Books on the topic 'Matrix interfaces'

M, Arnold Steven, and United States. National Aeronautics and Space Administration., eds. Critique of macro flow/damage surface representations for metal matrix composites using micromechanics. National Aeronautics and Space Administration, 1996.

A, Bahei-El-Din Y., Mirdamadi M, and Langley Research Center, eds. Time-dependent deformation of titanium metal matrix composites. National Aeronautics and Space Administration, Langley Research Center, 1995.

A, Bahei-El-Din Y., Mirdamadi M, and Langley Research Center, eds. Time-dependent deformation of titanium metal matrix composites. National Aeronautics and Space Administration, Langley Research Center, 1995.

Pete, Kantzos, Telesman Jack, and United States. National Aeronautics and Space Administration., eds. Fatigue crack growth and crack bridging in SCS-6/Ti-24-11. National Aeronautics and Space Administration, 1995.

Bansal, Narottam P. Strong and tough Hi-Nicalon fiber-reinforced celsian matrix composites. National Aeronautics and Space Administration, Lewis Research Center, 1997.

Bansal, Narottam P. Strong and tough Hi-Nicalon fiber-reinforced celsian matrix composites. National Aeronautics and Space Administration, Lewis Research Center, 1997.

Bansal, Narottam P. Strong and tough Hi-Nicalon fiber-reinforced celsian matrix composites. National Aeronautics and Space Administration, Lewis Research Center, 1997.

Bansal, Narottam P. Strong and tough hi-nicalon fiber-reinforced celsian matrix composites. Lewis Research Center, 1997.

Asthana, R. Influence of CR and W alloying on the fiber-matrix interfacial shear strength in cast and directionally solidified sapphire NiAI composites. National Aeronautics and Space Administration, 1995.

Bansal, Narottam P. Effects of fiber/matrix interface and its composition on mechanical properties of Hi-Nicalon/celsian composites. National Aeronautics and Space Administration, Glenn Research Center, 1999.

Bansal, Narottam P. Effects of fiber/matrix interface and its composition on mechanical properties of Hi-Nicalon/celsian composites. National Aeronautics and Space Administration, Glenn Research Center, 1999.

Bansal, Narottam P. Effects of fiber/matrix interface and its composition on mechanical properties of Hi-Nicalon/celsian composites. National Aeronautics and Space Administration, Glenn Research Center, 1999.

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. National Aeronautics and Space Administration, 1995.

Hatsuo, Ishida, ed. Interfaces in polymer, ceramic, and metal matrix composites: Proceedings of the Second International Conference on Composite Interfaces (ICCI-II) held June 13-17, 1988, in Cleveland, Ohio, USA. Elsevier, 1988.

S, Salzar Robert, and Langley Research Center, eds. Optimization of residual stresses in MMC's through process parameter control and the use of heterogeneous compensating/complaint interfacial layers: OPTCOMP2 user's guide. National Aeronautics and Space Administration, 1996.

S, Salzar Robert, and Langley Research Center, eds. Optimization of residual stresses in MMC's through process parameter control and the use of heterogeneous compensating/complaint interfacial layers: OPTCOMP2 user's guide. National Aeronautics and Space Administration, 1996.

Dickerson, R. M. Microstructures of BN/SiC coatings on Nicalon fibers. National Aeronautics and Space Administration, 1995.

Bansal, Narottam P. CVD silicon carbide monofilament reinforced SrO-Al₂O₃-2SiO₂ (SAS) glass-ceramic composites. National Aeronautics and Space Administration, 1995.

T, Bhatt Ramakrishna, Kiser James D, United States. National Aeronautics and Space Administration., and United States. Army Aviation Systems Command., eds. Investigation of interfacial shear strength in SiC/Si₃N₄ composites. National Aeronautics and Space Administration, 1991.

United States. National Aeronautics and Space Administration., ed. "Creep of refractory fibers and modeling of metal and ceramic matrix composite creep behavior": (NCC-3-119), project closing report. National Aeronautics and Space Administration, 1995.

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. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1994.

Spragg, CJ, and LT Drzal, eds. Fiber, Matrix, and Interface Properties. ASTM International, 1996. http://dx.doi.org/10.1520/stp1290-eb.

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. ASTM, 1996.

United States. National Aeronautics and Space Administration., ed. Failure analysis of 2-D and 3-D woven composites: Final report, NASA grant NAG-1-1324, September 1, 1991-December 31, 1994. National Aeronautics and Space Administration, 1994.

United States. National Aeronautics and Space Administration., ed. Failure analysis of 2-D and 3-D woven composites: Final report, NASA grant NAG-1-1324, September 1, 1991-December 31, 1994. 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. Lewis Research Center, 1994.

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. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1994.

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. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1994.

J, Bowles Kenneth, Papadopoulos 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. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1994.

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

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

S, Jacobson Nathan, and United States. National Aeronautics and Space Administration., eds. Chemical stability of the fiber coating/matrix interface in silicon-based ceramic matrix composites. National Aeronautics and Space Administration, 1995.

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

Naik, Rajiv A. Determination of fiber-matrix interface failure parameters from off-axis tests. National Aeronautics and Space Administration, Langley Research Center, 1993.

Naik, Rajiv A. Determination of fiber-matrix interface failure parameters from off-axis tests. National Aeronautics and Space Administration, Langley Research Center, 1993.

Naik, Rajiv A. Determination of fiber-matrix interface failure parameters from off-axis tests. National Aeronautics and Space Administration, Langley Research Center, 1993.

Naik, Rajiv A. Determination of fiber-matrix interface failure parameters from off-axis tests. National Aeronautics and Space Administration, Langley Research Center, 1993.

Naik, Rajiv A. Closed-form analysis of fiber-matrix interface stresses under thermo-mechanical loadings. National Aeronautics and Space Administration, Langley Research Center, 1992.

Naik, Rajiv A. Closed-form analysis of fiber-matrix interface stresses under thermo-mechanical loadings. National Aeronautics and Space Administration, Langley Research Center, 1992.

H, Crews John, and Langley Research Center, eds. Closed-form analysis of fiber-matrix interface stresses under thermo-mechanical loadings. National Aeronautics and Space Administration, Langley Research Center, 1992.

A, Leckie Frederick, and United States. National Aeronautics and Space Administration., eds. Elasto-plastic analysis of interface layers for fiber reinforced metal matrix composites. National Aeronautics and Space Administration, 1991.

JFCC International Workshop on Fine Ceramics '98 (1998 Nagoya, Japan). Ceramic material systems with composite structures: Towards optimum interface control and design. American Ceramic Society, 1998.

Saha, Jaydeep. Analysis, Optimization and Control of Grid-Interfaced Matrix-Based Isolated AC-DC Converters. Springer Nature Singapore, 2022. http://dx.doi.org/10.1007/978-981-19-4902-9.

Funn, John V. Creep behavior of the interface region in continuous fiber reinforced metal-matrix composites. Naval Postgraduate School, 1997.