Nonlinear Aeroelastic Analysis of the X-56 Multi-Utility Aeroelastic Demonstrator
Author:
Affiliation:
1. University of Michigan, Ann Arbor
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2016-1799
Reference20 articles.
1. Development of a finite element aeroelastic analysis capability
2. Numerical Investigation of Nonlinear Aeroelastic Effects on Flexible High-Aspect-Ratio Wings
3. Nonlinear Flutter Calculations Using Finite Elements in a Direct Eulerian-Lagrangian Formulation
4. Static Nonlinear Aeroelasticity of Flexible Slender Wings in Compressible Flow
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