion of Drag Measurements
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