Books on the topic 'Composite Plates'

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

J, Turvey G., and Marshall I. H, eds. Buckling and postbuckling of composite plates. London: Chapman & Hall, 1995.

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

Turvey, G. J., and I. H. Marshall, eds. Buckling and Postbuckling of Composite Plates. Dordrecht: Springer Netherlands, 1995. http://dx.doi.org/10.1007/978-94-011-1228-4.

Composite panels/plates: Analysis and design. Lancaster, Pa: Technomic Pub. Co., 1986.

Finn, Scott R. Composite plates impact damage: An atlas. Lancaster, Pa: Technomic Pub. Co., 1991.

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

Hussein, Raafat M. M. Composite panels/plates: Analysis and design. Lancaster, Pa: Technomic Pub., 1986.

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.

Turvey, G. J. Buckling and Postbuckling of Composite Plates. Dordrecht: Springer Netherlands, 1995.

Birman, Victor. Response of composite plates to blast loading. [S.l.]: [s.n.], 1987.

Hwu, Chyanbin. Anisotropic elastic plates. New York: Springer, 2010.

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.

Center, Langley Research, ed. A treatise on equivalent-plate stiffnesses for stiffened laminated-composite plates and plate-like lattices. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 2011.

Albert, Filemyr, and Delaware Valley Ornithological Club, eds. The composite plates of Audubon's Birds of America. Philadelphia, Pa: Delaware Valley Ornithological Club, 2008.

W, Hyer M., and United States. National Aeronautics and Space Administration., eds. Postbuckling failure of composite plates with central holes. Blacksburg, Va: Virginia Polytechnic Institute and State University, 1992.

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

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

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

United States. National Aeronautics and Space Administration., ed. Response of composite plates subjected to acoustic loading. [Washington, DC: National Aeronautics and Space Administration, 1989.

Malvern, L. E. Delamination sensing and modeling in localized impacts on filament-reinforced laminated plates. Gainesville, Florida: University of Florida, Dept. of Engineering Sciences, 1986.

W, Hyer M., and United States. National Aeronautics and Space Administration., eds. The stress distribution in pin-loaded orthotropic plates. Blacksburg, VA: College of Engineering, Virginia Polytechnic Institute and State University, 1985.

Abrate, Serge. Impact engineering of composite structures. Wien: Springer, 2011.

Kennedy, Stephen John. Behaviour of transversely loaded continuous steel-concrete composite plates. Edmonton, Alta: Dept. of Civil Engineering, University of Alberta, 1987.

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

Waas, Anthony M. Failure of composite plates under static biaxial planar loading. [Ann Arbor, Mich.]: Composite Structures Laboratory, Dept. of Aerospace Engineering, College of Engineering, University of Michigan, 1992.

W, 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. Blacksburg, Va: Center for Composite Materials and Structures, College of Engineering, Virginia Polytechnic Institute and State University, 1991.

Gabriel, Cederbaum, ed. Random vibration and reliability of composite structures. Lancaster, Pa: Technomic Pub. Co., 1992.

Kreja, Ireneusz. Geometrically non-linear analysis of layered composite plates and shells. Gdańsk: Wydawn. Politechniki Gdańskiej, 2007.

Simitses, George J. Buckling of delaminated shells and multi-annular plates. Atlanta, Ga: Georgia Institute of Technology, School of Engineering Science and Mechanics, 1985.

Engineering mechanics of composite structures. Boca Raton: CRC Press, 1993.

1945-, Reddy J. N., ed. Mechanics of laminated composite plates and shells: Theory and analysis. 2nd ed. Boca Raton: CRC Press, 2004.

Dutta, Piyush K. Buckling of unidirectional graphite/epoxy composite plates at low temperatures. Hanover, N. H: U.S. Army Cold Regions Research and Engineering Laboratory, 1991.

Chen, Jiye. The analysis of transient dynamic response of composite laminated plates. Birmingham: University of Birmingham, 1997.

Carper, Douglas M. Large deformation behavior of long shallow cylindrical composite panels. Hampton, Va: Langley Research Center, 1991.

Hodges, Dewey H. Modeling of composite beams and plates for static and dynamic analysis. Atlanta, Ga: School of Aerospace Engineering, Georgia Institute of Technology, 1990.

United States. National Aeronautics and Space Administration., ed. Modeling of composite beams and plates for static and dynamic analysis. [Washington, DC: National Aeronautics and Space Administration, 1993.

John, Morton, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Design and application of a quasistatic crush test fixture for investigating scale effects in energy absorbing composite plates. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

H, Starnes James, Prasad Chunchu B, and Langley Research Center, eds. Influence of transverse-shear and large-deformation effects on the low-speed impact response of laminated composite plates. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.

H, Starnes James, Prasad Chunchu B, and Langley Research Center, eds. Influence of transverse-shear and large-deformation effects on the low-speed impact response of laminated composite plates. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.

H, Starnes James, Prasad Chunchu B, and Langley Research Center, eds. Influence of transverse-shear and large-deformation effects on the low-speed impact response of laminated composite plates. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.

G, Rojas R., and Langley Research Center, eds. Electromagnetic on-aircraft antenna radiation in the presence of composite plates. Columbus, Ohio: The Ohio State University, ElectroScience Laboratory, Dept. of Electrical Engineering, 1994.

G, Rojas R., and Langley Research Center, eds. Electromagnetic on-aircraft antenna radiation in the presence of composite plates. Columbus, Ohio: The Ohio State University, ElectroScience Laboratory, Dept. of Electrical Engineering, 1994.

Al-Obeid, Askram. Vibration and buckling of laminated composite plates with various boundary conditions. Manchester: University of Manchester, 1993.

G, Rojas R., and Langley Research Center, eds. Electromagnetic on-aircraft antenna radiation in the presence of composite plates. Columbus, Ohio: The Ohio State University, ElectroScience Laboratory, Dept. of Electrical Engineering, 1994.

R, Johnson Eric, Starnes James H, and United States. National Aeronautics and Space Administration., eds. Nonlinear response and failure characteristics of internally pressurized composite cylindrical panels. Blacksburg, VA: College of Engineering, Virginia Polytechnic Institute and State University, 1985.

American Society of Mechanical Engineers. Winter Meeting. Vibration and behavior of composite structures, presented at the Winter Annual Meeting of the American Society of Mechanical Engineers, San Francisco, California, December 10-15, 1989. New York, N.Y: American Society of Mechanical Engineers, 1989.

Wang, Shemin. The use of spline functions in the analysis of composite laminated plates. Birmingham: University of Birmingham, 1990.

Prosser, William H. The propogation characteristics of the plate modes of acoustic emission waves in thin aluminium plates and thin graphite/epoxy composite plates and tubes. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.