Experimental Validation of Numerical Blade Flutter Prediction
Author:
Affiliation:
1. Faculty of Mechanics and Mathematics, Lomonosov Moscow State University, 119991, Moscow, Russia
2. Stress Department, Gas Turbine Engineering Research and Production Center, Salut, 105118, Moscow, Russia
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.B35419
Reference35 articles.
1. Recent Developments in Flutter Suppression Techniques for Turbomachinery Rotors
2. A REVIEW OF AEROELASTICITY METHODS WITH EMPHASIS ON TURBOMACHINERY APPLICATIONS
3. Flutter and Resonant Vibration Characteristics of Engine Blades
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