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Libros sobre el tema "Epoxy resins – Thermomechanical properties"

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1

Dow, Marvin B. Properties of two composite materials made of toughened epoxy resin and high-strain graphite fiber. National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.

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2

Greenfield, David C. L. The cure characteristics and physical properties of glycidyl-ether epoxy resins. Brunel University, 1988.

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3

Rule, D. L. Low-temperature thermal conductivity of composites: Alumina fiber/epoxy and alumina fiber/PEEK. U.S. Dept. of Commerce, National Institute of Standards and Technology, 1989.

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4

Rule, D. L. Low-temperature thermal conductivity of composites: Alumina fiber/epoxy and alumina fiber/PEEK. U.S. Dept. of Commerce, National Bureau of Standards, 1989.

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5

Rule, D. L. Low-temperature thermal conductivity of composites: Alumina fiber/epoxy and alumina fiber/PEEK. U.S. Dept. of Commerce, National Bureau of Standards, 1989.

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6

Rule, D. L. Low-temperature thermal conductivity of composites: Alumina fiber/epoxy and alumina fiber/PEEK. U.S. Dept. of Commerce, National Institute of Standards and Technology, 1989.

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7

Rule, D. L. Low-temperature thermal conductivity of composites: Alumina fiber/epoxy and alumina fiber/PEEK. U.S. Dept. of Commerce, National Bureau of Standards, 1989.

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8

Evans, R. W. Test report: Fault current through graphite filament reinforced plastic. National Aeronautics and Space Administration, Marshall Space Flight Center, 1997.

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9

Evans, R. W. Design guidelines for shielding effectiveness, current carrying capability, and the enhancement of conductivity of composite materials. National Aeronautics and Space Administration, [George C. Marshall Space Flight Center, 1997.

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10

J, Bowles Kenneth, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. A predictive model for failure properties of thermoset resins. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.

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11

Center, Goddard Space Flight, ed. Thermomechanical properties of polymeric materials and related stresses. National Aeronautics and Space Administration, Goddard Space Flight Center, 1990.

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12

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

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13

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

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14

Zitouni, Faiza. Chemical modification of perfluoropolyether oligomers and effects on compatability and properties of epoxy resins. 1992.

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15

Hamouda, Wael R. Modifications of optical properties of graphite epoxy surfaces by surfactant assisted embedment of mixed oxides: A thesis in chemistry. 1999.

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16

United States. National Aeronautics and Space Administration., ed. Report for period ending July 31, 1985 ... entitled Characterization of the relationship of the cure cycle chemistry to cure cycle processing properties. College of William and Mary, Dept. of Chemistry, 1985.

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17

George C. Marshall Space Flight Center., ed. Design guidelines for shielding effectiveness, current carrying capability, and the enhancement of conductivity of composite materials: Under contract NAS8-39983. National Aeronautics and Space Administration, [George C. Marshall Space Flight Center, 1997.

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