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An Approximate Solution For Interlaminar Stresses In Laminated Composites
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Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781723513756 Total Pages :212 pages Book Rating :4.5/5 (137 download)
Book Synopsis An Approximate Solution for Interlaminar Stresses in Laminated Composites by : National Aeronautics and Space Administration (NASA)
Download or read book An Approximate Solution for Interlaminar Stresses in Laminated Composites written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-23 with total page 212 pages. Available in PDF, EPUB and Kindle. Book excerpt: An approximate solution for interlaminar stresses in finite width, laminated composites subjected to uniform extensional, and bending loads is presented. The solution is based upon the principle of minimum complementary energy and an assumed, statically admissible stress state, derived by considering local material mismatch effects and global equilibrium requirements. The stresses in each layer are approximated by polynomial functions of the thickness coordinate, multiplied by combinations of exponential functions of the in-plane coordinate, expressed in terms of fourteen unknown decay parameters. Imposing the stationary condition of the laminate complementary energy with respect to the unknown variables yields a system of fourteen non-linear algebraic equations for the parameters. Newton's method is implemented to solve this system. Once the parameters are known, the stresses can be easily determined at any point in the laminate. Results are presented for through-thickness and interlaminar stress distributions for angle-ply, cross-ply (symmetric and unsymmetric laminates), and quasi-isotropic laminates subjected to uniform extension and bending. It is shown that the solution compares well with existing finite element solutions and represents an improved approximate solution for interlaminar stresses, primarily at interfaces where global equilibrium is satisfied by the in-plane stresses, but large local mismatch in properties requires the presence of interlaminar stresses. Rose, Cheryl A. and Herakovich, Carl T. Unspecified Center NASA-CR-190537, NAS 1.26:190537, AM-92-02 NAG1-841...
Book Synopsis Scientific and Technical Aerospace Reports by :
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1994 with total page 652 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Failure in Composites by : Anthony M. Waas
Download or read book Failure in Composites written by Anthony M. Waas and published by DEStech Publications, Inc. This book was released on 2013 with total page 282 pages. Available in PDF, EPUB and Kindle. Book excerpt: The fourth volume of the ASC series on advanced composites contains critical information on static and dynamic composite failure and how it is predicted and modeled using novel computational methods and micromechanical analysis.
Book Synopsis Recent Advances in Theoretical, Applied, Computational and Experimental Mechanics by : B. N. Singh
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Book Synopsis Engineering Mechanics of Fibre Reinforced Polymers and Composite Structures by : J. Hult
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Book Synopsis Delaware Composites Design Encyclopedia by : University of Delawa
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Book Synopsis Monthly Catalog of United States Government Publications by : United States. Superintendent of Documents
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Book Synopsis Composite Structures by : I.H. Marshall
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Book Synopsis Proceedings of the Tenth International Conference on Composite Materials by : Anoush Poursartip
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Book Synopsis Mechanics of Composite Materials by : J.N. Reddy
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Book Synopsis The ACEE Program and Basic Composites Research at Langley Research Center (1975 to 1986) by : Marvin B. Dow
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