Книги з теми "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.
Знайти повний текст джерелаCenter, 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.
Знайти повний текст джерелаF, 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. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.
Знайти повний текст джерелаF, 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. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.
Знайти повний текст джерелаChamis, C. C. Fiber composite sandwich thermostuctural behavior, computationalsimulation. [Washington, DC]: National Aeronautics and Space Administration, 1986.
Знайти повний текст джерелаYu, 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.
Знайти повний текст джерелаMartin, C. Wayne. A three-node C(superscript)0 element for analysis of laminated composite sandwich shells. Edwards, Calif: Ames Research Center, 1989.
Знайти повний текст джерелаR, Tullos Thomas, ed. Handbook of adhesive bonded structural repair. Park Ridge, N.J., U.S.A: Noyes Publications, 1992.
Знайти повний текст джерелаVibrations of elastic plates: Linear and nonlinear dynamical modeling of sandwiches, laminated composites, and piezoelectric layers. New York: Springer, 1996.
Знайти повний текст джерелаNettles, 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. Huntsville], Ala: National Aeronautics and Space Administration, Marshall Space Flight Center, 2011.
Знайти повний текст джерелаYe, Jianqiao. Laminated Composite Plates and Shells. London: Springer London, 2003. http://dx.doi.org/10.1007/978-1-4471-0095-9.
Повний текст джерелаDong, S. B. Edge vibrations in laminated composite plates. New York: American Society of Mechanical Engineers, 1985.
Знайти повний текст джерелаNettles, A. T. Basic mechanics of laminated composite plates. Washington D.C: National Aeronautics andSpace Administration, 1994.
Знайти повний текст джерелаGeorge C. Marshall Space Flight Center, ed. Basic mechanics of laminated composite plates. MSFC, Ala: Marshall Space Flight Center, National Aeronautics and Space Administration, 1994.
Знайти повний текст джерелаS, Springer George, and United States. National Aeronautics and Space Administration., eds. Compression behavior of delaminated composite plates. Stanford, Calif: Department of Aeronautics and Astronautics, Stanford University, 1989.
Знайти повний текст джерелаUnited 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.
Знайти повний текст джерелаUnited 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.
Знайти повний текст джерелаT, Haftka Raphael, and Hajela Prabhat 1956-, eds. Design and optimization of laminated composite materials. New York: Wiley, 1999.
Знайти повний текст джерелаAbrate, Serge. Dynamic Failure of Composite and Sandwich Structures. Dordrecht: Springer Netherlands, 2013.
Знайти повний текст джерелаAbrate, Serge, Bruno Castanié, and 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.
Повний текст джерелаM. J. L. van Tooren. Sandwich fuselage design. Delft, Netherlands: Delft University Press, 1998.
Знайти повний текст джерелаL, Palko Joseph, Gyekenyesi John P, and United States. National Aeronautics and Space Administration., eds. Structural reliabilty analysis of laminated CMC components. [Washington, DC]: National Aeronautics and Space Administration, 1991.
Знайти повний текст джерелаAnders, Doughett, and Asnarez Peder, eds. Composite laminates: Properties, performance, and applications. Hauppauge, NY: Nova Science Publishers, 2009.
Знайти повний текст джерелаDoughett, Anders. Composite laminates: Properties, performance and applications. New York: Nova Science Publishers, 2010.
Знайти повний текст джерелаDoughett, Anders. Composite laminates: Properties, performance, and applications. Hauppauge, NY: Nova Science Publishers, 2009.
Знайти повний текст джерелаFinn, Scott R. Delaminations in composite plates caused by non-penetrating impact. Stanford, Calif: Department of Aeronautics and Astronautics, Stanford University, 1989.
Знайти повний текст джерелаButler, Theresa Ann. The structural response of unsymmetrically laminated composite cylinders. [Washington, DC: National Aeronautics and Space Administration, 1989.
Знайти повний текст джерелаRosado, 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.
Знайти повний текст джерелаRosado, 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.
Знайти повний текст джерелаGeorge 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.
Знайти повний текст джерелаRodriguez, 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.
Знайти повний текст джерелаLeissa, A. W. Buckling of laminated composite plates and shells panels. Ohio: Ohio State Univ., 1985.
Знайти повний текст джерелаButler, Theresa Ann. The structural response of unsymmetrically laminated composite cylinders. [Washington, DC: National Aeronautics and Space Administration, 1989.
Знайти повний текст джерелаReddy, J. N. Mechanics of laminated composite plates: Theory and analysis. Boca Raton: CRC Press, 1997.
Знайти повний текст джерелаJ, Lapid A., and 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.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration., ed. Matrix plasticity in SiC/Ti-15-3 composite. [Washington, DC]: National Aeronautics and Space Administration, 1991.
Знайти повний текст джерелаNaaman, Antoine E. Ferrocement and laminated cementitious composites. Ann Arbor, Mich: Techno Press, 2000.
Знайти повний текст джерелаK, 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. Hanover, N.H: U.S. Army Cold Regions Research and Engineering Laboratory, 1996.
Знайти повний текст джерелаAltus, Eli. Mechanics of composite materials: An introductory course. [Toronto]: University of Toronto, Institute for Aerospace Studies, 1989.
Знайти повний текст джерелаCenter, Langley Research, ed. Investigation of composite material property requirements for sonic fatigue research. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1985.
Знайти повний текст джерелаCheung, E. W. Buckling of composite sandwich cylinders under axial compression. Amsterdam: Elsevier Science Publishers, 1988.
Знайти повний текст джерелаLee, 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.
Повний текст джерелаDaniel, I. M., E. E. Gdoutos, and 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.
Повний текст джерелаCheung, Eric Waihon. Buckling of composite sandwich cylinders under axial compression. [Downsview, Ont.]: Dept. of Aerospace Science and Engineering, University of Toronto, 1988.
Знайти повний текст джерелаFilho, Mário Kataoka. Optimization of nonhomogeneous facesheets in composite sandwich plates. Ottawa: National Library of Canada = Bibliothèque nationale du Canada, 1997.
Знайти повний текст джерелаZafer, Gürdal, and 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.
Знайти повний текст джерелаAuerkari, Pertti. Effect of impact face damage on strength of sandwich composites. Espoo, Finland: Technical Research Centre of Finland, 1993.
Знайти повний текст джерелаH, Meyn Erwin, and 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.
Знайти повний текст джерелаDelamination buckling of composite materials. Dordrecht: Kluwer, 1988.
Знайти повний текст джерела1945-, Reddy J. N., and 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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