Framework for Aeroservoelastic Analyses Involving Nonlinear Actuators
Author:
Affiliation:
1. Gulfstream Aerospace Corporation, Savannah, Georgia 31402
2. Newsom Aerospace Consulting, LLC, Poquoson, Virginia 23662
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C031246
Reference30 articles.
1. Limit Cycle Oscillation Flight Test Results of a Fighter with External Stores
2. Limit cycle phenomena in computational transonic aeroelasticity
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