Books on the topic 'Laminated and sandwich composite'
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Center, Langley Research, ed. A higher-order bending theory for laminated composite and sandwich beams. National Aeronautics and Space Administration, Langley Research Center, 1997.
Find full textCenter, Langley Research, ed. A higher-order bending theory for laminated composite and sandwich beams. National Aeronautics and Space Administration, Langley Research Center, 1997.
Find full textF, Lung S., Gupta K. K, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. A three-node C ̊element for analysis of laminated composite sandwich shells. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.
Find full textF, Lung S., Gupta K. K, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. A three-node C ̊element for analysis of laminated composite sandwich shells. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.
Find full textYu, Yi-Yuan. Vibrations of Elastic Plates: Linear and Nonlinear Dynamical Modeling of Sandwiches, Laminated Composites, and Piezoelectric Layers. Springer New York, 1996.
Find full textChamis, C. C. Fiber composite sandwich thermostuctural behavior, computationalsimulation. National Aeronautics and Space Administration, 1986.
Find full textMartin, C. Wayne. A three-node C(superscript)0 element for analysis of laminated composite sandwich shells. Ames Research Center, 1989.
Find full textCenter, Langley Research, ed. Analytic and computational perspectives of multi-scale theory for homogeneous, laminated composite, and sandwich beams and plates. National Aeronautics and Space Administration, Langley Research Center, 2012.
Find full textNettles, A. T. (Alan T.), Jackson J. R, and George C. Marshall Space Flight Center, eds. Comparison of open-hole compression strength and compression after impact strength on carbon fiber/epoxy laminates for the Ares I composite interstage. National Aeronautics and Space Administration, Marshall Space Flight Center, 2011.
Find full textYe, Jianqiao. Laminated Composite Plates and Shells. Springer London, 2003. http://dx.doi.org/10.1007/978-1-4471-0095-9.
Full textDong, S. B. Edge vibrations in laminated composite plates. American Society of Mechanical Engineers, 1985.
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.
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 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 textT, Haftka Raphael, and Hajela Prabhat 1956-, eds. Design and optimization of laminated composite materials. Wiley, 1999.
Find full textAbrate, Serge. Dynamic Failure of Composite and Sandwich Structures. Springer Netherlands, 2013.
Find full textAbrate, Serge, Bruno Castanié, and Yapa D. S. Rajapakse, eds. Dynamic Failure of Composite and Sandwich Structures. Springer Netherlands, 2013. http://dx.doi.org/10.1007/978-94-007-5329-7.
Full textAnders, Doughett, and Asnarez Peder, eds. Composite laminates: Properties, performance, and applications. Nova Science Publishers, 2009.
Find full textDoughett, Anders. Composite laminates: Properties, performance and applications. Nova Science Publishers, 2010.
Find full textDoughett, Anders. Composite laminates: Properties, performance, and applications. Nova Science Publishers, 2009.
Find full textL, Palko Joseph, Gyekenyesi John P, and United States. National Aeronautics and Space Administration., eds. Structural reliabilty analysis of laminated CMC components. National Aeronautics and Space Administration, 1991.
Find full textFinn, Scott R. Delaminations in composite plates caused by non-penetrating impact. Department of Aeronautics and Astronautics, Stanford University, 1989.
Find full textNaaman, Antoine E. Ferrocement and laminated cementitious composites. Techno Press, 2000.
Find full textButler, Theresa Ann. The structural response of unsymmetrically laminated composite cylinders. National Aeronautics and Space Administration, 1989.
Find full textRosado, Pablo Rodríguez. Design of multiple-ply laminated composite tapered beams. National Aeronautics and Space Administration, George C. Marshall Space Flight Center, 1993.
Find full textButler, Theresa Ann. The structural response of unsymmetrically laminated composite cylinders. National Aeronautics and Space Administration, 1989.
Find full textLeissa, A. W. Buckling of laminated composite plates and shells panels. Ohio State Univ., 1985.
Find full textReddy, J. N. Mechanics of laminated composite plates: Theory and analysis. CRC Press, 1997.
Find full textRosado, Pablo Rodríguez. Design of multiple-ply laminated composite tapered beams. National Aeronautics and Space Administration, George C. Marshall Space Flight Center, 1993.
Find full textGeorge C. Marshall Space Flight Center., ed. Design of multiple-ply laminated composite tapered beams. National Aeronautics and Space Administration, George C. Marshall Space Flight Center, 1993.
Find full textRodriguez, P. Design of multiple-ply laminated composite tapered beams. National Aeronautics and Space Administration, George C. Marshall Space Flight Center, 1993.
Find full textUnited States. National Aeronautics and Space Administration., ed. Matrix plasticity in SiC/Ti-15-3 composite. National Aeronautics and Space Administration, 1991.
Find full textK, Dutta Piyush, United States. Army. Office of the Chief of Engineers., Air Force Flight Dynamics Laboratory (U.S.), United States. Army Research Office., and Cold Regions Research and Engineering Laboratory (U.S.), eds. Ballistic perforation of graphic-epoxy composite. U.S. Army Cold Regions Research and Engineering Laboratory, 1996.
Find full textJ, Lapid A., and United States. National Aeronautics and Space Administration., eds. The experimental behavior of spinning pretwisted laminated composite plates. University of Californiam San Diego, Structural Systems Research Project ; [Washington, DC, 1993.
Find full textAltus, Eli. Mechanics of composite materials: An introductory course. University of Toronto, Institute for Aerospace Studies, 1989.
Find full textCenter, Langley Research, ed. Investigation of composite material property requirements for sonic fatigue research. National Aeronautics and Space Administration, Langley Research Center, 1985.
Find full textCheung, E. W. Buckling of composite sandwich cylinders under axial compression. Elsevier Science Publishers, 1988.
Find full textLee, Sung W., ed. Advances in Thick Section Composite and Sandwich Structures. Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-31065-3.
Full textDaniel, I. M., E. E. Gdoutos, and Y. D. S. Rajapakse, eds. Major Accomplishments in Composite Materials and Sandwich Structures. Springer Netherlands, 2010. http://dx.doi.org/10.1007/978-90-481-3141-9.
Full textFilho, Mário Kataoka. Optimization of nonhomogeneous facesheets in composite sandwich plates. National Library of Canada = Bibliothèque nationale du Canada, 1997.
Find full textCheung, Eric Waihon. Buckling of composite sandwich cylinders under axial compression. Dept. of Aerospace Science and Engineering, University of Toronto, 1988.
Find full textH, Meyn Erwin, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Vibration testing of impact-damaged composite laminates. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.
Find full textZafer, Gürdal, and United States. National Aeronautics and Space Administration., eds. Compression of thick laminated composite beams with intitial impact-like damage. College of Engineering, Virginia Polytechnic Institute and State University, 1992.
Find full textAuerkari, Pertti. Effect of impact face damage on strength of sandwich composites. Technical Research Centre of Finland, 1993.
Find full textW, Hyer M., Shuart Mark J, Virginia Polytechnic Institute and State University. Center for Composite Materials and Structures., and Langley Research Center. Aircraft Structures Branch., eds. Thermal buckling and postbuckling of symmetrically laminated composite plates. Center for Composite Materials and Structures, College of Engineering, Virginia Polytechnic Institute and State University, 1991.
Find full textNational Aeronautics and Space Administration (NASA) Staff. Higher-Order Bending Theory for Laminated Composite and Sandwich Beams. Independently Published, 2018.
Find full textAbrate, Serge. Dynamics of Composite and Sandwich Marine Structures: Water Impact and Underwater Explosions. Wiley & Sons, Limited, John, 2022.
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