Coupled finite-difference/finite-element approach for wing-body aeroelasticity
Author:
Affiliation:
1. NASA, Ames Research Center, Moffett Field, CA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1992-4680
Reference29 articles.
1. sonic Steady and Unsteady Aerodpnarnics for Aerorlastic Applications, Volume I-Theoretical Manual," AFWAL-TR-80-3107, Dec. 1985.
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