Książki na temat „Matrix interfaces”
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International Conference on Composite Interfaces (2nd 1988 Cleveland, Ohio). Interfaces in polymer, ceramic and metal matrix composites. Redaktor Ishida Hatsuo. London: Elsevier, 1988.
Znajdź pełny tekst źródła1938-, Dhingra Ashok K., Fishman Steven G, Metallurgical Society-American Society of Metals Composite Committee. i Metallurgical Society of AIME. Meeting, red. Interfaces in metal-matrix composites: Proceedings of a symposium. Warrendale, PA: Metallurgical Society, 1986.
Znajdź pełny tekst źródłaS, Jacobson Nathan, i United States. National Aeronautics and Space Administration., red. Chemical status of the fiber coating/matrix interface in silicon-based ceramic matrix composites. Washington, DC: National Aeronautics and Space Administration, 1995.
Znajdź pełny tekst źródłaL, Walter John, King Alexander H. 1954-, Tangri Kris i ASM International, red. Structure & property relationships for interfaces. [Materials Park, Ohio]: ASM International, 1991.
Znajdź pełny tekst źródłaNaik, Rajiv A. Fracture mechanics analysis for various fiber/matrix interface loadings. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.
Znajdź pełny tekst źródłaLi, Yinghai. EDS in TEM: (1) artefacts (2) application to SiC and ceramic matrix interfaces. Birmingham: University of Birmingham, 1993.
Znajdź pełny tekst źródłaMurthy, 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.
Znajdź pełny tekst źródłaA, Bahei-El-Din Y., Mirdamadi M i Langley Research Center, red. Time-dependent deformation of titanium metal matrix composites. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.
Znajdź pełny tekst źródłaA, Bahei-El-Din Y., Mirdamadi M i Langley Research Center, red. Time-dependent deformation of titanium metal matrix composites. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.
Znajdź pełny tekst źródłaM, Arnold Steven, i United States. National Aeronautics and Space Administration., red. Critique of macro flow/damage surface representations for metal matrix composites using micromechanics. [Washington, D.C: National Aeronautics and Space Administration, 1996.
Znajdź pełny tekst źródłaPete, Kantzos, Telesman Jack i United States. National Aeronautics and Space Administration., red. Fatigue crack growth and crack bridging in SCS-6/Ti-24-11. [Washington, D.C: National Aeronautics and Space Administration, 1995.
Znajdź pełny tekst źródłaBansal, Narottam P. Strong and tough Hi-Nicalon fiber-reinforced celsian matrix composites. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1997.
Znajdź pełny tekst źródłaBansal, Narottam P. Strong and tough Hi-Nicalon fiber-reinforced celsian matrix composites. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1997.
Znajdź pełny tekst źródłaBansal, Narottam P. Strong and tough Hi-Nicalon fiber-reinforced celsian matrix composites. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1997.
Znajdź pełny tekst źródłaBansal, Narottam P. Strong and tough hi-nicalon fiber-reinforced celsian matrix composites. Cleveland, Ohio: Lewis Research Center, 1997.
Znajdź pełny tekst źródłaBansal, 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.
Znajdź pełny tekst źródłaBansal, 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.
Znajdź pełny tekst źródłaBansal, 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.
Znajdź pełny tekst źródłaAsthana, 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.
Znajdź pełny tekst źródłaHatsuo, Ishida, red. 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.
Znajdź pełny tekst źródłaUnited States. National Aeronautics and Space Administration. i U.S. Army Research Laboratory., red. 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.
Znajdź pełny tekst źródłaS, Salzar Robert, i Langley Research Center, red. 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.
Znajdź pełny tekst źródłaS, Salzar Robert, i Langley Research Center, red. 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.
Znajdź pełny tekst źródłaDickerson, R. M. Microstructures of BN/SiC coatings on Nicalon fibers. [Washington, DC: National Aeronautics and Space Administration, 1995.
Znajdź pełny tekst źródłaBansal, Narottam P. CVD silicon carbide monofilament reinforced SrO-Al₂O₃-2SiO₂ (SAS) glass-ceramic composites. [Washington, D.C.]: National Aeronautics and Space Administration, 1995.
Znajdź pełny tekst źródłaT, Bhatt Ramakrishna, Kiser James D, United States. National Aeronautics and Space Administration. i United States. Army Aviation Systems Command., red. Investigation of interfacial shear strength in SiC/Si₃N₄ composites. [Washington, D.C.]: National Aeronautics and Space Administration, 1991.
Znajdź pełny tekst źródłaUnited States. National Aeronautics and Space Administration., red. "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.
Znajdź pełny tekst źródłaSpragg, CJ, i LT Drzal, red. 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.
Pełny tekst źródła1959-, Spragg Christopher J., Drzal Lawrence T, ASTM Committee D-30 on High Modulus Fibers and Their Composites. i Symposium on Fiber, Matrix, and Interface Properties (1994 : Phoenix, Ariz.), red. Fiber, matrix, and interface properties. West Conshohocken, Penn: ASTM, 1996.
Znajdź pełny tekst źródłaJ, Bowles Kenneth, Papadopolous Demetrios S, United States. National Aeronautics and Space Administration. Office of Management. i United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., red. 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.
Znajdź pełny tekst źródłaUnited States. National Aeronautics and Space Administration., red. 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.
Znajdź pełny tekst źródłaUnited States. National Aeronautics and Space Administration., red. 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.
Znajdź pełny tekst źródłaAdams, Donald Frederick. Polymer matrix and graphite fiber interface study. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1985.
Znajdź pełny tekst źródłaV, Pepper Steven, i United States. National Aeronautics and Space Administration., red. Auger analysis of a fiber/matrix interface in a ceramic matrix composite. [Washington, D.C.]: National Aeronautics and Space Administration, 1988.
Znajdź pełny tekst źródłaMadhukar, 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.
Znajdź pełny tekst źródłaJ, Bowles Kenneth, Papadopolous Demetrios S, United States. National Aeronautics and Space Administration. Office of Management. i United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., red. 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.
Znajdź pełny tekst źródłaJ, Bowles Kenneth, Papadopolous Demetrios S, United States. National Aeronautics and Space Administration. Office of Management. i United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., red. 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.
Znajdź pełny tekst źródłaJ, Bowles Kenneth, Papadopoulos Demetrios S, United States. National Aeronautics and Space Administration. Office of Management. i United States. National Aeronautics and Space Administration. Scientific and Technical Information Program, red. 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.
Znajdź pełny tekst źródłaS, Jacobson Nathan, i United States. National Aeronautics and Space Administration., red. Chemical stability of the fiber coating/matrix interface in silicon-based ceramic matrix composites. Washington, DC: National Aeronautics and Space Administration, 1995.
Znajdź pełny tekst źródła1939-, Vigo Tyrone L., i Kinzig Barbara J, red. Composite applications: The role of matrix, fiber, and interface. New York, N.Y: VCH, 1992.
Znajdź pełny tekst źródłaInterfacce della materia: Esperienze progettuali, sedie e comportamenti = The interfaces of material : design experiments, chairs and behavior. Milano: Domus Academy, 1991.
Znajdź pełny tekst źródłaNaik, Rajiv A. Determination of fiber-matrix interface failure parameters from off-axis tests. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.
Znajdź pełny tekst źródłaNaik, Rajiv A. Determination of fiber-matrix interface failure parameters from off-axis tests. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.
Znajdź pełny tekst źródłaNaik, Rajiv A. Determination of fiber-matrix interface failure parameters from off-axis tests. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.
Znajdź pełny tekst źródłaNaik, Rajiv A. Determination of fiber-matrix interface failure parameters from off-axis tests. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.
Znajdź pełny tekst źródłaNaik, 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.
Znajdź pełny tekst źródłaNaik, 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.
Znajdź pełny tekst źródłaH, Crews John, i Langley Research Center, red. Closed-form analysis of fiber-matrix interface stresses under thermo-mechanical loadings. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.
Znajdź pełny tekst źródłaA, Leckie Frederick, i United States. National Aeronautics and Space Administration., red. Elasto-plastic analysis of interface layers for fiber reinforced metal matrix composites. [Washington, DC]: National Aeronautics and Space Administration, 1991.
Znajdź pełny tekst źródłaSaha, 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.
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