Books on the topic 'Carbon fibers polymer composite'

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1

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

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2

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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3

Center, Langley Research, ed. Processing and properties of fiber reinforced polymeric matrix composites: I.IM7/LARC(TM)-PETI-7 polyimide composites. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

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4

Loewy, Robert G. Composite structural materials: Semi-annual progress report, September 30, 1984 through April 30, 1985. Troy, N.Y: Rensselaer Polytechnic Institute, 1985.

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5

Fitzer, Erich. Carbon Fibres and Their Composites: Based on papers presented at the International Conference on Carbon Fibre Applications, Sāo José dos Campos (SP), Brazil, 5-9 December 1983, which was jointly sponsored by the Centro Técnico Aerospacial, the United Nations Industrial Development Organization and the United Nations Financing System for Science and Technology for Development. Berlin, Heidelberg: Springer Berlin Heidelberg, 1985.

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6

1923-, Donnet Jean-Baptiste, ed. Carbon fibers. 3rd ed. New York: Marcel Dekker, 1998.

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7

Center, Langley Research, ed. Interfacial adhesion of carbon fibers. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1987.

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8

Buckley, John D. Carbon-carbon materials and composites. Hampton, Va: Langley Research Center, 1992.

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9

Gaier, James R. Prospects for using carbon-carbon composites for EMI shielding. [Washington, DC]: National Aeronautics and Space Administration, 1991.

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10

Materials Technology Conference (6th 1990 Carbondale, Ill.). Composite-technology. Carbondale, Ill: The Center, 1989.

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11

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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12

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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13

Standage, A. E. High-resistance and raised modulus carbon fibers. Washington DC: National Aeronautics and Space Administration, 1985.

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14

Standage, A. E. High-resistance and raised modulus carbon fibers. Washington DC: National Aeronautics and Space Administration, 1985.

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15

Standage, A. E. High-resistance and raised modulus carbon fibers. Washington DC: National Aeronautics and Space Administration, 1985.

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16

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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17

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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18

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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19

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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20

Scudder, Lawrence Philip. Characterisation and testing of carbon fibre reinforced polymer composites using laser generated ultrasound. [s.l.]: typescript, 1994.

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21

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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22

Eftekhari, Abe. A capacitive technique for real-time monitoring polymer coating thickness on carbon filaments during prepregging process. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

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23

J, Chapman John, and Langley Research Center, eds. A capacitive technique for real-time monitoring polymer coating thickness on carbon filaments during prepregging process. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

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24

Adams, Donald Frederick. Polymer matrix and graphite fiber interface study. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1985.

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25

Cogswell, F. N. Thermoplastic aromatic polymer composites: A study of the structure, processing, and properties of carbon fibre reinforced polyetheretherketone and related materials. Oxford [England]: Butterworth-Heinemann, 1992.

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26

Materials Technology Conference (4th 1987 Carbondale, Ill.). Recent research into carbon-carbon composites: Proceedings of the Fourth Annual Conference on Materials Technology, May 5, 1987. Carbondale, Ill: The Center, 1987.

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27

Pierre, Delhaes, ed. Fibers and composites. London: Taylor & Francis, 2003.

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28

DeVilbiss, T. A. Surface characterization in composite and titanium bonding: Carbon fiber surface treatments for improved adhesion to thermoplastic polymers. Blacksburg, VA: Virginia Polytechnic and State University, 1987.

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29

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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30

Center, Lewis Research, ed. Thermal and mechanical durability of graphite-fiber-reinforced PMR-15 composites. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.

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31

United States. National Aeronautics and Space Administration., ed. Thermal and mechanical durability of graphite-fiber-reinforced PMR-15 composites. [Washington, D.C: National Aeronautics and Space Administration, 1997.

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32

Center, Lewis Research, ed. Thermal and mechanical durability of graphite-fiber-reinforced PMR-15 composites. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.

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33

United States. National Aeronautics and Space Administration., ed. Thermal and mechanical durability of graphite-fiber-reinforced PMR-15 composites. [Washington, D.C: National Aeronautics and Space Administration, 1997.

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34

United States. National Aeronautics and Space Administration., ed. Thermo-oxidative stability studies of PMR-15 polymer matrix composites reinforced with various continuous fibers. [Washington, DC]: National Aeronautics and Space Administration, 1990.

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35

United States. National Aeronautics and Space Administration., ed. Thermo-oxidative stability studies of PMR-15 polymer matrix composites reinforced with various continuous fibers. [Washington, DC]: National Aeronautics and Space Administration, 1990.

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36

United States. National Aeronautics and Space Administration., ed. Composite matrix regenerator for Stirling engines. [Washington, DC]: National Aeronautics and Space Administration, 1997.

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37

H, Shah C., Postyn A. S, and Langley Research Center, eds. Properties of two carbon composite materials using LTM25 epoxy resin. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1996.

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38

H, Shah C., Postyn A. S, and Langley Research Center, eds. Properties of two carbon composite materials using LTM25 epoxy resin. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1996.

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39

Abraham, Thomas. Structural carbon: High performance, high value added. Norwalk, CT: Business Communications Co., 1989.

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40

Center, NASA Glenn Research, ed. The oxidation kinetics of continuous carbon fibers in a cracked ceramic matrix composite. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2001.

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41

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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42

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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43

S, Kaith B., Kaur Inderjeet, and SpringerLink (Online service), eds. Cellulose Fibers: Bio- and Nano-Polymer Composites: Green Chemistry and Technology. Berlin, Heidelberg: Springer-Verlag Berlin Heidelberg, 2011.

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44

United States. National Aeronautics and Space Administration., ed. Rapid prototyping of composite structures: Annual performance report, performance period 7/14/97 to 6/30/98 : NASA LaRC #NLPN 97-620, GT # E25-A55. [Washington, DC: National Aeronautics and Space Administration, 1998.

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45

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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46

Ai Bi Ai, Kabushiki Kaisha., ed. Japan's new materials industries. Tokyo: International Business Information, 1985.

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47

Center, Langley Research, ed. Translaminar fracture toughness of a composite wing skin made of stitched warp-knit fabric: Under contract NAS1-96014. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

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48

Masters, John E. Translaminar fracture toughness of a composite wing skin made of stitched warp-knit fabric: Under contract NAS1-96014. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

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49

Nettles, A. T. (Alan T.), Jackson J. R, and George C. Marshall Space Flight Center, eds. Comparison of open-hole compression strength and compression after impact strength on carbon fiber/epoxy laminates for the Ares I composite interstage. Huntsville], Ala: National Aeronautics and Space Administration, Marshall Space Flight Center, 2011.

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50

ZnO bao mo zhi bei ji qi guang, dian xing neng yan jiu. Shanghai Shi: Shanghai da xue chu ban she, 2010.

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