Numerical Analysis of Store-Induced Limit-Cycle Oscillation
Author:
Affiliation:
1. U.S. Air Force Research Laboratory, Wright–Patterson Air Force Base, Ohio 45433
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.404
Reference26 articles.
1. Limit Cycle Oscillation Flight Test Results of a Fighter with External Stores
2. Effect of Store Aerodynamics on Wing/Store Flutter
3. Static and Dynamic Aeroelasticity of Advanced Aircraft Wings Carrying External Stores
4. Transonic Flutter Analysis of a Rectangular Wing with Conventional Airfoil Sections
5. Nonlinear simulation of F-16 aeroelastic instability
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