Livros sobre o tema "Composites avec le graphite"

1964-, Chan H. E., ed. 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., ed. 371 C mechanical properties of graphite/polyimide composites. [Washington, D.C.]: National Aeronautics and Space Administration, 1985.

1928-, Sun C. T., e United States. National Aeronautics and Space Administration., eds. 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., ed. 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 e United States. National Aeronautics and Space Administration., eds. 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 e United States. National Aeronautics and Space Administration., eds. 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, e United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. 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 e United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. 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 e United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. 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, ed. 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, ed. 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., ed. 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, ed. 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, e United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. 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, e United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. 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, e United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. 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., ed. 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., ed. 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, ed. 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, e United States. National Aeronautics and Space Administration. Scientific and Technical Information Program, eds. 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., e Langley Research Center, eds. 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, e Lewis Research Center, eds. Ultrasonic verification of fire wave fronts in unidirectional graphite epoxy composite. Cambridge, Mass: Massachusetts Institute of Technology, 1990.

Center, Lewis Research, ed. 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, ed. 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., ed. 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. e Langley Research Center, eds. 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, ed. 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, e United States. National Aeronautics and Space Administration., eds. 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., ed. 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, ed. 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.