Dynamic stiffness testing-based flutter analysis of a fin with an actuator
Author:
Funder
National Natural Science Foundation of China
Publisher
Elsevier BV
Subject
Mechanical Engineering,Aerospace Engineering
Reference20 articles.
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2. Beier T. Prediction and measurement of the dynamic stiffness and damping of hydraulic servo-actuators. Reston, VA: AIAA; 1997. Report No.: AIAA-1977-0420.
3. New flutter-suppression method for a missile fin with an actuator;Zhang;J Aircraf,2013
4. Nonlinear flutter analysis of missiles with pneumatic fin actuators;Yehezkely;J Guid Control Dyn,1996
5. Flutter analysis for control surface of launch vehicle with dynamic stiffness;Paek;Comput Struct,1996
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