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Flutter Analysis of a supersonic composite AirFoil skin by using the Differential Quadrature Method

โœ Scribed by Yaobin Niu, Zhongwei Wang, Weihua Zhang

Book ID
118806159
Publisher
Springer US
Year
2012
Tongue
English
Weight
488 KB
Volume
48
Category
Article
ISSN
1573-8922

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Vibration analysis of functionally graded thin-walled rotating blades under high temperature supersonic flow using the differential quadrature method
โœ S.A. Fazelzadeh; P. Malekzadeh; P. Zahedinejad; M. Hosseini ๐Ÿ“‚ Article ๐Ÿ“… 2007 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 337 KB

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 whi