Development of a finite element aeroelastic analysis capability
Author:
Affiliation:
1. NASA Dryden Flight Research Center, Edwards, California 93523
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.47046
Reference26 articles.
1. Unsteady full potential aeroelastic computations for flexible configurations
2. Time-accurate unsteady aerodynamic and aeroelastic calculations for wings using Euler equations
3. Vortical flow computations on a flexible blended wing-body configuration
4. Aeroelastic analysis of wings using the Euler equations with a deforming mesh
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