Stability and Control of a Structurally Nonlinear Aeroelastic System
Author:
Affiliation:
1. Texas A&M University, College Station, Texas 77843-3141
2. University of Florida, Gainesville, Florida 32611-6250
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.4317
Reference21 articles.
1. Flutter and stall response of a helicopter blade with structural nonlinearity
2. NONLINEAR BEHAVIOR OF A TYPICAL AIRFOIL SECTION WITH CONTROL SURFACE FREEPLAY: A NUMERICAL AND EXPERIMENTAL STUDY
3. Digital Adaptive Flutter Suppression and Simulation Using Approximate Transonic Aerodynamics
4. Adaptive Control of Aeroelastic Instabilities in Transonic Flow and Its Scaling
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