Reduced-Order Dynamic Aeroelastic Model Development and Integration with Nonlinear Simulation
Author:
Affiliation:
1. The Boeing Company, Long Beach, California 90807
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.2677
Reference24 articles.
1. Equations of motion of a quasisteady flight vehicle utilizing restrained static aeroelastic characteristics
2. Aeroelastic effects on the B-2 maneuver response
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