Aeroelastic Analysis of Aircraft Wind-Tunnel Model Coupling Structural and Fluid Dynamic Codes
Author:
Affiliation:
1. Piaggio Aero Industries, 80078 Naples, Italy
2. University of Rome “Tor Vergata”, 00133 Rome, Italy
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C031293
Reference15 articles.
1. Fluid-Structure-Coupled Analysis of a Transport Aircraft and Comparison to Flight Data
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3. Mesh deformation based on radial basis function interpolation
4. Higher-order time integration through smooth mesh deformation for 3D fluid–structure interaction simulations
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