1. Friction Damping of Resonant Stresses in Gas Turbine Engine Airfoils
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3. Wang, J. H., and Yau, H. Y. , 1990, “Design of Shroud Interface-Angle to Minimize the Forced Vibration of Blades,” ASME Gas Turbine and Aeroengine Congress and Exhibition, Brussels, ASME Paper No. 90-GT-247.
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5. The influence of a variable friction coefficient on the dynamic behavior of a blade with a friction damper