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1

Chung, Deborah D. L. Carbon fiber composites. Boston: Butterworth-Heinemann, 1994.

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2

Rehkopf, Jackie D. Automotive Carbon Fiber Composites. Warrendale, PA: SAE International, 2011. http://dx.doi.org/10.4271/t-124.

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3

Kelly, Vincent. Carbon fiber: Manufacture and applications. Kidlington, Oxford, UK: Elsevier, 2004.

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4

Carolyn, Maciag, and United States. National Aeronautics and Space Administration., eds. Improving the interlaminar shear strength of carbon fiber-epoxy composites through carbon fiber bromination. [Washington, DC: National Aeronautics and Space Administration, 1987.

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5

Carolyn, Maciag, and United States. National Aeronautics and Space Administration., eds. Improving the interlaminar shear strength of carbon fiber-epoxy composites through carbon fiber bromination. [Washington, DC: National Aeronautics and Space Administration, 1987.

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6

Delmonte, John. Technology of carbon and graphite fiber composites. Malabar, Fla: R.E. Krieger Pub. Co., 1987.

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7

Bo, Zhu, ed. Ju bing xi jing ji tan xian wei. Beijing: Ke xue chu ban she, 2011.

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8

I, Harper Sheila, Bascom Willard D, and Langley Research Center, eds. Effects of fiber, matrix, and interphase on carbon fiber compression strength. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.

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9

Veit, Görner, Lower Saxony (Germany). Ministerium für Wissenschaft und Kultur, and CFK-Forschungszentrum Nord, eds. Carbon art. Drochtersen: MCE Verlagsgesellschaft, 2011.

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10

Chilton, J. E. Hybrid fiber-optic-electrochemical carbon monoxide monitor. Washington, D.C: U.S. Dept. of the Interior, Bureau of Mines, 1992.

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11

Beaumont, Peter W. R., Constantinos Soutis, and Alma Hodzic, eds. The Structural Integrity of Carbon Fiber Composites. Cham: Springer International Publishing, 2017. http://dx.doi.org/10.1007/978-3-319-46120-5.

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12

Chilton, J. E. Hybrid fiber-optic-electrochemical carbon monoxide monitor. Washington, D.C: U.S. Dept. of the Interior, Bureau of Mines, 1992.

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13

R, Carpenter C., ed. Hybrid fiber-optic-electrochemical carbon monoxide monitor. Washington, D.C: U.S. Dept. of the Interior, Bureau of Mines, 1992.

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14

Chilton, J. E. Hybrid fiber-optic-electrochemical carbon monoxide monitor. Washington, D.C: U.S. Dept. of the Interior, Bureau of Mines, 1992.

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15

R, Carpenter C., ed. Hybrid fiber-optic-electrochemical carbon monoxide monitor. Washington, D.C: U.S. Dept. of the Interior, Bureau of Mines, 1992.

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16

T, Drzal Lawrence, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office., eds. The surface properties of carbon fibers and their adhesion to organic polymers. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Office, 1987.

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17

Rehkopf, Jackie D. Automotive carbon fiber composites: From evolution to implementation. Warrendale, Pa: SAE International, 2012.

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18

Burrill, Daniel. How to fabricate automotive fiberglass & carbon fiber parts. North Branch, MN: CarTech, 2012.

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19

United States. National Aeronautics and Space Administration., ed. Carbon-rich ceramic composites from ethynyl aromatic precursors. [Washington, DC: National Aeronautics and Space Administration, 1986.

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20

United States. National Aeronautics and Space Administration., ed. Carbon-rich ceramic composites from ethynyl aromatic precursors. [Washington, DC: National Aeronautics and Space Administration, 1986.

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21

United States. National Aeronautics and Space Administration., ed. Carbon-rich ceramic composites from ethynyl aromatic precursors. [Washington, DC: National Aeronautics and Space Administration, 1986.

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22

Hideo, Arakawa, Namekawa Takashi, and United States. National Aeronautics and Space Administration., eds. Reciprocating sliding wear characteristics of copper-carbon fiber composites. Washington, DC: National Aeronautics and Space Administration, 1988.

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23

Monica, Starnes, and National Institute of Standards and Technology (U.S.), eds. Strength and ductility of concrete beams reinforced with carbon FRP and steel. Gaithersburg, MD: U.S. Dept. of Commerce, Technology Administration, National Institute of Standards and Technology, 2001.

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24

Tredway, W. K. Carbon fiber reinforced glass matrix composites for satellite applications. East Hartford, Ct: United Technologies Research Center, 1992.

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25

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. A statistical comparison of two carbon fiber/epoxy fabrication techniques. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991.

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26

Tanso sen'i no saisentan gijutsu: The recent trends of carbon fiber. Tōkyō-to Chiyoda-ku: Shīemushī Shuppan, 2013.

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27

Mohamed, Saiful Bahri, Radzuwan Ab Rashid, Martini Muhamad, and Jailani Ismail. Down Milling Trimming Process Optimization for Carbon Fiber-Reinforced Plastic. Singapore: Springer Singapore, 2019. http://dx.doi.org/10.1007/978-981-13-1804-7.

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28

Keiichi, Kuniya, and United States. National Aeronautics and Space Administration., eds. Application of copper-carbon fiber composites to power semiconductor devices. Washington, DC: National Aeronautics and Space Administration, 1988.

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29

Bansal, Narottam P. Effects of fiber coating composition on mechanical behavior of silicon carbide fiber-reinforced celsian composites. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.

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30

Bansal, Narottam P. Effects of fiber/matrix interface and its composition on mechanical properties of Hi-Nicalon/celsian composites. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

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31

Bansal, Narottam P. Effects of fiber/matrix interface and its composition on mechanical properties of Hi-Nicalon/celsian composites. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

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32

Bansal, Narottam P. Effects of fiber/matrix interface and its composition on mechanical properties of Hi-Nicalon/celsian composites. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

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33

Nettles, A. T. Low temperature mechanical testing of carbon-fiber/epoxy-resin composite materials. Washington, D.C: National Aeronautics and Space Administration, 1996.

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34

R, Gaier James, and Lewis Research Center, eds. Fabrication and resistivity of IBr intercalated vapor-grown carbon fiber composites. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.

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35

J, Biss Emily, and George C. Marshall Space Flight Center., eds. Low temperature mechanical testing of carbon-fiber/epoxy-resin composite materials. Marshall Space Flight Center, Ala: National Aeronautics and Space Administration, George C. Marshall Space Flight Center, 1996.

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36

P, Kosuri Ranga, Bowles Kenneth J, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Monitoring fiber stress during curing of single fiber glass- and graphite-expoxy composites. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1994.

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37

Bennett, James P. Effect of natural flake graphite and carbon fiber additions on the high-temperature properties of dolomite-carbon refractories. Washington, D.C: U.S. Dept. of the Interior, Bureau of Mines, 1989.

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38

P, Bennett James. Effect of natural flake graphite and carbon fiber additions on the high-temperature properties of dolomite-carbon refractories. Washington, DC: Dept. of the Interior, 1989.

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39

Purba, Burt K. Reinforcement of circular concrete columns with carbon fiber reinforced polymer (CFRP) jackets. Halifax, N.S: Nova Scotia CAD/CAM Centre, 1998.

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40

George C. Marshall Space Flight Center., ed. Evaluation of microcracking in two carbon-fiber/epoxy-matrix composite cryogenic tanks. Marshall Space Flight Center, Ala: National Aeronautics and Space Administration, Marshall Space Flight Center, 2001.

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41

C, Maciag, and United States. National Aeronautics and Space Administration., eds. The effect of bromination of carbon fibers on the coefficient of thermal expansion of graphite fiber-epoxy composites. [Washington, D.C.]: National Aeronautics and Space Administration, 1987.

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42

Langley Research Center. ACEE Composites Project Office. and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. NASA/aircraft industry standard specification for graphite fiber/toughened thermoset resin composite material. Washington, D.C: Scientific and Technical Information Branch, 1985.

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43

B, Lease Kevin, and United States. National Aeronautics and Space Administration., eds. Studies of the role of surface treatment and sizing of carbon fiber surfaces on the mechanical properties of composites containing carbon fibers: Final report, Kansas NASA-EPSCoR Program ... [Washington, DC: National Aeronautics and Space Administration, 1996.

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44

S, Sternstein S., Rensselaer Polytechnic Institute. Materials Engineering Dept., and United States. National Aeronautics and Space Administration., eds. A micrographic study of bending failure in five thermoplastic/carbon fiber composite laminates. Trou [i.e. Troy], N.Y: Rensselaer Polytechnic Institute, Materials Engineering Dept., 1987.

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45

United States. National Aeronautics and Space Administration., ed. Ultrasonic inspection of carbon fiber reinforced plastic by means of sample recognition methods. Washington D.C: National Aeronautics and Space Administration, 1985.

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46

Frankland, S. J. V. Analysis of carbon nanotube pull-out from a polymer matrix. Hampton, VA: ICASE, NASA Langley Research Center, 2002.

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47

Frankland, S. J. V. Analysis of carbon nanotube pull-out from a polymer matrix. Hampton, VA: ICASE, NASA Langley Research Center, 2002.

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48

Jang-Kyo, Kim, ed. Carbon nanotubes for polymer reinforcement. Boca Raton, FL: Taylor & Francis, 2011.

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49

1935-, Adams Donald Frederick, and Langley Research Center, eds. Mechanical properties of neat polymer matrix materials and their unidirectional carbon fiber-reinforced composites. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1989.

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50

1935-, Adams Donald Frederick, and Langley Research Center, eds. Mechanical properties of several neat polymer matrix materials and unidirectional carbon-fiber reinforced composites. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1989.

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