Bücher zum Thema „Composites avec le graphite“

1964-, Chan H. E., Hrsg. Graphene and graphite materials. Hauppauge. NY: Nova Science Publishers, 2009.

Graves, Michael J. Initiation and extent of impact damage in graphite/epoxy and graphite/PEEK composites. New York: AIAA, 1988.

L, Smith Donald. Properties of three graphite/toughened resin composites. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991.

Vannucci, Raymond D. Graphite/PMR polyimide composites with improved toughness. [Washington, DC]: National Aeronautics and Space Administration, 1985.

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

Gaier, James R. EMI shields made from intercalated graphite composites. [Washington, DC]: National Aeronautics and Space Administration, 1995.

Abel, Phillip B. Ohmic heating of composite candidate graphite-fiber/coating combinations. Cleveland, Ohio: Lewis Research Center, 1993.

Le, Jia-Liang. Graphene nanoplatelet (GNP) reinforced asphalt mixtures: A novel multifunctional pavement material. Washington, DC: IDEA Programs, Transportation Research Board of the National Academies, 2015.

United States. National Aeronautics and Space Administration., Hrsg. 371 C mechanical properties of graphite/polyimide composites. [Washington, D.C.]: National Aeronautics and Space Administration, 1985.

1928-, Sun C. T., und United States. National Aeronautics and Space Administration., Hrsg. Dynamic delamination crack propagation in a graphite/epoxy laminate. [Washington, DC]: National Aeronautics and Space Administration, 1991.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., Hrsg. Ohmic heating of composite candidate graphite-fiber/coating combinations. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

D, Roberts Gary, Papadopoulos Demetrios S und United States. National Aeronautics and Space Administration., Hrsg. The effect of contact stresses in four-point bend testing of graphite/epoxy and graphite/PMR-15 composite beams. [Washington, DC: National Aeronautics and Space Administration, 1992.

D, Roberts Gary, Papadopoulos Demetrios S und United States. National Aeronautics and Space Administration., Hrsg. The effect of contact stresses in four-point bend testing of graphite/epoxy and graphite/PMR-15 composite beams. [Washington, DC: National Aeronautics and Space Administration, 1992.

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

Sohi, Mohsen M. The effect of resin toughness and modulus on compressive failure modes of quasi-isotropic graphite/epoxy laminates. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1986.

Sohi, Mohsen M. The effect of resin toughness and modulus on compressive failure modes of quasi-isotropic graphite/epoxy laminates. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1986.

W, Deaton Jerry, und United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., Hrsg. The interlaminar fracture toughness of woven graphite/epoxy composites. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.

D, Carden Huey, Peters Jeanne M und United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., Hrsg. Free vibrations of thin-walled semicircular graphite-epoxy composites. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

D, Carden Huey, Peters Jeanne M und United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., Hrsg. Free vibrations of thin-walled semicircular graphite-epoxy composites. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

Ankara, Alpay. Effect of post curing process on the properties of graphite/epoxy composites. London: European Office of Aerospace Research and Development, 1985.

Center, Langley Research, Hrsg. Effects of elevated temperature on the viscoplastic modeling of graphite/polymeric composites. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.

Gaier, James R. Technological hurdles to the application of intercalated graphite fibers. Cleveland, Ohio: Lewis Research Center, NASA, 1988.

Gaier, James R. Intercalated graphite fiber composites as EMI shields in aeorspace structures. [Washington, DC]: National Aeronautics and Space Administration, 1990.

Ellis, David L. Thermal conductivity and thermal expansion of graphite fiber/copper matrix composites. [Washington, DC]: National Aeronautics and Space Administration, 1991.

Center, Goddard Space Flight, Hrsg. Hygrothermal properties of composites. Greenbelt, Md: National Aeronautics and Space Administration, Goddard Space Flight Center, 1996.

Slomiani, Maria. Delamination growth in graphite epoxy laminates under compressive loads. [S.l.]: Drexel University, 1985.

Engli, F. R. Ultrasonic non-destructive examination of graphite/epoxy and glass/epoxy composite materials. Toronto: University of Toronto, Institute for Aerospace Studies, 1985.

Fornes, R. E. Effects of high energy radiation on the mechanical properties of epoxy/graphite fiber reinforced composites, covering the period January 1, 1984 - December 31, 1984. [Raleigh, Va.]: North Carolina State University, 1985.

Ellis, David L. Properties of graphite fiber reinforced copper matrix composites for space power applications. [Washington, DC]: NASA National Aeronautics and Space Administration, 1992.

United States. National Aeronautics and Space Administration., Hrsg. The correlation of low-velocity impact resistance of graphite-fiber-reinforced composites with matrix properties. [Washington, D.C: National Aeronautics and Space Administration, 1986.

United States. National Aeronautics and Space Administration, Hrsg. The correlation of low-velocity impact resistance of graphite-fiber-reinforced composites with matrix properties. [Washington, D.C: National Aeronautics and Space Administration, 1986.

D, Buckley John, und United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., Hrsg. Fiber-tex, 1992: The sixth Conference on Advanced Engineering Fibers and Textile Structures for Composites : proceedings of a conference sponsored by the National Aeronautics and Space Administration ... and held in Philadelphia, Pennsylvania, October 27-29, 1992. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

D, Buckley John, und United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., Hrsg. Fiber-tex, 1992: The sixth Conference on Advanced Engineering Fibers and Textile Structures for Composites : proceedings of a conference sponsored by the National Aeronautics and Space Administration ... and held in Philadelphia, Pennsylvania, October 27-29, 1992. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

D, Buckley John, und United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., Hrsg. Fiber-tex, 1992: The sixth Conference on Advanced Engineering Fibers and Textile Structures for Composites : proceedings of a conference sponsored by the National Aeronautics and Space Administration ... and held in Philadelphia, Pennsylvania, October 27-29, 1992. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

United States. National Aeronautics and Space Administration., Hrsg. The correlation of low-velocity impact resistance of graphite-fiber-reinforced composites with matrix properties. [Washington, D.C: National Aeronautics and Space Administration, 1986.

United States. National Aeronautics and Space Administration., Hrsg. The correlation of low-velocity impact resistance of graphite-fiber-reinforced composites with matrix properties. [Washington, D.C: National Aeronautics and Space Administration, 1986.

United States. National Aeronautics and Space Administration, Hrsg. The correlation of low-velocity impact resistance of graphite-fiber-reinforced composites with matrix properties. [Washington, D.C: National Aeronautics and Space Administration, 1986.

D, Buckley John, und United States. National Aeronautics and Space Administration. Scientific and Technical Information Program, Hrsg. Fiber-tex, 1992: The sixth Conference on Advanced Engineering Fibers and Textile Structures for Composites : proceedings of a conference sponsored by the National Aeronautics and Space Administration ... and held in Philadelphia, Pennsylvania, October 27-29, 1992. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

A, Naik R. V., und Langley Research Center, Hrsg. Combinded bearing and bypass loading on a graphite-epoxy laminate. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1986.

Walker, James L. Thermographic qualification of graphite/epoxy instrumentation racks. [Washington, DC: National Aeronautics and Space Administration, 1998.

H, Williams James, und Lewis Research Center, Hrsg. Ultrasonic verification of fire wave fronts in unidirectional graphite epoxy composite. Cambridge, Mass: Massachusetts Institute of Technology, 1990.

Center, Lewis Research, Hrsg. Adjusting measured weight loss of aged graphite fabric/PMR-15 composites. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.

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

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

1954-, Salpekar Satish A., United States. Army Aviation Research and Technology Activity. und Langley Research Center, Hrsg. Scale effects on the transverse tensile strength of graphite epoxy composites. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

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

M, Daniel Isaac, und United States. National Aeronautics and Space Administration., Hrsg. Temperature effects on high strain rate properties of graphite/epoxy composites. [Washington, DC]: National Aeronautics and Space Administration, 1992.

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

United States. National Aeronautics and Space Administration, Hrsg. Differences in interfacial bond strengths of graphite fiber-epoxy resin composites. [Washington, DC: National Aeronautics and Space Administration, 1985.

Gaier, James R. Effect of lightning strike on bromine intercalated graphite fiber/epoxy composites. [Washington, DC]: National Aeronautics and Space Administration, 1991.