CFD-Based Aeroelastic Response of an Active Aeroelastic Wing
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American Institute of Aeronautics and Astronautics
Reference11 articles.
1. Ausman, J., and Volk, J. "Integration of Flap Load Limiting into ASTROS," 38thAIAA/ ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Kissimmee, FL, April7-10,1997, AIAA-97-1115.
2. Volk, J., and Ausman, J. "Integration of a Generic Flight Control System into ASTROS," 36thAIAA/ ASME/ASCE/AHS/ASC Structures, Structural DynamiCS, and Materials Conference, Salt Lake City, UT, April15-17,1996, AIAA-96-1335.
3. Miller, G.D. "An Active Flexible Wing Multi-Disciplinary Design Optimization Method," 5thAIAA/ USAF/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization, Panama City, FL, September7-9,1994,AIAA-94-4412.
4. Maneuver Trim Optimization Techniques for Active Aeroelastic Wings
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