Livros sobre o tema "Matrix interfaces"
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International Conference on Composite Interfaces (2nd 1988 Cleveland, Ohio). Interfaces in polymer, ceramic and metal matrix composites. Editado por Ishida Hatsuo. London: Elsevier, 1988.
Encontre o texto completo da fonte1938-, Dhingra Ashok K., Fishman Steven G, Metallurgical Society-American Society of Metals Composite Committee. e Metallurgical Society of AIME. Meeting, eds. Interfaces in metal-matrix composites: Proceedings of a symposium. Warrendale, PA: Metallurgical Society, 1986.
Encontre o texto completo da fonteS, Jacobson Nathan, e United States. National Aeronautics and Space Administration., eds. Chemical status of the fiber coating/matrix interface in silicon-based ceramic matrix composites. Washington, DC: National Aeronautics and Space Administration, 1995.
Encontre o texto completo da fonteL, Walter John, King Alexander H. 1954-, Tangri Kris e ASM International, eds. Structure & property relationships for interfaces. [Materials Park, Ohio]: ASM International, 1991.
Encontre o texto completo da fonteNaik, Rajiv A. Fracture mechanics analysis for various fiber/matrix interface loadings. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.
Encontre o texto completo da fonteLi, Yinghai. EDS in TEM: (1) artefacts (2) application to SiC and ceramic matrix interfaces. Birmingham: University of Birmingham, 1993.
Encontre o texto completo da fonteMurthy, Pappu L. N. Probabilistic micromechanics and macromechanics for ceramic matrix composites. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1997.
Encontre o texto completo da fonteA, Bahei-El-Din Y., Mirdamadi M e Langley Research Center, eds. Time-dependent deformation of titanium metal matrix composites. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.
Encontre o texto completo da fonteA, Bahei-El-Din Y., Mirdamadi M e Langley Research Center, eds. Time-dependent deformation of titanium metal matrix composites. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.
Encontre o texto completo da fonteM, Arnold Steven, e United States. National Aeronautics and Space Administration., eds. Critique of macro flow/damage surface representations for metal matrix composites using micromechanics. [Washington, D.C: National Aeronautics and Space Administration, 1996.
Encontre o texto completo da fontePete, Kantzos, Telesman Jack e United States. National Aeronautics and Space Administration., eds. Fatigue crack growth and crack bridging in SCS-6/Ti-24-11. [Washington, D.C: National Aeronautics and Space Administration, 1995.
Encontre o texto completo da fonteBansal, Narottam P. Strong and tough Hi-Nicalon fiber-reinforced celsian matrix composites. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1997.
Encontre o texto completo da fonteBansal, Narottam P. Strong and tough Hi-Nicalon fiber-reinforced celsian matrix composites. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1997.
Encontre o texto completo da fonteBansal, Narottam P. Strong and tough Hi-Nicalon fiber-reinforced celsian matrix composites. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1997.
Encontre o texto completo da fonteBansal, Narottam P. Strong and tough hi-nicalon fiber-reinforced celsian matrix composites. Cleveland, Ohio: Lewis Research Center, 1997.
Encontre o texto completo da fonteBansal, Narottam P. Effects of fiber/matrix interface and its composition on mechanical properties of Hi-Nicalon/celsian composites. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.
Encontre o texto completo da fonteBansal, Narottam P. Effects of fiber/matrix interface and its composition on mechanical properties of Hi-Nicalon/celsian composites. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.
Encontre o texto completo da fonteBansal, Narottam P. Effects of fiber/matrix interface and its composition on mechanical properties of Hi-Nicalon/celsian composites. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.
Encontre o texto completo da fonteAsthana, R. Influence of CR and W alloying on the fiber-matrix interfacial shear strength in cast and directionally solidified sapphire NiAI composites. Washington, DC: National Aeronautics and Space Administration, 1995.
Encontre o texto completo da fonteHatsuo, 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. New York: Elsevier, 1988.
Encontre o texto completo da fonteUnited States. National Aeronautics and Space Administration. e 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.
Encontre o texto completo da fonteS, Salzar Robert, e 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. Hampton, Va: National Aeronautics and Space Administration, 1996.
Encontre o texto completo da fonteS, Salzar Robert, e 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. Hampton, Va: National Aeronautics and Space Administration, 1996.
Encontre o texto completo da fonteDickerson, R. M. Microstructures of BN/SiC coatings on Nicalon fibers. [Washington, DC: National Aeronautics and Space Administration, 1995.
Encontre o texto completo da fonteBansal, Narottam P. CVD silicon carbide monofilament reinforced SrO-Al₂O₃-2SiO₂ (SAS) glass-ceramic composites. [Washington, D.C.]: National Aeronautics and Space Administration, 1995.
Encontre o texto completo da fonteT, Bhatt Ramakrishna, Kiser James D, United States. National Aeronautics and Space Administration. e United States. Army Aviation Systems Command., eds. Investigation of interfacial shear strength in SiC/Si₃N₄ composites. [Washington, D.C.]: National Aeronautics and Space Administration, 1991.
Encontre o texto completo da fonteUnited 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. [Washington, DC: National Aeronautics and Space Administration, 1995.
Encontre o texto completo da fonteSpragg, CJ, e LT Drzal, eds. Fiber, Matrix, and Interface Properties. 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959: ASTM International, 1996. http://dx.doi.org/10.1520/stp1290-eb.
Texto completo da fonte1959-, Spragg Christopher J., Drzal Lawrence T, ASTM Committee D-30 on High Modulus Fibers and Their Composites. e Symposium on Fiber, Matrix, and Interface Properties (1994 : Phoenix, Ariz.), eds. Fiber, matrix, and interface properties. West Conshohocken, Penn: ASTM, 1996.
Encontre o texto completo da fonteJ, Bowles Kenneth, Papadopolous Demetrios S, United States. National Aeronautics and Space Administration. Office of Management. e 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.
Encontre o texto completo da fonteUnited 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. [Washington, DC: National Aeronautics and Space Administration, 1994.
Encontre o texto completo da fonteUnited 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. [Washington, DC: National Aeronautics and Space Administration, 1994.
Encontre o texto completo da fonteAdams, Donald Frederick. Polymer matrix and graphite fiber interface study. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1985.
Encontre o texto completo da fonteV, Pepper Steven, e 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.
Encontre o texto completo da fonteMadhukar, 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.
Encontre o texto completo da fonteJ, Bowles Kenneth, Papadopolous Demetrios S, United States. National Aeronautics and Space Administration. Office of Management. e 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.
Encontre o texto completo da fonteJ, Bowles Kenneth, Papadopolous Demetrios S, United States. National Aeronautics and Space Administration. Office of Management. e 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.
Encontre o texto completo da fonteJ, Bowles Kenneth, Papadopoulos Demetrios S, United States. National Aeronautics and Space Administration. Office of Management. e 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.
Encontre o texto completo da fonteS, Jacobson Nathan, e United States. National Aeronautics and Space Administration., eds. Chemical stability of the fiber coating/matrix interface in silicon-based ceramic matrix composites. Washington, DC: National Aeronautics and Space Administration, 1995.
Encontre o texto completo da fonte1939-, Vigo Tyrone L., e Kinzig Barbara J, eds. Composite applications: The role of matrix, fiber, and interface. New York, N.Y: VCH, 1992.
Encontre o texto completo da fonteInterfacce della materia: Esperienze progettuali, sedie e comportamenti = The interfaces of material : design experiments, chairs and behavior. Milano: Domus Academy, 1991.
Encontre o texto completo da fonteNaik, Rajiv A. Determination of fiber-matrix interface failure parameters from off-axis tests. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.
Encontre o texto completo da fonteNaik, Rajiv A. Determination of fiber-matrix interface failure parameters from off-axis tests. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.
Encontre o texto completo da fonteNaik, Rajiv A. Determination of fiber-matrix interface failure parameters from off-axis tests. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.
Encontre o texto completo da fonteNaik, Rajiv A. Determination of fiber-matrix interface failure parameters from off-axis tests. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.
Encontre o texto completo da fonteNaik, Rajiv A. Closed-form analysis of fiber-matrix interface stresses under thermo-mechanical loadings. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.
Encontre o texto completo da fonteNaik, Rajiv A. Closed-form analysis of fiber-matrix interface stresses under thermo-mechanical loadings. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.
Encontre o texto completo da fonteH, Crews John, e Langley Research Center, eds. Closed-form analysis of fiber-matrix interface stresses under thermo-mechanical loadings. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.
Encontre o texto completo da fonteA, Leckie Frederick, e United States. National Aeronautics and Space Administration., eds. Elasto-plastic analysis of interface layers for fiber reinforced metal matrix composites. [Washington, DC]: National Aeronautics and Space Administration, 1991.
Encontre o texto completo da fonteSaha, Jaydeep. Analysis, Optimization and Control of Grid-Interfaced Matrix-Based Isolated AC-DC Converters. Singapore: Springer Nature Singapore, 2022. http://dx.doi.org/10.1007/978-981-19-4902-9.
Texto completo da fonte