Books on the topic 'Laminated and sandwich composite'

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.

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.

F, 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.

F, 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.

Chamis, C. C. Fiber composite sandwich thermostuctural behavior, computationalsimulation. [Washington, DC]: National Aeronautics and Space Administration, 1986.

Yu, 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.

Martin, C. Wayne. A three-node C(superscript)0 element for analysis of laminated composite sandwich shells. Edwards, Calif: Ames Research Center, 1989.

R, Tullos Thomas, ed. Handbook of adhesive bonded structural repair. Park Ridge, N.J., U.S.A: Noyes Publications, 1992.

Vibrations of elastic plates: Linear and nonlinear dynamical modeling of sandwiches, laminated composites, and piezoelectric layers. New York: Springer, 1996.

Nettles, 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.

Ye, Jianqiao. Laminated Composite Plates and Shells. London: Springer London, 2003. http://dx.doi.org/10.1007/978-1-4471-0095-9.

Dong, S. B. Edge vibrations in laminated composite plates. New York: American Society of Mechanical Engineers, 1985.

Nettles, A. T. Basic mechanics of laminated composite plates. Washington D.C: National Aeronautics andSpace Administration, 1994.

George C. Marshall Space Flight Center, ed. Basic mechanics of laminated composite plates. MSFC, Ala: Marshall Space Flight Center, National Aeronautics and Space Administration, 1994.

S, 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.

United 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.

United 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.

T, Haftka Raphael, and Hajela Prabhat 1956-, eds. Design and optimization of laminated composite materials. New York: Wiley, 1999.

Abrate, Serge. Dynamic Failure of Composite and Sandwich Structures. Dordrecht: Springer Netherlands, 2013.

Abrate, 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.

M. J. L. van Tooren. Sandwich fuselage design. Delft, Netherlands: Delft University Press, 1998.

L, 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.

Anders, Doughett, and Asnarez Peder, eds. Composite laminates: Properties, performance, and applications. Hauppauge, NY: Nova Science Publishers, 2009.

Doughett, Anders. Composite laminates: Properties, performance and applications. New York: Nova Science Publishers, 2010.

Doughett, Anders. Composite laminates: Properties, performance, and applications. Hauppauge, NY: Nova Science Publishers, 2009.

Finn, Scott R. Delaminations in composite plates caused by non-penetrating impact. Stanford, Calif: Department of Aeronautics and Astronautics, Stanford University, 1989.

Butler, Theresa Ann. The structural response of unsymmetrically laminated composite cylinders. [Washington, DC: National Aeronautics and Space Administration, 1989.

Rosado, 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.

Rosado, 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.

George 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.

Rodriguez, 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.

Leissa, A. W. Buckling of laminated composite plates and shells panels. Ohio: Ohio State Univ., 1985.

Butler, Theresa Ann. The structural response of unsymmetrically laminated composite cylinders. [Washington, DC: National Aeronautics and Space Administration, 1989.

Reddy, J. N. Mechanics of laminated composite plates: Theory and analysis. Boca Raton: CRC Press, 1997.

J, 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.

United States. National Aeronautics and Space Administration., ed. Matrix plasticity in SiC/Ti-15-3 composite. [Washington, DC]: National Aeronautics and Space Administration, 1991.

Naaman, Antoine E. Ferrocement and laminated cementitious composites. Ann Arbor, Mich: Techno Press, 2000.

K, 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.

Altus, Eli. Mechanics of composite materials: An introductory course. [Toronto]: University of Toronto, Institute for Aerospace Studies, 1989.

Center, Langley Research, ed. Investigation of composite material property requirements for sonic fatigue research. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1985.

Cheung, E. W. Buckling of composite sandwich cylinders under axial compression. Amsterdam: Elsevier Science Publishers, 1988.

Lee, 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.

Daniel, 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.

Cheung, Eric Waihon. Buckling of composite sandwich cylinders under axial compression. [Downsview, Ont.]: Dept. of Aerospace Science and Engineering, University of Toronto, 1988.

Filho, Mário Kataoka. Optimization of nonhomogeneous facesheets in composite sandwich plates. Ottawa: National Library of Canada = Bibliothèque nationale du Canada, 1997.

Zafer, 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.

Auerkari, Pertti. Effect of impact face damage on strength of sandwich composites. Espoo, Finland: Technical Research Centre of Finland, 1993.

H, 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.

Delamination buckling of composite materials. Dordrecht: Kluwer, 1988.

1945-, 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.