Books on the topic 'Composite Laminate'
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BridgeComposites, LLC. Laminate specification and characterization: Composite bridge decking. U.S. Department of Transportation, Federal Highway Administration, Highways for LIFE, 2012.
Find full textMartin, Roderick H. Delamination failure in a unidirectional curved composite laminate. National Aeronautics and Space Administration, Langley Research Center, 1990.
Find full textToledano, A. A composite plate theory for arbitrary laminate configurations. Office of Naval Research, 1985.
Find full textC, Chamis C., and United States. National Aeronautics and Space Administration., eds. Composite laminate tailoring with probabilistic constraints and loads. NASA, 1990.
Find full textC, Chamis C., Minnetyan L, and United States. National Aeronautics and Space Administration., eds. Prediction of composite laminate fracture: Micromechanics and progressive fracture. National Aeronautics and Space Administration, 1996.
Find full textMurthy, P. L. N. Free-edge lamination: Laminate width and loading conditions effects. National Aeronautics and Space Administration, 1987.
Find full textMurthy, P. L. N. Free-edge lamination: Laminate width and loading conditions effects. National Aeronautics and Space Administration, 1987.
Find full textMurthy, P. L. N. Free-edge lamination: Laminate width and loading conditions effects. National Aeronautics and Space Administration, 1987.
Find full textMurthy, P. L. N. Free-edge lamination: Laminate width and loading conditions effects. National Aeronautics and Space Administration, 1987.
Find full textGeorge C. Marshall Space Flight Center., ed. The effects of embedded internal delaminations on composite laminate compression strength: An experimental review. National Aeronautics and Space Administration, George C. Marshall Space Flight Center, 1994.
Find full textÖchsner, Andreas. A Simplified Approach to the Classical Laminate Theory of Composite Materials. Springer Nature Switzerland, 2023. http://dx.doi.org/10.1007/978-3-031-38192-8.
Full textÖchsner, Andreas, and Resam Makvandi. A Numerical Approach to the Classical Laminate Theory of Composite Materials. Springer Nature Switzerland, 2023. http://dx.doi.org/10.1007/978-3-031-32975-3.
Full textCenter, Langley Research, ed. The effects of uneven fiber spacing on thermal residual stresses in a unidirectional SCS-6Ti-15-3 laminate. National Aeronautics and Space Administration, Langley Research Center, 1992.
Find full textCenter, Langley Research, ed. The effects of uneven fiber spacing on thermal residual stresses in a unidirectional SCS-6Ti-15-3 laminate. National Aeronautics and Space Administration, Langley Research Center, 1992.
Find full textN, Shivakumar K., and Langley Research Center, eds. Strain-energy release rate analysis of a laminate with a postbuckled delamination. National Aeronautics and Space Administration, Langley Research Center, 1987.
Find full textShaini, Firas Jiries. The clinical performance of porcelain laminate veneers and the factors affecting porcelain/composite bonding. University of Birmingham, 1995.
Find full textUnited States. National Aeronautics and Space Administration., ed. Coupled mixed-field laminate theory and finite element for smart piezolectric composite shell structures. National Aeronautics and Space Administration, 1996.
Find full textUnited States. National Aeronautics and Space Administration., ed. Coupled mixed-field laminate theory and finite element for smart piezolectric composite shell structures. National Aeronautics and Space Administration, 1996.
Find full textUnited States. National Aeronautics and Space Administration., ed. Coupled mixed-field laminate theory and finite element for smart piezolectric composite shell structures. National Aeronautics and Space Administration, 1996.
Find full textS, Raju I., O'Brien T. Kevin, Langley Research Center, and United States. Army Aviation Research and Technology Activity., eds. Strain energy release rate analysis of delamination in a tapered laminate subjected to tension load. National Aeronautics and Space Administration, Langley Research Center, 1990.
Find full textAir Force Wright Aeronautical Laboratories. Cumulative damage model for advanced composite materials. Materials Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, 1985.
Find full textReddy, J. N. A higher-order theory for geometrically nonlinear analysis of composite laminates. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.
Find full textReddy, J. N. A higher-order theory for geometrically nonlinear analysis of composite laminates. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.
Find full textReddy, J. N. A higher-order theory for geometrically nonlinear analysis of composite laminates. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.
Find full textReddy, J. N. A higher-order theory for geometrically nonlinear analysis of composite laminates. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.
Find full textL, Bradley Walter, and United States. National Aeronautics and Space Administration, eds. Micromechanics of composite laminate compression failures: Semi-annual progress report for NASA research grant NAG-1-659, (for work through November 1, 1986). National Aeronautics and Space Administration, 1986.
Find full textMalvern, L. E. Delamination sensing and modeling in localized impacts on filament-reinforced laminated plates. University of Florida, Dept. of Engineering Sciences, 1986.
Find full textKo, William L. Open-mode delamination stress concentrations in horseshoe and elliptic composite curved bars subjected to end forces. Ames Research Center, 1990.
Find full textH, Jackson Raymond, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Open-mode delamination stress concentrations in horseshoe and elliptic composite curved bars subjected to end forces. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.
Find full textYe, Jianqiao. Laminated Composite Plates and Shells. Springer London, 2003. http://dx.doi.org/10.1007/978-1-4471-0095-9.
Full text1942-, Grant Peter, and Rousseau Carl Q. 1962-, eds. Composite structures: Theory and practice. ASTM, 2000.
Find full textS, Springer George, and United States. National Aeronautics and Space Administration., eds. Compression behavior of delaminated composite plates. Department of Aeronautics and Astronautics, Stanford University, 1989.
Find full textSohi, Mohsen M. The effect of resin toughness and modulus on compressive failure modes of quasi-isotropic graphite/epoxy laminates. National Aeronautics and Space Administration, Langley Research Center, 1986.
Find full textSohi, Mohsen M. The effect of resin toughness and modulus on compressive failure modes of quasi-isotropic graphite/epoxy laminates. National Aeronautics and Space Administration, Langley Research Center, 1986.
Find full textUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Division., ed. Delamination stresses in semicircular laminated composite bars. National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.
Find full textUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Division., ed. Delamination stresses in semicircular laminated composite bars. National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.
Find full textCarper, Douglas M. Large deformation behavior of long shallow cylindrical composite panels. Langley Research Center, 1991.
Find full textGabriel, Cederbaum, ed. Random vibration and reliability of composite structures. Technomic Pub. Co., 1992.
Find full textDong, S. B. Edge vibrations in laminated composite plates. American Society of Mechanical Engineers, 1985.
Find full textOchoa, O. O., and J. N. Reddy. Finite Element Analysis of Composite Laminates. Springer Netherlands, 1992. http://dx.doi.org/10.1007/978-94-015-7995-7.
Full textAltenbach, Holm, and Wilfried Becker, eds. Modern Trends in Composite Laminates Mechanics. Springer Vienna, 2003. http://dx.doi.org/10.1007/978-3-7091-2544-1.
Full textAnders, Doughett, and Asnarez Peder, eds. Composite laminates: Properties, performance, and applications. Nova Science Publishers, 2009.
Find full textGeorge C. Marshall Space Flight Center, ed. Basic mechanics of laminated composite plates. Marshall Space Flight Center, National Aeronautics and Space Administration, 1994.
Find full textNettles, A. T. Basic mechanics of laminated composite plates. National Aeronautics andSpace Administration, 1994.
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