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Books on the topic 'Structural composite elements'

Author: Grafiati

Published: 4 June 2021

Last updated: 8 February 2022

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1

Altenbach, Holm, Johannes Altenbach, and Wolfgang Kissing. Mechanics of Composite Structural Elements. Berlin, Heidelberg: Springer Berlin Heidelberg, 2004. http://dx.doi.org/10.1007/978-3-662-08589-9.

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2

Altenbach, Holm, Johannes Altenbach, and Wolfgang Kissing. Mechanics of Composite Structural Elements. Singapore: Springer Singapore, 2018. http://dx.doi.org/10.1007/978-981-10-8935-0.

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3

Russell, A. T. Foam-reinforced composite structural elements for impactenergyabsorption. Manchester: UMIST, 1994.

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4

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.

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5

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.

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6

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.

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7

Tuhfatullin, Boris. Nonlinear problems of structural mechanics. Methods of optimal design of structures. ru: INFRA-M Academic Publishing LLC., 2021. http://dx.doi.org/10.12737/1201340.

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The textbook discusses methods of optimal design of structures, including methods for minimizing the functions of one and several variables; methods for solving linear and nonlinear programming problems; examples of optimal design of flat steel frames with elements made of rolled and composite I-beams. It is intended for students studying in the specialty 08.05.01 "Construction of unique buildings and structures", undergraduates studying in the training program 08.04.01.24 "Modern technologies of design and construction of buildings and structures", studying the discipline "Nonlinear problems of structural mechanics", as well as for postgraduates of the direction 08.06.01 " Engineering and construction technologies. Construction of buildings and structures", studying the discipline "Construction Mechanics".

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8

Kenel, Albin. Zur Berechnung von Holz/Beton-Verbundkonstruktionen: Entwicklung und Vergleich verschiedener Berechnungsmethoden = Calculation and dimensioning of timber concrete composite structural elements : development and comparison of various methods. Dübendorf: EMPA, Eidgenössische Materialprüfungs- und Forschungsanstalt, Abt. Holz, 2000.

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9

Tenek, Lazarus Teneketzis. Finite element analysis for composite structures. Dordrecht: Kluwer Academic Publishers, 1998.

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10

Tenek, Lazarus Teneketzis. Finite Element Analysis for Composite Structures. Dordrecht: Springer Netherlands, 1998.

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11

Tenek, Lazarus Teneketzis, and John Argyris. Finite Element Analysis for Composite Structures. Dordrecht: Springer Netherlands, 1998. http://dx.doi.org/10.1007/978-94-015-9044-0.

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12

Ellis, J. R. Specimens and reusable fixturing for testing advanced aeropropulsion materials under in-plane biaxial loading. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2001.

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13

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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14

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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15

Gotsis, Pascal K. Progressive fracture of fiber composite build-up structures. [Washington, D.C: National Aeronautics and Space Administration, 1997.

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16

Gotsis, Pascal K. Progressive fracture of fiber composite build-up structures. [Washington, D.C: National Aeronautics and Space Administration, 1995.

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17

Gotsis, Pascal K. Progressive fracture of fiber composite build-up structures. [Washington, D.C: National Aeronautics and Space Administration, 1997.

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18

Gotsis, Pascal K. Progressive fracture of fiber composite build-up structures. [Washington, D.C: National Aeronautics and Space Administration, 1995.

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19

Chamis, C. C. Computational simulation of structural fracture in fiber composites. [Washington, D.C.]: National Aeronautics and Space Administration, 1990.

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20

Link, R. A. Finite element analysis of composite ice resisting walls. Edmonton, Alta., Canada: Dept. of Civil Engineering, University of Alberta, 1992.

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21

Chamis, C. C. Probabilistic simulation of stress concentation in composite laminates. [Washington, DC]: National Aeronautics and Space Administration, 1994.

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22

Chamis, C. C. Probabilistic simulation of stress concentation in composite laminates. [Washington, DC]: National Aeronautics and Space Administration, 1994.

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23

Gotsis, Pascal K. Progressive fracture of fiber composite thin shell structures under internal pressure and axial loads. [Washington, DC]: National Aeronautics and Space Administration, 1996.

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24

Gotsis, Pascal K. Progressive fracture of fiber composite thin shell structures under internal pressure and axial loads. [Washington, DC]: National Aeronautics and Space Administration, 1996.

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25

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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26

Qian, Duan. The development of two dimensional mixed finite elements for bonded joint structures. [Downsview, Ont.]: Aerospace Science and Engineering, 1985.

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27

Salamon, N. J. Analysis for thermo-chemical decomposition of composite structures: Final report. University Park, PA: Pennsylvania State University, College of Engineering, 1995.

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28

Carden, Huey D. Free vibrations of thin-walled semicircular graphite epoxy composite frames. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

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29

Carden, Huey D. Free vibrations of thin-walled semicircular graphite epoxy composite frames. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

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30

Carden, Huey D. Free vibrations of thin-walled semicircular graphite epoxy composite frames. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

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31

Carden, Huey D. Free vibrations of thin-walled semicircular graphite epoxy composite frames. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

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32

Ostachowicz, W. M. Guided waves in structures for SHM: The time-domain spectral element method. Chichester, West Sussex: Wiley, 2012.

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33

Altenbach, Holm, Johannes Altenbach, and Wolfgang Kissing. Mechanics of Composite Structural Elements. Springer, 2018.

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34

Altenbach, Holm, Johannes Altenbach, and Wolfgang Kissing. Mechanics of Composite Structural Elements. Springer, 2018.

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35

Morozov, Evgeny, and Valery V. Vasiliev. Advanced Mechanics of Composite Materials and Structural Elements. Elsevier Science & Technology Books, 2013.

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36

Mechanics of Composite Structural Elements (Foundations of Engineering Mechanics). Springer, 2004.

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37

Wu, Jiing-Kae. Optimization of material damping and stiffness of laminated fiber-reinforced composite structural elements. 1985.

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38

L, Boitnott Richard, Fasanella Edwin L, Langley Research Center, and United States. Army Aviation Systems Command., eds. Behavior of composite/metal aircraft structural elements and components under crash type loads: What are they telling us? Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

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39

L, Boitnott Richard, Fasanella Edwin L, Langley Research Center, and United States. Army Aviation Systems Command., eds. Behavior of composite/metal aircraft structural elements and components under crash type loads: What are they telling us? Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

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40

S, Harrison E., and United States. National Aeronautics and Space Administration, eds. Develop and demonstrate manufacturing processes for fabricating graphite filament reinforced polyimide (Gr/PI) composite structural elements. [Washington, D.C: National Aeronautics and Space Administration, 1985.

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41

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.

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42

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.

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43

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.

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44

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.

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45

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.

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46

Chimenti, Dale, Stanislav Rokhlin, and Peter Nagy. Physical Ultrasonics of Composites. Oxford University Press, 2011. http://dx.doi.org/10.1093/oso/9780195079609.001.0001.

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Physical Ultrasonics of Composites is a rigorous introduction to the characterization of composite materials by means of ultrasonic waves. Composites are treated here not simply as uniform media, but as inhomogeneous layered anisotropic media with internal structure characteristic of composite laminates. The objective here is to concentrate on exposing the singular behavior of ultrasonic waves as they interact with layered, anisotropic materials, materials which incorporate those structural elements typical of composite laminates. This book provides a synergistic description of both modeling and experimental methods in addressing wave propagation phenomena and composite property measurements. After a brief review of basic composite mechanics, a thorough treatment of ultrasonics in anisotropic media is presented, along with composite characterization methods. The interaction of ultrasonic waves at interfaces of anisotropic materials is discussed, as are guided waves in composite plates and rods. Waves in layered media are developed from the standpoint of the "Stiffness Matrix", a major advance over the conventional, potentially unstable Transfer Matrix approach. Laminated plates are treated both with the stiffness matrix and using Floquet analysis. The important influence on the received electronic signals in ultrasonic materials characterization from transducer geometry and placement are carefully exposed in a dedicated chapter. Ultrasonic wave interactions are especially susceptible to such influences because ultrasonic transducers are seldom more than a dozen or so wavelengths in diameter. The book ends with a chapter devoted to the emerging field of air-coupled ultrasonics. This new technology has come of age with the development of purpose-built transducers and electronics and is finding ever wider applications, particularly in the characterization of composite laminates.

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47

London, University of, C. Soutis, G. A. Davies, D. Hitchings, and F. L. Matthews. Finite Element Modelling of Composite Materials and Structures. Woodhead Publishing Ltd, 2000.

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48

Matthews, Frank L., G. A. O. Davies, D. Hitchings, and C. Soutis. Finite Element Modelling of Composite Materials and Structures. CRC, 2000.

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49

Center, Langley Research, ed. Analysis of selected compression splice joint locations in a graphite-epoxy transport wing stub box. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

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50

V, Sankar Bhavani, and Langley Research Center, eds. Micromechanical models for textile structural composites. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

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