Libros sobre el tema "Laminated and sandwich composite"
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Center, Langley Research, ed. A higher-order bending theory for laminated composite and sandwich beams. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.
Buscar texto completoCenter, Langley Research, ed. A higher-order bending theory for laminated composite and sandwich beams. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.
Buscar texto completoF, Lung S., Gupta K. K y 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. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.
Buscar texto completoF, Lung S., Gupta K. K y 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. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.
Buscar texto completoChamis, C. C. Fiber composite sandwich thermostuctural behavior, computationalsimulation. [Washington, DC]: National Aeronautics and Space Administration, 1986.
Buscar texto completoYu, Yi-Yuan. Vibrations of Elastic Plates: Linear and Nonlinear Dynamical Modeling of Sandwiches, Laminated Composites, and Piezoelectric Layers. New York, NY: Springer New York, 1996.
Buscar texto completoMartin, C. Wayne. A three-node C(superscript)0 element for analysis of laminated composite sandwich shells. Edwards, Calif: Ames Research Center, 1989.
Buscar texto completoR, Tullos Thomas, ed. Handbook of adhesive bonded structural repair. Park Ridge, N.J., U.S.A: Noyes Publications, 1992.
Buscar texto completoVibrations of elastic plates: Linear and nonlinear dynamical modeling of sandwiches, laminated composites, and piezoelectric layers. New York: Springer, 1996.
Buscar texto completoNettles, A. T. (Alan T.), Jackson J. R y 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. Huntsville], Ala: National Aeronautics and Space Administration, Marshall Space Flight Center, 2011.
Buscar texto completoYe, Jianqiao. Laminated Composite Plates and Shells. London: Springer London, 2003. http://dx.doi.org/10.1007/978-1-4471-0095-9.
Texto completoDong, S. B. Edge vibrations in laminated composite plates. New York: American Society of Mechanical Engineers, 1985.
Buscar texto completoNettles, A. T. Basic mechanics of laminated composite plates. Washington D.C: National Aeronautics andSpace Administration, 1994.
Buscar texto completoGeorge C. Marshall Space Flight Center, ed. Basic mechanics of laminated composite plates. MSFC, Ala: Marshall Space Flight Center, National Aeronautics and Space Administration, 1994.
Buscar texto completoS, Springer George y United States. National Aeronautics and Space Administration., eds. Compression behavior of delaminated composite plates. Stanford, Calif: Department of Aeronautics and Astronautics, Stanford University, 1989.
Buscar texto completoUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Division., ed. Delamination stresses in semicircular laminated composite bars. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.
Buscar texto completoUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Division., ed. Delamination stresses in semicircular laminated composite bars. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.
Buscar texto completoT, Haftka Raphael y Hajela Prabhat 1956-, eds. Design and optimization of laminated composite materials. New York: Wiley, 1999.
Buscar texto completoAbrate, Serge. Dynamic Failure of Composite and Sandwich Structures. Dordrecht: Springer Netherlands, 2013.
Buscar texto completoAbrate, Serge, Bruno Castanié y Yapa D. S. Rajapakse, eds. Dynamic Failure of Composite and Sandwich Structures. Dordrecht: Springer Netherlands, 2013. http://dx.doi.org/10.1007/978-94-007-5329-7.
Texto completoM. J. L. van Tooren. Sandwich fuselage design. Delft, Netherlands: Delft University Press, 1998.
Buscar texto completoL, Palko Joseph, Gyekenyesi John P y United States. National Aeronautics and Space Administration., eds. Structural reliabilty analysis of laminated CMC components. [Washington, DC]: National Aeronautics and Space Administration, 1991.
Buscar texto completoAnders, Doughett y Asnarez Peder, eds. Composite laminates: Properties, performance, and applications. Hauppauge, NY: Nova Science Publishers, 2009.
Buscar texto completoDoughett, Anders. Composite laminates: Properties, performance and applications. New York: Nova Science Publishers, 2010.
Buscar texto completoDoughett, Anders. Composite laminates: Properties, performance, and applications. Hauppauge, NY: Nova Science Publishers, 2009.
Buscar texto completoFinn, Scott R. Delaminations in composite plates caused by non-penetrating impact. Stanford, Calif: Department of Aeronautics and Astronautics, Stanford University, 1989.
Buscar texto completoButler, Theresa Ann. The structural response of unsymmetrically laminated composite cylinders. [Washington, DC: National Aeronautics and Space Administration, 1989.
Buscar texto completoRosado, Pablo Rodríguez. Design of multiple-ply laminated composite tapered beams. [Marshall Space Flight Center, Ala.]: National Aeronautics and Space Administration, George C. Marshall Space Flight Center, 1993.
Buscar texto completoRosado, Pablo Rodríguez. Design of multiple-ply laminated composite tapered beams. [Marshall Space Flight Center, Ala.]: National Aeronautics and Space Administration, George C. Marshall Space Flight Center, 1993.
Buscar texto completoGeorge C. Marshall Space Flight Center., ed. Design of multiple-ply laminated composite tapered beams. [Marshall Space Flight Center, Ala.]: National Aeronautics and Space Administration, George C. Marshall Space Flight Center, 1993.
Buscar texto completoRodriguez, P. Design of multiple-ply laminated composite tapered beams. [Marshall Space Flight Center, Ala.]: National Aeronautics and Space Administration, George C. Marshall Space Flight Center, 1993.
Buscar texto completoLeissa, A. W. Buckling of laminated composite plates and shells panels. Ohio: Ohio State Univ., 1985.
Buscar texto completoButler, Theresa Ann. The structural response of unsymmetrically laminated composite cylinders. [Washington, DC: National Aeronautics and Space Administration, 1989.
Buscar texto completoReddy, J. N. Mechanics of laminated composite plates: Theory and analysis. Boca Raton: CRC Press, 1997.
Buscar texto completoJ, Lapid A. y United States. National Aeronautics and Space Administration., eds. The experimental behavior of spinning pretwisted laminated composite plates. [La Jolla, Calif.]: University of Californiam San Diego, Structural Systems Research Project ; [Washington, DC, 1993.
Buscar texto completoUnited States. National Aeronautics and Space Administration., ed. Matrix plasticity in SiC/Ti-15-3 composite. [Washington, DC]: National Aeronautics and Space Administration, 1991.
Buscar texto completoNaaman, Antoine E. Ferrocement and laminated cementitious composites. Ann Arbor, Mich: Techno Press, 2000.
Buscar texto completoK, Dutta Piyush, United States. Army. Office of the Chief of Engineers., Air Force Flight Dynamics Laboratory (U.S.), United States. Army Research Office. y Cold Regions Research and Engineering Laboratory (U.S.), eds. Ballistic perforation of graphic-epoxy composite. Hanover, N.H: U.S. Army Cold Regions Research and Engineering Laboratory, 1996.
Buscar texto completoAltus, Eli. Mechanics of composite materials: An introductory course. [Toronto]: University of Toronto, Institute for Aerospace Studies, 1989.
Buscar texto completoCenter, Langley Research, ed. Investigation of composite material property requirements for sonic fatigue research. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1985.
Buscar texto completoCheung, E. W. Buckling of composite sandwich cylinders under axial compression. Amsterdam: Elsevier Science Publishers, 1988.
Buscar texto completoLee, Sung W., ed. Advances in Thick Section Composite and Sandwich Structures. Cham: Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-31065-3.
Texto completoDaniel, I. M., E. E. Gdoutos y Y. D. S. Rajapakse, eds. Major Accomplishments in Composite Materials and Sandwich Structures. Dordrecht: Springer Netherlands, 2010. http://dx.doi.org/10.1007/978-90-481-3141-9.
Texto completoCheung, Eric Waihon. Buckling of composite sandwich cylinders under axial compression. [Downsview, Ont.]: Dept. of Aerospace Science and Engineering, University of Toronto, 1988.
Buscar texto completoFilho, Mário Kataoka. Optimization of nonhomogeneous facesheets in composite sandwich plates. Ottawa: National Library of Canada = Bibliothèque nationale du Canada, 1997.
Buscar texto completoZafer, Gürdal y United States. National Aeronautics and Space Administration., eds. Compression of thick laminated composite beams with intitial impact-like damage. Blacksburg, Va: College of Engineering, Virginia Polytechnic Institute and State University, 1992.
Buscar texto completoAuerkari, Pertti. Effect of impact face damage on strength of sandwich composites. Espoo, Finland: Technical Research Centre of Finland, 1993.
Buscar texto completoH, Meyn Erwin y United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Vibration testing of impact-damaged composite laminates. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.
Buscar texto completoDelamination buckling of composite materials. Dordrecht: Kluwer, 1988.
Buscar texto completo1945-, Reddy J. N. y United States. National Aeronautics and Space Administration., eds. Nonlinear probabilistic finite element models of laminated composite shells. [Washington, DC]: National Aeronautics and Space Administration, 1993.
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