Aeroelastic Analysis of SUGAR Truss-Braced Wing Wind-Tunnel Model Using FUN3D and a Nonlinear Structural Model
Author:
Affiliation:
1. NASA Langley Research Center
2. The Boeing Company
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2015-1174
Reference15 articles.
1. Multipoint High-Fidelity Aerostructural Optimization of a Transport Aircraft Configuration
2. Geometry and Structural Modeling for High-Fidelity Aircraft Conceptual Design Optimization
3. Conceptual Design Studies of a Strut-Braced Wing Transonic Transport
4. Design Optimization of a Truss-Braced-Wing Transonic Transport Aircraft
5. Multidisciplinary Design Optimization of Medium-Range Transonic Truss-Braced Wing Transport Aircraft
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