Books on the topic 'Fiber-matrix composite'

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

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

Brown, Henry Clifton. Fiber shape effects on metal matrix composite behavior. [Washington, DC]: National Aeronautics and Space Administration, 1993.

Johnson, W. S. Elastic-plastic stress concentrations around crack-like notches in continuous fiber reinforced metal matrix composites. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1987.

Johnson, W. S. Elastic-plastic stress concentrations around crack-like notches in continuous fiber reinforced metal matrix composites. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1987.

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

Crews, John H. An analysis of fiber-matrix interface failure stresses for a range of ply stress states. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.

Crews, John H. An analysis of fiber-matrix interface failure stresses for a range of ply stress states. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.

Castelli, Michael G. Isothermal damage and fatigue behavior and SCS-6/timetal 21S [0/90]s composite at 650C̊. [Washington, DC]: National Aeronautics and Space Administration, 1994.

Madhukar, Madhu S. Thermo-oxidative stability of graphite/PMR-15 composites: Effect of fiber surface modification on composite shear properties. Cleveland, Ohio: Lewis Research Center, 1994.

King, Joel David. Characterization of the corrosion of a P-130x graphite fiber reinforced 6063 aluminum metal matrix composite. Monterey, Calif: Naval Postgraduate School, 1989.

Tien, John K. Understanding the interdiffusion behavior and determining the long term stability of tungsten fiber reinforced niobium base matrix composite systems: Final report. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1990.

Castelli, Michael G. Thermomechanical testing techniques for high-temperature composites: TMF behavior of SiC(SCS-6)/Ti-15-3. [Washington, D.C.]: NASA, 1990.

Dara, Philip H. Thermoplastic matrix composite processing model. Blacksburg, Va: Virginia Polytechnic Institute and State University, 1985.

Saruhan, Bilge. Oxide-Based Fiber-Reinforced Ceramic-Matrix Composites. Boston, MA: Springer US, 2003. http://dx.doi.org/10.1007/978-1-4615-0319-4.

McDanels, David L. Tungsten fiber reinforced copper matrix composites: A review. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.

Mavinkere Rangappa, Sanjay, Thottyeapalayam Palanisamy Satishkumar, Marta Maria Moure Cuadrado, Suchart Siengchin, and Claudia Barile, eds. Fracture Failure Analysis of Fiber Reinforced Polymer Matrix Composites. Singapore: Springer Singapore, 2021. http://dx.doi.org/10.1007/978-981-16-0642-7.

1959-, Spragg Christopher J., Drzal Lawrence T, ASTM Committee D-30 on High Modulus Fibers and Their Composites., and Symposium on Fiber, Matrix, and Interface Properties (1994 : Phoenix, Ariz.), eds. Fiber, matrix, and interface properties. West Conshohocken, Penn: ASTM, 1996.

1939-, Vigo Tyrone L., and Kinzig Barbara J, eds. Composite applications: The role of matrix, fiber, and interface. New York, N.Y: VCH, 1992.

Fiber shape effects on metal matrix composite behavior. [Washington, DC]: National Aeronautics and Space Administration, 1993.

E, Grady Joseph, and United States. National Aeronautics and Space Administration., eds. Ceramic matrix and resin matrix composites: A comparison. [Washington, DC]: National Aeronautics and Space Administration, 1987.

V, Pepper Steven, and United States. National Aeronautics and Space Administration., eds. Auger analysis of a fiber/matrix interface in a ceramic matrix composite. [Washington, D.C.]: National Aeronautics and Space Administration, 1988.

(Editor), Tyrone Vigo, and Barabara Kinzig (Editor), eds. Composite Applications: The Role of Matrix, Fiber, and Interface. Wiley-VCH, 1992.

A, Lerch Bradley, and United States. National Aeronautics and Space Administration., eds. A preliminary characterization of the tensile and fatigue behavior of tungsten-fiber/waspaloy-matrix composite. [Washington, DC]: National Aeronautics and Space Administration, 1992.

Elastic-plastic stress concentrations around crack-like notches in continuous fiber reinforced metal matrix composites. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1987.

A comparison of fiber effects on polymer matrix composite oxidation. [Washington, DC]: National Aeronautics and Space Administration, 1991.

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.

Center, Langley Research, ed. Standard test evaluation of graphite fiber/resin matrix composite materials for improved toughness. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1987.

D, Noebe Ronald, and United States. National Aeronautics and Space Administration., eds. The role of rapid solidification processing in the fabrication of fiber reinforced metal matrix composites. [Washington, DC]: National Aeronautics and Space Administration, 1989.

1940-, Jones William R., Prahl Joseph M, and United States. National Aeronautics and Space Administration., eds. Design of a unidirectional composite momentum wheel rim. [Washington, DC]: National Aeronautics and Space Administration, 1995.

United States. Army Aviation Research and Technology Activity. and United States. National Aeronautics and Space Administration., eds. Oxidation effects on the mechanical propertiesof SiC fiber-reinforced reaction bonded silicon nitride matrix composites. [Washington, DC]: National Aeronautics and Space Administration, 1989.

A, Naik Rajiv, Lubowinski S. J, and Langley Research Center, eds. An analysis of fiber-matrix interface failure stresses for a range of ply stress states. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.

Fabrication of Ceramic Matrix Composite Tubes Using a Porous Mullite/ Alumina Matrix and Alumina/Mullite Fiber. Storming Media, 2001.

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.

L, Chen J., Sun C. T. 1939-, and Langley Research Center, eds. Micromechanical characterization of nonlinear behavior of advanced polymer matrix composites. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.

Effect of fiber reinforcements on thermo-oxidative stability and mechanical properties of polymer matrix composites. [Washington, DC]: National Aeronautics and Space Administration, 1991.

D, Kiser James, United States. Army Aviation Research and Technology Activity., and United States. National Aeronautics and Space Administration., eds. Matrix density effects on the mechanical properties of SiC/RBSN composites. [Washington, D.C.]: National Aeronautics and Space Administration, 1990.

J, Bowles Kenneth, Papadopolous Demetrios S, United States. National Aeronautics and Space Administration. Office of Management., and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Thermo-oxidative stability of graphite/PMR-15 composites: Effect of fiber surface modification on composite shear properties. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1994.

United States. National Aeronautics and Space Administration. and U.S. Army Research Laboratory., eds. Heat treatment effects on the tensile properties and microstructures of a SiC/RBSN composite in nitrogen. [Washington, D.C.]: National Aeronautics and Space Administration, 1995.

Linda, McCorkle, Ingrahm Linda, and Lewis Research Center, eds. Comparison of graphite fabric reinforced PMR-15 and avimid N composites after long term isothermal aging at various temperatures. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.

Jack, Telesman, Kantzos Peter, and United States. National Aeronautics and Space Administration., eds. Fatigue crack growth in unidirectional metal matrix composite. [Washington, D.C.]: NASA, 1990.

S, Johnson W., and Langley Research Center, eds. Matrix fatigue crack development in a notched continuous fiber SCS-6/Ti-15-3 composite. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

Mechanical characterization and modeling of non-linear deformation and fracture of a fiber reinforced metal matrix composite. [Cleveland, Ohio?]: National Aeronautics and Space Administration, Lewis Research Center, 1991.

Rate dependent stress-strain behavior of advanced polymer matrix composites. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.

Rate dependent stress-strain behavior of advanced polymer matrix composites. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.

Center, Langley Research, ed. Rate dependent stress-strain behavior of advanced polymer matrix composites. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.

United States. National Aeronautics and Space Administration., ed. Elastic-plastic finite element analyses of an unidirectional, 9 vol % tungsten fiber reinforced copper matrix composite. [Washington, DC: National Aeronautics and Space Administration, 1993.

United States. National Aeronautics and Space Administration., ed. Elastic-plastic finite element analyses of an unidirectional, 9 vol % tungsten fiber reinforced copper matrix composite. [Washington, DC: National Aeronautics and Space Administration, 1993.

United States. National Aeronautics and Space Administration., ed. Elastic-plastic finite element analyses of an unidirectional, 9 vol % tungsten fiber reinforced copper matrix composite. [Washington, DC: National Aeronautics and Space Administration, 1993.

United States. National Aeronautics and Space Administration., ed. Elastic-plastic finite element analyses of an unidirectional, 9 vol % tungsten fiber reinforced copper matrix composite. [Washington, DC: National Aeronautics and Space Administration, 1993.