Aeroelastic analysis of transonic wings using Navier-Stokes equations and a nonlinear beam finite element model
Author:
Affiliation:
1. NASA, Ames Research Center, Moffett Field, CA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1999-1215
Reference32 articles.
1. Large deflection of cantilever beams
2. On the Nonlinear Deformation Geometry of Euler-Bernoulli Beams.
3. Nonlinear aeroelastic analysis of aircraft with high-aspect-ratio wings
4. Matrix displacement solution to elastica problems of beams and frames
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