FLUTTER OF COMPOSITE PLATES WITH ELASTIC SUPPORTS

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REZAEI PAJAND J.; ESMAILI J.

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Paper Information

Journal: AMIRKABIR Year:2005 | Volume:16 | Issue:62-B Page(s): 1-8

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Title

FLUTTER OF COMPOSITE PLATES WITH ELASTIC SUPPORTS

Author(s)

REZAEI PAJAND J. | ESMAILI J. | Issue Writer Certificate

Keywords

FLUTTERQ2

ELASTIC SUPPORTSQ2

ORTHOTROPIC PLATESQ3

COMPOSITESQ4

IN-PLANE LOADQ4

Abstract

This study aims at FLUTTER characteristics of ORTHOTROPIC PLATES subjected to supersonic flow. The plate is subjected to uniform in-plane forces (Nx, Ny) and its edges are assumed to be elastically restrained (with various degree) against rotation. This type of boundary conditions covered a wide range of B.C's from simply support to clamped supports. The analytical solution is obtained using classical plate theory. Frequency equations of these systems are very large and difficult to solve. A simple method of solving this type of equations has been used in order to investigate the FLUTTER characteristics of 011hotropic plates. The effect of plate geometry, material propel1ies, IN-PLANE LOAD and boundary condition are presented and discussed.

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APA: Copy

REZAEI PAJAND, J., & ESMAILI, J.. (2005). FLUTTER OF COMPOSITE PLATES WITH ELASTIC SUPPORTS. AMIRKABIR, 16(62-B), 1-8. SID. https://sid.ir/paper/750/en

Vancouver: Copy

REZAEI PAJAND J., ESMAILI J.. FLUTTER OF COMPOSITE PLATES WITH ELASTIC SUPPORTS. AMIRKABIR[Internet]. 2005;16(62-B):1-8. Available from: https://sid.ir/paper/750/en

IEEE: Copy

J. REZAEI PAJAND, and J. ESMAILI, “FLUTTER OF COMPOSITE PLATES WITH ELASTIC SUPPORTS,” AMIRKABIR, vol. 16, no. 62-B, pp. 1–8, 2005, [Online]. Available: https://sid.ir/paper/750/en

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