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1

Huang, Lujun, and Lin Geng. Discontinuously Reinforced Titanium Matrix Composites. Singapore: Springer Singapore, 2017. http://dx.doi.org/10.1007/978-981-10-4449-6.

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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

Johnson, S., J. Larsen, and B. Cox, eds. Life Prediction Methodology for Titanium Matrix Composites. 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959: ASTM International, 1996. http://dx.doi.org/10.1520/stp1253-eb.

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5

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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6

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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7

Johnson, W. S. Damage development in titanium metal matrix composites subjected to cyclic loading. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

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8

Ding, Wei. Modelling and experimental studies of damage in titanium metal matrix composites. Birmingham: University of Birmingham, 1997.

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9

Ibbotson, Andrew Robert. Fatigue crack growth in continuous fibre reinforced titanium alloy matrix composites. Birmingham: University of Birmingham, 1994.

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10

Castelli, Michael G. Thermomechanical and isothermal fatigue behavior of a (90) titanium matrix composite. Cleveland, Ohio: Lewis Research Center, National Aeronautics and Space Administration, 1993.

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11

Naik, Rajiv A. Observations of fatigue crack initiation and damage growth in notched titanium matrix composites. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

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12

Ltjering, G. Titanium. Berlin: Springer, 2003.

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13

Brown, Andrew. A microstructural examination of the bond in titanium-based, continuous-fibre, metal matrix composites. Birmingham: University of Birmingham, 1990.

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14

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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15

Dore, Amanda Louise. Effects of fibre volume fraction on tensile damage and fatigue crack growth in Titanium metal matrix composites. Birmingham: University of Birmingham, 1997.

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16

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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17

Castelli, Michael G. Isothermal damage and fatigue behavior and SCS-6/timetal 21S [0/90]s composite at 650C̊. [Washington, DC]: National Aeronautics and Space Administration, 1994.

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18

Titanium Matrix Composites: Mechanical Behavior. CRC, 1997.

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19

Mall, Shankar, and Ted Nichols. Titanium Matrix Composites: Mechanical Behavior. Taylor & Francis Group, 2020.

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20

Mall, Shankar, and Ted Nichols. Titanium Matrix Composites: Mechanical Behavior. Taylor & Francis Group, 2020.

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21

Shankar, Mall, and Nicholas T, eds. Titanium matrix composites: Mechanical behavior. Lancaster, Pa: Technomic Pub. Co. Inc., 1998.

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22

Mall, Shankar, and Ted Nichols. Titanium Matrix Composites: Mechanical Behavior. Taylor & Francis Group, 2020.

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23

Mall, Shankar, and Ted Nichols. Titanium Matrix Composites: Mechanical Behavior. Taylor & Francis Group, 2020.

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24

T, Herakovich Carl, Pindera M. J, and Langley Research Center, eds. Inelastic deformation of metal matrix composites. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.

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25

S, Johnson W., Larsen James M, and Cox B. N, eds. Life prediction methodology for titanium matrix composites. West Conshohocken, PA: ASTM, 1996.

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26

S, Johnson W., and Langley Research Center, eds. Effect of fiber-matrix debonding on notched strength of titanium metal matrix composites. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.

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27

S, Johnson W., and Langley Research Center, eds. Effect of fiber-matrix debonding on notched strength of titanium metal matrix composites. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.

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28

S, Johnson W., and Langley Research Center, eds. Effect of fiber-matrix debonding on notched strength of titanium metal matrix composites. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.

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29

A, Bahei-El-Din Y., Mirdamadi M, and Langley Research Center, eds. Time-dependent deformation of titanium metal matrix composites. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

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30

Time-dependent deformation of titanium metal matrix composites. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

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31

A, Bahei-El-Din Y., Mirdamadi M, and Langley Research Center, eds. Time-dependent deformation of titanium metal matrix composites. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

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32

S, Johnson W., and Langley Research Center, eds. Implementation of thermal residual stresses in the analysis of fiber bridged matrix crack growth in titanium matrix composites. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.

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33

Monitoring damage growth in titanium matrix composites using acoustic emission. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.

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34

H, Prosser W., Johnson W. S, and Langley Research Center, eds. Monitoring damage growth in titanium matrix composites using acoustic emission. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.

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35

S, Johnson W., and Langley Research Center, eds. Modeling fatigue crack growth in cross ply titanium matrix composites. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.

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36

Orthorhombic Titanium Aluminide Metal Matrix Composites (O TMS's) - A review. Storming Media, 1999.

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37

M, Mirdamadi, and Langley Research Center, eds. Analysis of thermomechanical fatigue of unidirectional titanium metal matrix composites. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.

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38

Geng, Lin, and Lujun Huang. Discontinuously Reinforced Titanium Matrix Composites: Microstructure Design and Property Optimization. Springer, 2018.

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39

S, Johnson W., and Langley Research Center, eds. A methodology to predict damage initiation, damage growth and residual strength in titanium matrix composites. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.

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40

S, Johnson W., Bigelow C. A, and Langley Research Center, eds. Fatigue damage in cross-ply titanium metal matrix composites containing center holes. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

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41

Fatigue damage in cross-ply titanium metal matrix composites containing center holes. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

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42

Fatigue damage in cross-ply titanium metal matrix composites containing center holes. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

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43

Application of fiber bridging models to fatigue crack growth in unidirectional titanium matrix composites. [Washington, DC: National Aeronautics and Space Administration, 1992.

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44

S, Johnson W., and United States. National Aeronautics and Space Administration., eds. Application of fiber bridging models to fatigue crack growth in unidirectional titanium matrix composites. [Washington, DC: National Aeronautics and Space Administration, 1992.

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45

M, Mirdamadi, and Langley Research Center, eds. Analysis of the thermomechanical fatigue of unidirectional titanium metal matrix composites. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.

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46

Modeling and life prediction methodology for titanium matrix composites subjected to mission profiles. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.

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47

Modeling and life prediction methodology for titanium matrix composites subjected to mission profiles. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.

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48

High temperature composites. [Washington, DC]: National Aeronautics and Space Administration, 1995.

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49

Froes, F. H. Recent Advances in Titanium Metal Matrix Composites: Proceedings of a Symposium Held During Materials Week, Oct 2-6 1994, in Rosemont, Illinois. Minerals, Metals, & Materials Society, 1995.

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50

H, Froes F., Storer J, and Materials Week '94 (1994 : Rosemont, Ill.)., eds. Recent advances in titanium metal matrix composites: Proceedings of a symposium held during Materials Week, October 2-6, 1994, in Rosemont, Illinois. Warrendale, Pa: TMS, 1995.

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