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1

International Conference on Composite Interfaces (2nd 1988 Cleveland, Ohio). Interfaces in polymer, ceramic and metal matrix composites. Edited by Ishida Hatsuo. London: Elsevier, 1988.

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2

1938-, Dhingra Ashok K., Fishman Steven G, Metallurgical Society-American Society of Metals Composite Committee., and Metallurgical Society of AIME. Meeting, eds. Interfaces in metal-matrix composites: Proceedings of a symposium. Warrendale, PA: Metallurgical Society, 1986.

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3

S, Jacobson Nathan, and 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.

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4

L, Walter John, King Alexander H. 1954-, Tangri Kris, and ASM International, eds. Structure & property relationships for interfaces. [Materials Park, Ohio]: ASM International, 1991.

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5

Naik, Rajiv A. Fracture mechanics analysis for various fiber/matrix interface loadings. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.

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6

Li, Yinghai. EDS in TEM: (1) artefacts (2) application to SiC and ceramic matrix interfaces. Birmingham: University of Birmingham, 1993.

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7

Murthy, 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.

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8

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

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9

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

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10

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. [Washington, D.C: National Aeronautics and Space Administration, 1996.

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11

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. [Washington, D.C: National Aeronautics and Space Administration, 1995.

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12

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

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13

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

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14

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

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15

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

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16

Bansal, 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.

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17

Bansal, 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.

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18

Bansal, 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.

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19

Asthana, 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.

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20

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. New York: Elsevier, 1988.

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21

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.

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22

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. Hampton, Va: National Aeronautics and Space Administration, 1996.

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23

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. Hampton, Va: National Aeronautics and Space Administration, 1996.

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24

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

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25

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

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26

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. [Washington, D.C.]: National Aeronautics and Space Administration, 1991.

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27

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. [Washington, DC: National Aeronautics and Space Administration, 1995.

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28

Spragg, CJ, and 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.

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29

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.

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30

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.

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31

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. [Washington, DC: National Aeronautics and Space Administration, 1994.

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32

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. [Washington, DC: National Aeronautics and Space Administration, 1994.

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33

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

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34

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.

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35

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.

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36

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.

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37

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.

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38

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. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1994.

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39

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. Washington, DC: National Aeronautics and Space Administration, 1995.

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40

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

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41

Interfacce della materia: Esperienze progettuali, sedie e comportamenti = The interfaces of material : design experiments, chairs and behavior. Milano: Domus Academy, 1991.

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42

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

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43

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

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44

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

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45

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

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46

Naik, 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.

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47

Naik, 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.

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48

H, Crews John, and 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.

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49

A, Leckie Frederick, and 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.

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50

Saha, 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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