Computational Aeroelastic Simulation of Rapidly Morphing Air Vehicles
Author:
Affiliation:
1. Technion — Israel Institute of Technology, 32000 Haifa, Israel
2. Israeli Computational Fluid Dynamics Center, 38900 Caesarea Industrial Park, Israel
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C031041
Reference37 articles.
1. Coupling of substructures for dynamic analyses.
2. Modelling the Dynamic Response of a Morphing Wing with Active Winglets
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