Estimation of Aeroelastic Models in Structural Limit-Cycle Oscillations from Test Data
Author:
Affiliation:
1. Aeronautical Research Laboratory, Taichung, Taiwan 40722, Republic of China
2. University of Kansas, Lawrence, Kansas 66045
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.190
Reference19 articles.
1. Understanding and development of a prediction method of transonic limit cycle oscillation characteristics of fighter aircraft
2. Transonic wind tunnel investigation of limit cycle oscillations on fighter type wings - Update
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4. Transonic region of high dynamic response encountered on an elastic supercritical wing
5. Parameter identification and modeling of longitudinal aerodynamics
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