Computational Technology Resources - CCP

Paper I.14

Structural Response of the Plain Weave GFRP Cylindrical Shell Subjected to Low-Velocity Central Impact

B.D. Choi and Y.S. Lee

Department of Mechanical Design Engineering, Chungnam National University, Taejon, Korea

doi:10.4203/ccp.67.1.14

B.D. Choi, Y.S. Lee, "Structural Response of the Plain Weave GFRP Cylindrical Shell Subjected to Low-Velocity Central Impact", in B.H.V. Topping, (Editor), "Computational Techniques for Materials, Composites and Composite Structures", Civil-Comp Press, Edinburgh, UK, pp 121-126, 2000. doi:10.4203/ccp.67.1.14

Abstract

The structural response for the plain weave composite GFRP circular cylindrical shell under low-velocity central impact by a foreign body is presented. The analytical solution using the first order shear deformation theory with the Hertzian contact law is derived. A numerical analysis using the finite element structural code and the experiment with the drop weight test apparatus are carried out concurrently. The strain responses of the shell obtained in three ways are well agreed with each other.

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Front Page Browse CCP CSETS CTR IJRT Other Authors Search Purchase Guide FAQ Contact us	Civil-Comp Proceedings ISSN 1759-3433 CCP: 67 COMPUTATIONAL TECHNIQUES FOR MATERIALS, COMPOSITES AND COMPOSITE STRUCTURES Edited by: B.H.V. Topping Paper I.14 Structural Response of the Plain Weave GFRP Cylindrical Shell Subjected to Low-Velocity Central Impact B.D. Choi and Y.S. Lee Department of Mechanical Design Engineering, Chungnam National University, Taejon, Korea doi:10.4203/ccp.67.1.14 purchase the full-text of this paper Full Bibliographic Reference for this paper B.D. Choi, Y.S. Lee, "Structural Response of the Plain Weave GFRP Cylindrical Shell Subjected to Low-Velocity Central Impact", in B.H.V. Topping, (Editor), "Computational Techniques for Materials, Composites and Composite Structures", Civil-Comp Press, Edinburgh, UK, pp 121-126, 2000. doi:10.4203/ccp.67.1.14 Abstract The structural response for the plain weave composite GFRP circular cylindrical shell under low-velocity central impact by a foreign body is presented. The analytical solution using the first order shear deformation theory with the Hertzian contact law is derived. A numerical analysis using the finite element structural code and the experiment with the drop weight test apparatus are carried out concurrently. The strain responses of the shell obtained in three ways are well agreed with each other. purchase the full-text of this paper (price £20) go to the previous paper go to the next paper return to the table of contents return to the book description purchase this book (price £92 +P&P)
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