Libros sobre el tema "Composite and sandwich plate"

Plate and panel structures of isotropic, composite and piezoelectric materials, including sandwich construction. Dordrecht: Springer, 2005.

Vinson, Jack R. Plate and Panel Structures of Isotropic, Composite and Piezoelectric Materials, Including Sandwich Construction. Dordrecht: Springer Netherlands, 2005. http://dx.doi.org/10.1007/1-4020-3111-4.

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

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.

F, 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.

F, 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.

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

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

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

Abrate, 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.

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

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 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.

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

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

Gopalakrishnan, Srinivasan y Yapa Rajapakse, eds. Blast Mitigation Strategies in Marine Composite and Sandwich Structures. Singapore: Springer Singapore, 2018. http://dx.doi.org/10.1007/978-981-10-7170-6.

Toledano, A. A composite plate theory for arbitrary laminate configurations. Arlington, Va: Office of Naval Research, 1985.

Oskooei, Saeid G. A higher order finite element for sandwich plate analysis. Ottawa: National Library of Canada, 1998.

Storakers, Bertil. Nonlinear plate theory applied to delamination in composites. Stockholm, Sweden: The Royal Institute of Technology, Department of Strength of Materials and Solid Mechanics, 1987.

Jungbluth, O. Verbund- und Sandwichtragwerke: Tragverhalten, Feuerwiderstand, Bauphysik. Berlin: Springer-Verlag, 1986.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. Optimization of composite sandwich cover panels subjected to compressive loadings. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991.

The behavior of sandwich structures of isotropic and composite materials. Lancaster, Pa: Technomic Pub. Co., 1999.

D, Vannucci Raymond y United States. National Aeronautics and Space Administration., eds. Mechanical properties characterization of composite sandwich materials intended for space antenna applications. [Washington, DC: National Aeronautics and Space Administration, 1987.

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.

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.

R, Ambur Damodar y Langley Research Center, eds. Damage-tolerance characteristics of composite fuselage sandwich structures with thick facesheets. Hampton, Va: Langley Research Center, 1997.

R, Ambur Damodar y Langley Research Center, eds. Damage-tolerance characteristics of composite fuselage sandwich structures with thick facesheets. Hampton, Va: Langley Research Center, 1997.

R, Ambur Damodar y Langley Research Center, eds. Damage-tolerance characteristics of composite fuselage sandwich structures with thick facesheets. Hampton, Va: Langley Research Center, 1997.

C, Marques Elizabeth R., Lee Samson S, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, Massachusetts Institute of Technology y Lewis Research Center, eds. Modes of vibration on square fiberglass epoxy composite thick plate. [Washington, D.C.?]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

H, Williams James. Modes of vibration on square fiberglass epoxy composite thick plate. [Washington, D.C.?]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

Walker, Sandra P. Evaluation of composite honeycomb sandwich panels under compressive loads at elevated temperatures. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.

Somers, M. Effect of delamination location on postbuckling behavior of sandwich structures. Haifa, Israel: Technion-Israel Institute of Technology, Faculty of Aerospace Engineering, 1989.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. Study of compression-loaded and impact-damaged structurally efficient graphite-thermoplastic trapezoidal-corrugation sandwich and semisandwich panels. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

Jegley, Dawn C. Study of compression-loaded and impact-damaged structurally efficient graphite-thermoplastic trapezoidal-corrugation sandwich and semisandwich panels. Hampton, Va: Langley Research Center, 1992.

Somers, M. Buckling and postbuckling behavior of sandwich structures in the presence of a delamination. Haifa: Technion Israel Institute of Technology, Dept. of Aeronautical Engineering, 1989.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. Study of compression-loaded and impact-damaged structurally efficient graphite-thermoplastic trapezoidal-corrugation sandwich and semisandwich panels. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

Najafi, Ali A. End plate connections and their influence on steel and composite structures. [s.l.]: typescript, 1992.

Y, Rajapakse, Kardomateas George A, American Society of Mechanical Engineers. Applied Mechanics Division. y International Mechanical Engineering Congress and Exposition (1999 : Nashville, Tenn.), eds. Thick composites for load bearing structures: Presented at the 1999 ASME International Mechanical Engineering Congress and Exposition, November 14-19, 1999, Nashville, Tennessee. New York: American Society of Mechanical Engineers, 1999.

United States. National Aeronautics and Space Administration., ed. Development of curved-plate elements for the exact buckling analysis of composite plate assemblies including transverse-shear effects. [Washington, D.C: National Aeronautics and Space Administration, 1997.

McGowan, David Michael. Development of curved-plate elements for the exact buckling analysis of composite plate assemblies including transverse-shear effects. [Washington, D.C: National Aeronautics and Space Administration, 1997.

Center, Langley Research, ed. Development of curved-plate elements for the exact buckling analysis of composite plate assemblies including transverse-shear effects. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

McGowan, David Michael. Development of curved-plate elements for the exact buckling analysis of composite plate assemblies including transverse-shear effects. [Washington, D.C: National Aeronautics and Space Administration, 1997.

McGowan, David Michael. Development of curved-plate elements for the exact buckling analysis of composite plate assemblies including transverse-shear effects. [Washington, D.C: National Aeronautics and Space Administration, 1997.

Center, Langley Research, ed. Development of curved-plate elements for the exact buckling analysis of composite plate assemblies including transverse-shear effects. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

Brown, Nigel D. Aspects of sway frame design and ductility of composite end plate connections. [s.l.]: typescript, 1995.

Facility, Dryden Flight Research, ed. Stress concentration around a small circular hole in the HiMAT composite plate. Edwards, Calif: National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1986.

Ko, William L. Combined-load buckling behavior of metal-matrix composite sandwich panels under different thermal environments. Edwards, Calif: Dryden Flight Research Facility, 1991.

Viita-Aho, Tarvo. A finite element analysis of the response of composite sandwich panels to blast loading. Manchester: UMIST, 1992.