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    Modeling of Friction Contact and Its Application to the Design of Shroud Contact 

    Source: Journal of Engineering for Gas Turbines and Power:;1997:;volume( 119 ):;issue: 004:;page 958
    Author(s): B.-D. Yang; C.-H. Menq
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Designers of aircraft engines frequently employ shrouds in turbine design. In this paper, a variable normal load friction force model is proposed to investigate the influence of shroudlike contact ...
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    Characterization of Contact Kinematics and Application to the Design of Wedge Dampers in Turbomachinery Blading: Part 2—Prediction of Forced Response and Experimental Verification 

    Source: Journal of Engineering for Gas Turbines and Power:;1998:;volume( 120 ):;issue: 002:;page 418
    Author(s): B. D. Yang; C. H. Menq
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In the second part of this paper, the application of the proposed dual-interface model to the prediction of the forced response of a blade constrained by wedge dampers will be presented. When ...
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    Characterization of Contact Kinematics and Application to the Design of Wedge Dampers in Turbomachinery Blading: Part 1—Stick-Slip Contact Kinematics 

    Source: Journal of Engineering for Gas Turbines and Power:;1998:;volume( 120 ):;issue: 002:;page 410
    Author(s): B. D. Yang; C. H. Menq
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Friction dampers are often used in turbine design to attenuate blade vibration to acceptable levels so as to prolong blades’ service life. A wedge damper, also called a self-centering, ...
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    Prediction of Resonant Response of Shrouded Blades With Three-Dimensional Shroud Constraint 

    Source: Journal of Engineering for Gas Turbines and Power:;1999:;volume( 121 ):;issue: 003:;page 523
    Author(s): B. D. Yang; J. J. Chen; C. H. Menq
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In this paper, the three-dimensional shroud contact kinematics of a shrouded blade system is studied. The assumed blade motion has three components, namely axial, tangential, and radial components, ...
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