Nonlinear Aeroelastic Analysis for a Control Fin with an Actuator
Author:
Affiliation:
1. Korea Advanced Institute of Science and Technology, Daejeon 305-701, Republic of Korea
2. Agency for Defense Development, Daejeon 305-701, Republic of Korea
3. Hankuk Aviation University, Seoul 200-1, Republic of Korea
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.24721
Reference18 articles.
1. An Investigation of Effects of Certain Types of Structural NonHnearities on Wing and Control Surface Flutter
2. Flutter Analysis of Missile Control Surfaces Containing Structural Nonlinearities
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5. Analysis of limit cycle flutter of an airfoil in incompressible flow
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