The effect of semigeodesic winding on the free vibration characteristics of filament wound shells of revolution is studied. For this purpose multisegment numerical integration technique is extended to the solution of the free vibration problem of composite shells of revolution which are wound along the semigeodesic fiber paths counting on the preset friction used during the winding process. Sample results are obtained for truncated conical and spherical shells of revolution and the effect of preset friction on the vibration characteristics of filament wound shells of revolution is particularly analyzed. Results show that when the preset friction is increased natural frequencies of higher circumferential vibration modes also increase irrespective of the initial winding angle, and the circumferential bending stiffness stands out as the dominant parameter governing the natural frequencies of higher circumferential vibration modes.
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November 2011
Research Papers
Effect of Semi-Geodesic Winding on the Vibration Characteristics of Filament Wound Shells of Revolution
Altan Kayran,
Altan Kayran
Department of Aerospace Engineering,
e-mail: [email protected]
Middle East Technical University
, 06531 Ankara, Turkey
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Can Serkan İbrahimoğlu
Can Serkan İbrahimoğlu
Department of Aerospace Engineering,
e-mail: [email protected]
Middle East Technical University
, 06531 Ankara, Turkey
Search for other works by this author on:
Altan Kayran
Department of Aerospace Engineering,
Middle East Technical University
, 06531 Ankara, Turkey
e-mail: [email protected]
Can Serkan İbrahimoğlu
Department of Aerospace Engineering,
Middle East Technical University
, 06531 Ankara, Turkey
e-mail: [email protected]
J. Appl. Mech. Nov 2011, 78(6): 061008 (11 pages)
Published Online: August 24, 2011
Article history
Received:
April 23, 2010
Revised:
March 19, 2011
Published:
August 24, 2011
Citation
Kayran, A., and İbrahimoğlu, C. S. (August 24, 2011). "Effect of Semi-Geodesic Winding on the Vibration Characteristics of Filament Wound Shells of Revolution." ASME. J. Appl. Mech. November 2011; 78(6): 061008. https://doi.org/10.1115/1.4003907
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