Books on the topic 'Composite Sandwich Structures'

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, 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.

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.

Gopalakrishnan, Srinivasan, and 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.

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.

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

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

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.

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.

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

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

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

M, McGowan David. Compression response of a sandwich fuselage keel panel with and without damage. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

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

C, Smith, Lumban-Tobing F, and Langley Research Center, eds. Analysis of thick sandwich shells with embedded ceramic tiles. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1996.

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.

Y, Rajapakse, Kardomateas George A, American Society of Mechanical Engineers. Applied Mechanics Division., and 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.

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.

H, Jackson Raymond, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Combined-load buckling behavior of metal-matrix composite sandwich panels under different thermal environments. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991.

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

Daniel, Isaac M. Major accomplishments in composite materials and sandwich structures: An anthology of ONR sponsored research. Dordrecht (Germany): Springer, 2009.

Center, Langley Research, ed. Analytic and computational perspectives of multi-scale theory for homogeneous, laminated composite, and sandwich beams and plates. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 2012.

J, Hodge A., Jackson J. R, and George C. Marshall Space Flight Center, eds. The effects of foam thermal protection system on the damage tolerance characteristics of composite sandwich structures for launch vehicles. Huntsville], Ala: National Aeronautics and Space Administration, Marshall Space Flight Center, 2011.

McGowan, David M. Damage characteristics and residual strength of composite sandwaich panels impacted with and without compression loading: Presented at the 39th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, session no. 15--damage tolerance : Long Beach, California, April 20-23, 1998. [Washington, DC: National Aeronautics and Space Administration, 1998.

International Mechanical Engineering Congress and Exposition (2001 New York, N.Y.). Three-dimensional effects in composite and sandwich structures: Presented at the 2001 ASME International Mechanical Engineering Congress and Exposition, November 11-16, 2001, New York, New York. New York, N.Y: American Society of Mechanical Engineers, 2001.

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.

NASA Dryden Flight Research Center., ed. Open-mode debonding analysis of curved sandwich panels subjected to heating and cryogenic cooling on opposite faces. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 1999.

Ko, William L. Open-mode debonding analysis of curved sandwich panels subjected to heating and cryogenic cooling on opposite faces. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 1999.

NASA Dryden Flight Research Center., ed. Open-mode debonding analysis of curved sandwich panels subjected to heating and cryogenic cooling on opposite faces. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 1999.

NASA Dryden Flight Research Center., ed. Open-mode debonding analysis of curved sandwich panels subjected to heating and cryogenic cooling on opposite faces. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 1999.

NASA Dryden Flight Research Center., ed. Open-mode debonding analysis of curved sandwich panels subjected to heating and cryogenic cooling on opposite faces. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 1999.

Center, Langley Research, ed. Aeroelastic sizing for high-speed research (HSR) longitudinal control alternatives project (LCAP). Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 2005.

Ma, Wenguang, and Russell Elkin. Sandwich Structural Composites. Boca Raton: CRC Press, 2021. http://dx.doi.org/10.1201/9781003035374.

Y, Rajapakse, and American Society of Mechanical Engineers. Materials Division., eds. Three-dimensional effects in composite and sandwich structures: Presented at the 2001 ASME International Mechanical Engineering Congress and Exposition, November 11-16, 2001, New York, New York. New York: American Society of Mechanical Engineers, 2001.

Keller, Thomas. Use of fibre reinforced polymers in bridge construction. Zurich, Switzerland: International Association for Bridge and Structural Engineering (IABSE), 2003. http://dx.doi.org/10.2749/sed007.

Carlsson, L. A., and G. A. Kardomateas. Structural and Failure Mechanics of Sandwich Composites. Dordrecht: Springer Netherlands, 2011. http://dx.doi.org/10.1007/978-1-4020-3225-7.

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.

McGowan, David M. Damage characteristics and residual strength of composite sandwich panels impacted with and without compression loading: Presented at the 39th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, session no. 15-damage tolerance : Long Beach, California, April 20-23, 1998. [Washington, DC: National Aeronautics and Space Administration, 1998.

J, Bäcklund, Zenkert D, and Åström B. T, eds. Composites and Sandwich Structures: Proceedings of the Second North European Engineering and Science Conference (NESCO II), Stockholm, Sweden, 22-23 October, 1997. Cradley Heath: Engineering Materials Advisory Services, 1997.

M, Waas Anthony, Whitcomb J. D, American Society of Mechanical Engineers. Aerospace Division., and International Mechanical Engineering Congress and Exposition (2001 : New York, New York), eds. Damage initiation and prediction in composites, sandwich structures and thermal barrier coatings: Presented at the 2001 ASME International Mechanical Engineering Congress and Exposition : November 11-16, 2001, New York, New York. New York, New York: American Society of Mechanical Engineers, 2001.

Castanié, Bruno, Yapa D. S. Rajapakse, and Serge Abrate. Dynamic Failure of Composite and Sandwich Structures. Springer Netherlands, 2016.

Dynamic Failure Of Composite And Sandwich Structures. Springer, 2012.

Behavior of Sandwich Structures of Isotropic and Composite Materials. Routledge, 1999.

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