In this study, differential quadrature (DQ) vibration analysis of a rotating thin walled-blade made of functionally graded materials (FGMs) operating under high temperature supersonic gas flow is investigated. The governing equations are based on the first-order shear deformation theory of beams which include the effects of the rotary inertias and the blade presetting angle. Quasi-steady aerodynamic pressure loadings and steady wall temperature assumptions are made. The explicit DQ-discretized form of the equations of motion and the related boundary conditions are presented. The convergence of the method is examined and to verify its accuracy, the results are compared with those of the Galerkin method where excellent agreements are observed. The effects of the Mach number, rotating speed, geometric parameters and blade material properties on the natural frequencies are examined. (c) 2007 Elsevier Ltd. All rights reserved.
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Virginia Polytech Inst & State Univ, Dept Engn Sci & Mech, Blacksburg, VA 24061 USAVirginia Polytech Inst & State Univ, Dept Engn Sci & Mech, Blacksburg, VA 24061 USA
Librescu, L
Oh, SY
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机构:Virginia Polytech Inst & State Univ, Dept Engn Sci & Mech, Blacksburg, VA 24061 USA
Oh, SY
Song, O
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机构:Virginia Polytech Inst & State Univ, Dept Engn Sci & Mech, Blacksburg, VA 24061 USA
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Ho Chi Minh City Univ Technol & Educ, Fac Civil Engn, Ho Chi Minh City, VietnamHo Chi Minh City Univ Technol & Educ, Fac Civil Engn, Ho Chi Minh City, Vietnam
Bui, Xuan-Bach
Nguyen, Trung-Kien
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HUTECH Univ, CIRTech Inst, 475A Dien Bien Phu St, Ho Chi Minh City, VietnamHo Chi Minh City Univ Technol & Educ, Fac Civil Engn, Ho Chi Minh City, Vietnam
Nguyen, Trung-Kien
Nguyen, Phong T. T.
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Ho Chi Minh City Univ Technol & Educ, Fac Int Educ, Ho Chi Minh City, VietnamHo Chi Minh City Univ Technol & Educ, Fac Civil Engn, Ho Chi Minh City, Vietnam