Books on the topic 'Notched composite'
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Poon, C. Tensile fracture of notched composite laminates. National Research Council Canada, 1991.
Find full textNaik, Rajiv A. Observations of fatigue crack initiation and damage growth in notched titanium matrix composites. National Aeronautics and Space Administration, Langley Research Center, 1990.
Find full textJohnson, W. S. Elastic-plastic stress concentrations around crack-like notches in continuous fiber reinforced metal matrix composites. National Aeronautics and Space Administration, Langley Research Center, 1987.
Find full textJohnson, W. S. Elastic-plastic stress concentrations around crack-like notches in continuous fiber reinforced metal matrix composites. National Aeronautics and Space Administration, Langley Research Center, 1987.
Find full textCraugh, Linda E. Progressive failure modeling in notched cross-ply fibrous composites. Naval Postgraduate School, 1999.
Find full textWebb, Geoffrey Matthew. The effects of sub-critical damage on the notched strength of carbon fibre composites. National Library of Canada = Bibliothèque nationale du Canada, 1993.
Find full textBakis, Charles E. Fatigue response of notched laminates subjected to tension-compression cyclic loads. Virginia Polytechnic Institute and State University, 1986.
Find full textJohnson, W. S. Fatigue damage growth mechanisms in continuous fiber reinforced titanium matrix composites. National Aeronautics and Space Administration, Langley Research Center, 1990.
Find full textJohnson, W. S. Fatigue damage growth mechanisms in continuous fiber reinforced titanium matrix composites. National Aeronautics and Space Administration, Langley Research Center, 1990.
Find full textJ. C. F. N. van Rijn. Preliminary model for the blunt notch behaviour of fibre metal laminates. National Aerospace Laboratory, 1994.
Find full textJ. C. F. N. van Rijn. The use of composite fracture models to describe the blunt notch behaviour of metal laminates. National Aerospace Laboratory, 1992.
Find full textHarris, C. E. Preliminary report on tests of tensile specimens with a part-through surface notch for a filament wound graphite/epoxy material. National Aeronautics and Space Administration, Langley Research Center, 1985.
Find full textA, Naik Rajiv, and Langley Research Center, eds. A macro-mechanics analysis of a notched metal matrix composite. National Aeronautics and Space Administration, Langley Research Center, 1990.
Find full textA, Naik Rajiv, and Langley Research Center, eds. A macro-mechanics analysis of a notched metal matrix composite. National Aeronautics and Space Administration, Langley Research Center, 1990.
Find full textA macro-mechanics analysis of a notched metal matrix composite. National Aeronautics and Space Administration, Langley Research Center, 1990.
Find full textCenter, Langley Research, ed. A Micromechanics-based strength prediction methodology for notched metal matrix composites. National Aeronautics and Space Administration, Langley Research Center, 1992.
Find full textCenter, Langley Research, ed. A Micromechanics-based strength prediction methodology for notched metal matrix composites. National Aeronautics and Space Administration, Langley Research Center, 1992.
Find full textA progressive damage methodology for residual strength predictions of notched composite panels. National Aeronautics and Space Administration, Langley Research Center, 1998.
Find full textUnited States. National Aeronautics and Space Administration., ed. A study of fiber volume fraction effects in notched unidirectional SCS-6/Ti-15V-3Cr-3Al-3Sn composite. National Aeronautics and Space Administration, 1993.
Find full textS, Johnson W., and Langley Research Center, eds. Matrix fatigue crack development in a notched continuous fiber SCS-6/Ti-15-3 composite. National Aeronautics and Space Administration, Langley Research Center, 1990.
Find full textExperimental observations and finite element analysis of the initiation of fiber microbuckling in notched composite laminates. Center for Mechanics of Composites, Texas A&M University, 1990.
Find full textS, Raju I., O'Brien T. Kevin, and Langley Research Center, eds. Strain-energy-release rate analysis of the end-notched flexure specimen using the finite-element method. National Aeronautics and Space Administration, Langley Research Center, 1987.
Find full textS, Raju I., O'Brien T. Kevin, and Langley Research Center, eds. Strain-energy-release rate analysis of the end-notched flexure specimen using the finite-element method. National Aeronautics and Space Administration, Langley Research Center, 1987.
Find full textS, Raju I., O'Brien T. Kevin, and Langley Research Center, eds. Strain-energy-release rate analysis of the end-notched flexure specimen using the finite-element method. National Aeronautics and Space Administration, Langley Research Center, 1987.
Find full textL, Bradley Walter, and United States. National Aeronautics and Space Administration., eds. Experimental observations and finite element analysis of the initiation of fiber microbuckling in notched composite laminates: An annual progress report. Center for Mechanics of Composites, Texas A&M University, 1989.
Find full textElastic-plastic stress concentrations around crack-like notches in continuous fiber reinforced metal matrix composites. National Aeronautics and Space Administration, Langley Research Center, 1987.
Find full textCenter, Langley Research, ed. Fracture analysis of notched composites. National Aeronautics and Space Administration, Langley Research Center, 1985.
Find full textCenter, Langley Research, ed. Analysis of notched metal matrix composites under tension loading. National Aeronautics and Space Administration, Langley Research Center, 1988.
Find full textS, Johnson W., and Langley Research Center, eds. Effect of fiber-matrix debonding on notched strength of titanium metal matrix composites. National Aeronautics and Space Administration, Langley Research Center, 1991.
Find full textS, Johnson W., and Langley Research Center, eds. Effect of fiber-matrix debonding on notched strength of titanium metal matrix composites. National Aeronautics and Space Administration, Langley Research Center, 1991.
Find full textS, Johnson W., and Langley Research Center, eds. Effect of fiber-matrix debonding on notched strength of titanium metal matrix composites. National Aeronautics and Space Administration, Langley Research Center, 1991.
Find full textT, Herakovich Carl, and United States. National Aeronautics and Space Administration, eds. An analytical and experimental study of crack extension in center-notched composites. College of Engineering, Virginia Polytechnic Institute and State University, 1987.
Find full textS, Johnson W., and Langley Research Center, eds. Prediction of matrix fatigue crack initiation in notched SCS-6/Ti-15-3 metal matrix composites. National Aeronautics and Space Administration, Langley Research Center, 1991.
Find full textP, Bansal Narottam, Gyekenyesi John P, and NASA Glenn Research Center, eds. Dependency of shear strength on test rate in SiC/BSAS ceramic matrix composite at elevated temperature. NASA Glenn Research Center, 2003.
Find full textC, Chamis C., and Lewis Research Center, eds. Interlaminar fracture toughness: Three-dimensional finite-element modeling for end-notch and mixed-mode flexure. National Aeronautics and Space Administration, Lewis Research Center, 1985.
Find full textCenter, Langley Research, ed. A progressive damage methodology for residual strength predictions of center-crack tension composite panels. National Aeronautics and Space Administration, Langley Research Center, 1996.
Find full textStrain energy release rates of composite interlaminar end-notch and mixed mode fracture: A subulaminate/ply [i.e. sublaminate/ply] level analysis and a computer code. National Aeronautics and Space Administration, 1987.
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