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1

McDanels, David L. Tungsten fiber reinforced copper matrix composites: A review. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.

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2

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Characterisation of fibre reinforced titanium matrix composites. Neuilly sur Seine, France: AGRD, 1994.

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3

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Characterisation of fibre reinforced titanium matrix composites. Neuilly sur Seine, France: AGARD, 1994.

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4

Grobstein, Toni. Creep behavior of tungsten fiber reinforced niobium metal matrix composites. [Washington, DC]: U.S. Dept. of Energy, Nuclear Energy, Reactor Systems Development and Technology, 1989.

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5

Johnson, W. S. Fatique testing and damage development in continuous fiber reinforced metal matrix composites. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.

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6

A, Leckie Frederick, and United States. National Aeronautics and Space Administration., eds. Elasto-plastic analysis of interface layers for fiber reinforced metal matrix composites. [Washington, DC]: National Aeronautics and Space Administration, 1991.

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7

Funn, John V. Creep behavior of the interface region in continuous fiber reinforced metal-matrix composites. Monterey, Calif: Naval Postgraduate School, 1997.

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8

M, Arnold S., Iyer Saiganesh K, and Lewis Research Center, eds. Flow/damage surfaces for fiber-reinforced metals having different periodic microstructures. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.

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9

Johnson, W. S. Fatigue damage growth mechanisms in continuous fiber reinforced titanium matrix composites. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

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10

Johnson, W. S. Fatigue damage growth mechanisms in continuous fiber reinforced titanium matrix composites. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

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11

A, Leckie Frederick, and Lewis Research Center, eds. Reduction of thermal stresses in continuous fiber reinforced metal matrix composites with interface layers. [Cleveland, Ohio?]: National Aeronautics and Space Administration, Lewis Research Center, 1990.

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12

Tien, John K. Understanding the interdiffusion behavior and determining the long term stability of tungsten fiber reinforced niobium base matrix composite systems: Final report. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1990.

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13

Johnson, W. S. Elastic-plastic stress concentrations around crack-like notches in continuous fiber reinforced metal matrix composites. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1987.

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14

Johnson, W. S. Elastic-plastic stress concentrations around crack-like notches in continuous fiber reinforced metal matrix composites. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1987.

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15

1933-, Richardson David E., and United States. National Aeronautics and Space Administration., eds. Micro-mechanical analysis of damage growth and fracture in discontinuous fiber reinforced metal matrix composites. Clemson, S.C: Dept. of Mechanical Engineering, Clemson University, 1991.

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16

D, Noebe Ronald, and United States. National Aeronautics and Space Administration., eds. The role of rapid solidification processing in the fabrication of fiber reinforced metal matrix composites. [Washington, DC]: National Aeronautics and Space Administration, 1989.

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17

King, Joel David. Characterization of the corrosion of a P-130x graphite fiber reinforced 6063 aluminum metal matrix composite. Monterey, Calif: Naval Postgraduate School, 1989.

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18

M, Arnold S., and NASA Glenn Research Center, eds. The applicability of the generalized method of cells for analyzing discontinuously reinforced composites. Cleveland, Ohio: National Aeronautics and Space Administration, Glenn Research Center, 2001.

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19

1933-, Richardson David E., and United States. National Aeronautics and Space Administration., eds. Micro-mechanical analysis of damage growth and fracture in discontinuous fiber reinforced metal matrix composites: Semi-annual report. Clemson, S.C: Dept. of Mechanical Engineering, Clemson University, 1990.

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20

M, Arnold Steven, and United States. National Aeronautics and Space Administration., eds. Micromechanical modeling of the finite deformation of thermoelastic multiphase composites. [Washington, D.C: National Aeronautics and Space Administration, 1997.

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21

M, Arnold S., and United States. National Aeronautics and Space Administration., eds. Micromechanical modeling of the finite deformation of thermoelastic multiphase composites. [Washington, D.C: National Aeronautics and Space Administration, 1997.

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22

Pursell, John Gareth. Analytical modelling and lifing of continuous fibre reinforced metal matrix composites. Birmingham: University of Birmingham, 1997.

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23

Wittmann, F. H. Durability of Strain-Hardening Fibre-Reinforced Cement-Based Composites (SHCC). Dordrecht: RILEM, 2011.

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24

Barney, Craig. Fatigue crack growth from unbridged defects in continuous fibre reinforced titanium metal matrix composites. Birmingham: University of Birmingham, 1995.

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25

Sweby, Stephen Victor. Fatigue crack growth resistance of as processed and heat treated continuous fibre reinforced titanium based metal matrix composites. Birmingham: University of Birmingham, 1997.

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26

Fiber Reinforced Metal Composites/Jan 1970 Oct 1989/272/Pb90-854258. Natl Technical Information, 1989.

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27

Elasto-plastic analysis of interface layers for fiber reinforced metal matrix composites. [Washington, DC]: National Aeronautics and Space Administration, 1991.

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28

Creep Behavior of the Interface Region in Continuous Fiber Reinforced Metal-Matrix Composites. Storming Media, 1997.

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29

Elastic-plastic stress concentrations around crack-like notches in continuous fiber reinforced metal matrix composites. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1987.

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30

National Aeronautics and Space Administration (NASA) Staff. Micro-Mechanical Analysis of Damage Growth and Fracture in Discontinuous Fiber Reinforced Metal Matrix Composites. Independently Published, 2019.

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31

Mechanical characterization and modeling of non-linear deformation and fracture of a fiber reinforced metal matrix composite. [Cleveland, Ohio?]: National Aeronautics and Space Administration, Lewis Research Center, 1991.

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32

National Aeronautics and Space Administration (NASA) Staff. Mechanical Characterization and Modeling of Non-Linear Deformation and Fracture of a Fiber Reinforced Metal Matrix Composite. Independently Published, 2018.

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33

Manson, S. S., and G. R. Halford. Fatigue and Durability of Metals at High Temperatures. ASM International, 2009. http://dx.doi.org/10.31399/asm.tb.fdmht.9781627083430.

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Fatigue and Durability of Metals at High Temperatures is a repository of knowledge, experience, and insights on high-temperature fatigue and its effect on component lifetime and failure. The first few chapters provide readers with an intuitive understanding of creep and creep-fatigue and how they progress based on time, temperature, and stress. In subsequent chapters, the authors present several fatigue life prediction techniques, comparing them to each other and to experimental test results. The authors focus on a method called strain-range partitioning that breaks stress-strain hysteresis loops into simpler components, the effects of which can be analyzed more easily. Through detailed examples, they show how strain-range partitioning can account for creep-fatigue interactions, multiaxial stresses and strains, temperature gradients, metallurgical and microstructural changes, thermal fatigue, and damage mitigation or “healing” due to sequential loading. The method is also used to examine the cyclic deformation characteristics of various steels and alloys and the obstacles to achieving high-temperature structural durability with fiber-reinforced metal-matrix composites. For information on the print version, ISBN 978-0-87170-718-5, follow this link.
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34

Thomas, Sabu, Kheng Lim Goh, Rangika Thilan De Silva, and Aswathi M. K. Interfaces in Particle and Fibre Reinforced Composites: Current Perspectives on Polymer, Ceramic, Metal and Extracellular Matrices. Elsevier Science & Technology, 2019.

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35

Hildebrand, Martin. The strength of adhesive-bonded joints between fibre-reinforced plastics and metals: Analysis, shape optimization and experiments. 1994.

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36

Hildebrand, Martin. The strength of adhesive-bonded joints between fibre-reinforced plastics and metals: Analysis, shape optimization and experiments. 1994.

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37

Zhao, Xiao-Ling. FRP-Strengthened Metallic Structures. Taylor & Francis Group, 2013.

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38

Zhao, Xiao-Ling. Frp-Strengthened Metallic Structures. Taylor & Francis Group, 2013.

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39

Zhao, Xiao-Ling. FRP-Strengthened Metallic Structures. Taylor & Francis Group, 2013.

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40

Zhao, Xiao-Ling. FRP-Strengthened Metallic Structures. Taylor & Francis Group, 2013.

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41

Zhao, Xiao-Ling. FRP-Strengthened Metallic Structures. Taylor & Francis Group, 2013.

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42

FRP-Strengthened Metallic Structures. Taylor & Francis Group, 2017.

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43

FRP-Strengthened Metallic Structures. Taylor & Francis Group, 2013.

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44

Zhao, Xiao-Ling. FRP-Strengthened Metallic Structures. Taylor & Francis Group, 2013.

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