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1

Abdullah, Abu. Machining of aluminium based Metal Matrix Composite (MMC). typescript, 1996.

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2

G, Wadley H. N., and Lewis Research Center, eds. Cost models for MMC manufacturing processes: Tog. National Aeronautics and Space Administration, [Lewis Research Center, 1996.

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3

United States. National Aeronautics and Space Administration., ed. Computer simulation of time-dependent effects for metal matrix composites (MMC) using METCAN. National Aeronautics and Space Administration, 1996.

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4

Coelho, Reginaldo Teixeira. The machinability of aluminium-based SiC reinforced metal matrix composite (MMC) alloy with emphasis on hole production. University of Birmingham, 1995.

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5

S, Majumdar Bhaskar, and United States. National Aeronautics and Space Administration., eds. In-phase thermomechanical fatigue mechanisms in an unidirectional SCS-6/Ti 15-3 MMC. National Aeronautics and Space Administration, 1995.

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6

S, Majumdar Bhaskar, and United States. National Aeronautics and Space Administration., eds. In-phase thermomechanical fatigue mechanisms in an unidirectional SCS-6/Ti 15-3 MMC. National Aeronautics and Space Administration, 1995.

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7

S, Majumdar Bhaskar, and United States. National Aeronautics and Space Administration., eds. In-phase thermomechanical fatigue mechanisms in an unidirectional SCS-6/Ti 15-3 MMC. National Aeronautics and Space Administration, 1995.

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8

B, Gurganus T., Walker J. A. 1939-, and Langley Research Center, eds. Development and characterization of powder metallurgy (PM) 2XXX series Al alloy products and metal matrix composite (MMC 2XXX Al/SiC materials for high temperature aircraft structural applications. National Aeronautics and Space Administration, Langley Research Center, 1992.

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9

Engineers, Society of Automotive, and International Congress and Exposition (1994 : Detroit, Mich.), eds. Metal matrix composites. Society of Automobile Engineers, 1994.

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10

(Firm), Knovel, ed. Composite materials handbook: Metal matrix composites. U.S. Department of Defense, 2002.

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11

Roux, Teresa Le. The machining of a metal matrix composite. University of Birmingham, 1994.

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12

J, Lee H., and United States. National Aeronautics and Space Administration., eds. Metal matrix composite analyzer: METCAN user's manual. 4th ed. National Aeronautics and Space Administration, 1991.

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13

C, Chamis C., and United States. National Aeronautics and Space Administration., eds. METal matrix Composite ANalyzer (METCAN): Theoretical manual. National Aeronautics and Space Administration, 1993.

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14

Brown, Henry Clifton. Fiber shape effects on metal matrix composite behavior. National Aeronautics and Space Administration, 1993.

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15

United States. National Aeronautics and Space Administration., ed. Acousto-ultrasonic decay in metal matrix composite panels. National Aeronautics and Space Administration, 1995.

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16

Jack, Telesman, Kantzos Peter, and United States. National Aeronautics and Space Administration., eds. Fatigue crack growth in unidirectional metal matrix composite. NASA, 1990.

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17

United States. National Aeronautics and Space Administration., ed. Acousto-ultrasonic decay in metal matrix composite panels. National Aeronautics and Space Administration, 1995.

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18

United States. National Aeronautics and Space Administration., ed. Acousto-ultrasonic decay in metal matrix composite panels. National Aeronautics and Space Administration, 1995.

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19

Caruso, John J. Prediction of high temperature metal matrix composite ply properties. National Aeronautics and Space Administration, 1990.

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20

International Conference on Composite Interfaces (2nd 1988 Cleveland, Ohio). Interfaces in polymer, ceramic and metal matrix composites. Edited by Ishida Hatsuo. Elsevier, 1988.

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21

Stephens, Joseph R. High temperature metal matrix composites for future aerospace systems. National Aeronautics and Space Administration, 1987.

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22

Johnson, W. S. Fatigue damage accumulation in various metal matrix composites. National Aeronautics and Space Administration, Langley Research Center, 1987.

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23

Bryant, Richard W. Metal matrix composites: New developments, applications, and markets. Business Communications Co., 1988.

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24

Davim, J. Paulo. Machining of Metal Matrix Composites. Springer-Verlag London Limited, 2012.

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25

Pete, Kantzos, Telesman Jack, and Lewis Research Center, eds. Modeling of crack bridging in a unidirectional metal matrix composite. National Aeronautics and Space Administration, Lewis Research Center, 1991.

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26

A, Naik Rajiv, and Langley Research Center, eds. A macro-mechanics analysis of a notched metal matrix composite. National Aeronautics and Space Administration, Langley Research Center, 1990.

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27

A, Naik Rajiv, and Langley Research Center, eds. A macro-mechanics analysis of a notched metal matrix composite. National Aeronautics and Space Administration, Langley Research Center, 1990.

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28

Peter, Kantzos, Telesman Jack, and Lewis Research Center, eds. Modeling of crack bridging in a unidirectional metal matrix composite. National Aeronautics and Space Administration, Lewis Research Center, 1991.

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29

C, Chamis C., and United States. National Aeronautics and Space Administration., eds. A unique set of micromechanics equations for high temperature metal matrix composites. National Aeronautics and Space Administration, 1985.

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30

United States. National Aeronautics and Space Administration., ed. Fatigue life prediction of an intermetallic matrix composite at elevated temperatures. National Aeronautics and Space Administration, 1991.

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31

Center, Langley Research, ed. A Micromechanics-based strength prediction methodology for notched metal matrix composites. National Aeronautics and Space Administration, Langley Research Center, 1992.

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32

Center, Langley Research, ed. A Micromechanics-based strength prediction methodology for notched metal matrix composites. National Aeronautics and Space Administration, Langley Research Center, 1992.

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33

Morel, M. Concurrent micromechanical tailoring and fabrication process optimization for metal-matrix composites. National Aeronautics and Space Administration, 1991.

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34

B, Cantor, Dunne Fionn, Stone Ian, Institute of Physics (Great Britain), and Oxford-Kobe Materials Seminar (3rd : 2000 : Kobe Institute), eds. Metal and ceramic matrix composites: An Oxford-Kobe materials text. IOP Pub., 2004.

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35

Daniel, Trowbridge, Chamis C. C, and United States. National Aeronautics and Space Administration., eds. Finite element applications to explore the effects of partial bonding on metal matrix composite properties. National Aeronautics and Space Administration, 1989.

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36

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

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37

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

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38

Ko, William L. Anomalous buckling characteristics of laminated metal-matrix composite plates with central square holes. National Aeronautics and Space Administration, Dryden Flight Research Center, 1998.

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39

H, Jackson Raymond, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Combined-load buckling behavior of metal-matrix composite sandwich panels under different thermal environments. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991.

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40

E, Tuttle M., and United States. National Aeronautics and Space Administration., eds. An investigation of the thermoviscoplastic behavior of a metal matrix composite at elevated temperatures. National Aeronautics and Space Administration, 1992.

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41

E, Tuttle M., and United States. National Aeronautics and Space Administration., eds. An investigation of the thermoviscoplastic behavior of a metal matrix composite at elevated temperatures. National Aeronautics and Space Administration, 1992.

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42

C, Chamis C., Brown Henry Clifton, and United States. National Aeronautics and Space Administration., eds. Parametric studies to determine the effect of compliant layers on metal matrix composite systems. National Aeronautics and Space Administration, 1990.

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43

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

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44

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. National Aeronautics and Space Administration, 1989.

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45

Ko, William L. Compressive and shear buckling analysis of metal matrix composite sandwich panels under different thermal environments. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

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46

Boardman, Bruce. Metal matrix composites, an opportunity for the off-highway industry: The Third V.F. Braun Lecture. Society of Automotive Engineers, 1990.

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47

A, Lerch Bradley, and United States. National Aeronautics and Space Administration., eds. Evaluation of thermal and mechanical loading effects on the structural behavior of a SiC/titanium composite. NASA, 1990.

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48

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. NASA-UVa light aerospace alloy and structure technology program supplement: Aluminum-based materials for high speed aircraft. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

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49

Center, Langley Research, ed. NASA-UVa light aerospace alloy and structure technology program supplement: Aluminum-based materials for high speed aircraft. National Aeronautics and Space Administration, Langley Research Center, 1997.

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50

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

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