Publisher
American Institute of Aeronautics and Astronautics
Cited by
4 articles.
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1. Delta Wing with Store Limit-Cycle-Oscillation Modeling Using a High-Fidelity Structural Model;Journal of Aircraft;2008-05
2. Non-linear aeroelastic prediction for aircraft applications;Progress in Aerospace Sciences;2007-05
3. Nonlinear Aeroelastic Response of the Flexible Wing in Trim;47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference<BR> 14th AIAA/ASME/AHS Adaptive Structures Conference<BR> 7th;2006-05
4. Aeroelastic Analysis for Future Air Vehicle Concepts Using a Fully Nonlinear Methodology;46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference;2005-04-18