Finite state aeroelastic model for use in rotor design optimization
Authors:
- 1 September 1993
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 30 (5) , 777-784
Abstract
No abstract availableKeywords
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- Validation of Rotor Vibratory Airloads and Application to Helicopter ResponseJournal of the American Helicopter Society, 1990
- Integrated aerodynamic/dynamic optimization of helicopter rotor blades1989
- Aeroelastic Optimization of a Helicopter RotorJournal of the American Helicopter Society, 1989
- Application of Design Optimization Techniques to Rotor Dynamics ProblemsJournal of the American Helicopter Society, 1988