Nonlinear Modal Aeroservoelastic Analysis Framework for Flexible Aircraft
Author:
Affiliation:
1. Imperial College, London, England SW7 2AZ, United Kingdom
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J054537
Reference32 articles.
1. Reexamined Structural Design Procedures for Very Flexible Aircraft
2. Integrated simulation model for preliminary aerodynamic, structural, and control-law design of aircraft
3. Unified Theory for the Dynamics and Control of Maneuvering Flexible Aircraft
4. Multibody Dynamic Approach of Flight Dynamics and Nonlinear Aeroelasticity of Flexible Aircraft
5. Applications of the unsteady vortex-lattice method in aircraft aeroelasticity and flight dynamics
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