Bücher zum Thema „Structures composite sandwich architecturée“
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Abrate, Serge. Dynamic Failure of Composite and Sandwich Structures. Dordrecht: Springer Netherlands, 2013.
Den vollen Inhalt der Quelle findenAbrate, Serge, Bruno Castanié und Yapa D. S. Rajapakse, Hrsg. Dynamic Failure of Composite and Sandwich Structures. Dordrecht: Springer Netherlands, 2013. http://dx.doi.org/10.1007/978-94-007-5329-7.
Der volle Inhalt der QuelleChamis, C. C. Fiber composite sandwich thermostuctural behavior, computationalsimulation. [Washington, DC]: National Aeronautics and Space Administration, 1986.
Den vollen Inhalt der Quelle findenLee, Sung W., Hrsg. Advances in Thick Section Composite and Sandwich Structures. Cham: Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-31065-3.
Der volle Inhalt der QuelleDaniel, I. M., E. E. Gdoutos und Y. D. S. Rajapakse, Hrsg. Major Accomplishments in Composite Materials and Sandwich Structures. Dordrecht: Springer Netherlands, 2010. http://dx.doi.org/10.1007/978-90-481-3141-9.
Der volle Inhalt der QuelleGopalakrishnan, Srinivasan, und Yapa Rajapakse, Hrsg. Blast Mitigation Strategies in Marine Composite and Sandwich Structures. Singapore: Springer Singapore, 2018. http://dx.doi.org/10.1007/978-981-10-7170-6.
Der volle Inhalt der QuelleCheung, E. W. Buckling of composite sandwich cylinders under axial compression. Amsterdam: Elsevier Science Publishers, 1988.
Den vollen Inhalt der Quelle findenCheung, Eric Waihon. Buckling of composite sandwich cylinders under axial compression. [Downsview, Ont.]: Dept. of Aerospace Science and Engineering, University of Toronto, 1988.
Den vollen Inhalt der Quelle findenSomers, 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.
Den vollen Inhalt der Quelle findenSomers, M. Effect of delamination location on postbuckling behavior of sandwich structures. Haifa, Israel: Technion-Israel Institute of Technology, Faculty of Aerospace Engineering, 1989.
Den vollen Inhalt der Quelle findenR, Ambur Damodar, und Langley Research Center, Hrsg. Damage-tolerance characteristics of composite fuselage sandwich structures with thick facesheets. Hampton, Va: Langley Research Center, 1997.
Den vollen Inhalt der Quelle findenR, Ambur Damodar, und Langley Research Center, Hrsg. Damage-tolerance characteristics of composite fuselage sandwich structures with thick facesheets. Hampton, Va: Langley Research Center, 1997.
Den vollen Inhalt der Quelle findenR, Ambur Damodar, und Langley Research Center, Hrsg. Damage-tolerance characteristics of composite fuselage sandwich structures with thick facesheets. Hampton, Va: Langley Research Center, 1997.
Den vollen Inhalt der Quelle findenWalker, 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.
Den vollen Inhalt der Quelle findenUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Program., Hrsg. 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.
Den vollen Inhalt der Quelle findenUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Program., Hrsg. 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.
Den vollen Inhalt der Quelle findenJegley, 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.
Den vollen Inhalt der Quelle findenCenter, Langley Research, Hrsg. A higher-order bending theory for laminated composite and sandwich beams. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.
Den vollen Inhalt der Quelle findenCenter, Langley Research, Hrsg. A higher-order bending theory for laminated composite and sandwich beams. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.
Den vollen Inhalt der Quelle findenVinson, 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.
Der volle Inhalt der QuelleY, Rajapakse, Kardomateas George A, American Society of Mechanical Engineers. Applied Mechanics Division. und International Mechanical Engineering Congress and Exposition (1999 : Nashville, Tenn.), Hrsg. 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.
Den vollen Inhalt der Quelle findenDaniel, Isaac M. Major accomplishments in composite materials and sandwich structures: An anthology of ONR sponsored research. Dordrecht (Germany): Springer, 2009.
Den vollen Inhalt der Quelle findenH, Jackson Raymond, und United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., Hrsg. 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.
Den vollen Inhalt der Quelle findenKo, William L. Combined-load buckling behavior of metal-matrix composite sandwich panels under different thermal environments. Edwards, Calif: Dryden Flight Research Facility, 1991.
Den vollen Inhalt der Quelle findenMartin, C. Wayne. A three-node C(superscript)0 element for analysis of laminated composite sandwich shells. Edwards, Calif: Ames Research Center, 1989.
Den vollen Inhalt der Quelle findenM, 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.
Den vollen Inhalt der Quelle findenCenter, Langley Research, Hrsg. 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.
Den vollen Inhalt der Quelle findenJ, Hodge A., Jackson J. R und George C. Marshall Space Flight Center, Hrsg. 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.
Den vollen Inhalt der Quelle findenC, Smith, Lumban-Tobing F und Langley Research Center, Hrsg. Analysis of thick sandwich shells with embedded ceramic tiles. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1996.
Den vollen Inhalt der Quelle findenInternational 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.
Den vollen Inhalt der Quelle findenMcGowan, 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.
Den vollen Inhalt der Quelle findenCenter, Langley Research, Hrsg. Aeroelastic sizing for high-speed research (HSR) longitudinal control alternatives project (LCAP). Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 2005.
Den vollen Inhalt der Quelle findenNettles, A. T. (Alan T.), Jackson J. R und George C. Marshall Space Flight Center, Hrsg. 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.
Den vollen Inhalt der Quelle findenNASA Dryden Flight Research Center., Hrsg. 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.
Den vollen Inhalt der Quelle findenKo, 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.
Den vollen Inhalt der Quelle findenNASA Dryden Flight Research Center., Hrsg. 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.
Den vollen Inhalt der Quelle findenNASA Dryden Flight Research Center., Hrsg. 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.
Den vollen Inhalt der Quelle findenNASA Dryden Flight Research Center., Hrsg. 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.
Den vollen Inhalt der Quelle findenY, Rajapakse, und American Society of Mechanical Engineers. Materials Division., Hrsg. 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.
Den vollen Inhalt der Quelle findenMcGowan, 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.
Den vollen Inhalt der Quelle findenKeller, 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.
Der volle Inhalt der QuelleCastanié, Bruno, Yapa D. S. Rajapakse und Serge Abrate. Dynamic Failure of Composite and Sandwich Structures. Springer Netherlands, 2016.
Den vollen Inhalt der Quelle findenDynamic Failure Of Composite And Sandwich Structures. Springer, 2012.
Den vollen Inhalt der Quelle findenBehavior of Sandwich Structures of Isotropic and Composite Materials. Routledge, 1999.
Den vollen Inhalt der Quelle findenNational Aeronautics and Space Administration (NASA) Staff. Nondestructive Evaluation (Nde) for Inspection of Composite Sandwich Structures. Independently Published, 2019.
Den vollen Inhalt der Quelle findenGopalakrishnan, Srinivasan, und Yapa Rajapakse. Blast Mitigation Strategies in Marine Composite and Sandwich Structures. Springer, 2017.
Den vollen Inhalt der Quelle findenBehavior of Sandwich Structures of Isotropic and Composite Materials. CRC Press LLC, 2018.
Den vollen Inhalt der Quelle findenBehavior of Sandwich Structures of Isotropic and Composite Materials. CRC Press LLC, 2018.
Den vollen Inhalt der Quelle findenVinson, JackR. Behavior of Sandwich Structures of Isotropic and Composite Materials. CRC Press LLC, 2018.
Den vollen Inhalt der Quelle findenBlast Mitigation Strategies in Marine Composite and Sandwich Structures. Springer, 2018.
Den vollen Inhalt der Quelle finden