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Livres sur le sujet « Structures composite sandwich architecturée »

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Auteur : Grafiati
Publié le 19 octobre 2024

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1

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

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2

Abrate, Serge, Bruno Castanié et Yapa D. S. Rajapakse, dir. Dynamic Failure of Composite and Sandwich Structures. Dordrecht : Springer Netherlands, 2013. http://dx.doi.org/10.1007/978-94-007-5329-7.

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3

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

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4

Lee, Sung W., dir. Advances in Thick Section Composite and Sandwich Structures. Cham : Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-31065-3.

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5

Daniel, I. M., E. E. Gdoutos et Y. D. S. Rajapakse, dir. Major Accomplishments in Composite Materials and Sandwich Structures. Dordrecht : Springer Netherlands, 2010. http://dx.doi.org/10.1007/978-90-481-3141-9.

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6

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

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7

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

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8

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

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9

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.

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10

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

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11

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

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12

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

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13

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

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14

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.

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15

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., dir. 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.

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16

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., dir. 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.

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17

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.

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18

Center, Langley Research, dir. A higher-order bending theory for laminated composite and sandwich beams. Hampton, Va : National Aeronautics and Space Administration, Langley Research Center, 1997.

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19

Center, Langley Research, dir. A higher-order bending theory for laminated composite and sandwich beams. Hampton, Va : National Aeronautics and Space Administration, Langley Research Center, 1997.

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20

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.

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21

Y, Rajapakse, Kardomateas George A, American Society of Mechanical Engineers. Applied Mechanics Division. et International Mechanical Engineering Congress and Exposition (1999 : Nashville, Tenn.), dir. 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.

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22

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

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23

H, Jackson Raymond, et United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., dir. 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.

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24

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

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25

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

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26

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.

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27

Center, Langley Research, dir. 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.

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28

J, Hodge A., Jackson J. R et George C. Marshall Space Flight Center, dir. 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.

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29

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

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30

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.

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31

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.

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32

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

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33

Nettles, A. T. (Alan T.), Jackson J. R et George C. Marshall Space Flight Center, dir. 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.

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34

NASA Dryden Flight Research Center., dir. 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.

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35

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.

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36

NASA Dryden Flight Research Center., dir. 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.

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37

NASA Dryden Flight Research Center., dir. 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.

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38

NASA Dryden Flight Research Center., dir. 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.

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39

Y, Rajapakse, et American Society of Mechanical Engineers. Materials Division., dir. 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.

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40

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.

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41

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.

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<p>The aim of the present Structural Engineering Document, a state-of-the-art report, is to review the progress made worldwide in the use of fibre rein­forced polymers as structural components in bridges until the end of the year 2000.<p> Due to their advantageous material properties such as high specific strength, a large tolerance for frost and de-icing salts and, furthermore, short installation times with minimum traffic interference, fibre reinforced polymers have matured to become valuable alternative building materials for bridge structures. Today, fibre reinforced polymers are manufactured industrially to semi-finished products and ccimplete structural components, which can be easily and quickly installed or erected on site.<p> Examples of semi-finished products and structural components available are flexible tension elements, profiles stiff in bending and sandwich panels. As tension elements, especially for the purpose of strengthening, strips and sheets are available, as weil as reinforcing bars for concrete reinforcement and prestressing members for internal prestressing or external use. Profiles are available for beams and columns, and sandwich constructions especially for bridge decks. During the manufacture of the structural components fibre-optic sensors for continuous monitoring can be integrated in the materials. Adhesives are being used more and more for joining com­ponents.<p> Fibre reinforced polymers have been used in bridge construction since the mid-1980s, mostly for the strengthening of existing structures, and increas­ingly since the mid-1990s as pilot projects for new structures. In the case of new structures, three basic types of applications can be distinguished: concrete reinforcement, new hybrid structures in combination with traditional construction materials, and all-composite applications, in which the new materials are used exclusively.<p> This Structural Engineering Document also includes application and research recommendations with particular reference to Switzerland.<p> This book is aimed at both students and practising engineers, working in the field of fibre reinforced polymers, bridge design, construction, repair and strengthening.
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42

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

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43

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

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44

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

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45

National Aeronautics and Space Administration (NASA) Staff. Nondestructive Evaluation (Nde) for Inspection of Composite Sandwich Structures. Independently Published, 2019.

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46

Gopalakrishnan, Srinivasan, et Yapa Rajapakse. Blast Mitigation Strategies in Marine Composite and Sandwich Structures. Springer, 2017.

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47

Behavior of Sandwich Structures of Isotropic and Composite Materials. CRC Press LLC, 2018.

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48

Behavior of Sandwich Structures of Isotropic and Composite Materials. CRC Press LLC, 2018.

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49

Vinson, JackR. Behavior of Sandwich Structures of Isotropic and Composite Materials. CRC Press LLC, 2018.

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50

Blast Mitigation Strategies in Marine Composite and Sandwich Structures. Springer, 2018.

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