Books on the topic 'Tensile Shear Fracture Strength'
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Consult the top 27 books for your research on the topic 'Tensile Shear Fracture Strength.'
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Center, Langley Research, ed. Test methods for textile composites. National Aeronautics and Space Administration, Langley Research Center, 1994.
Find full textPoon, C. Tensile fracture of notched composite laminates. National Research Council Canada, 1991.
Find full textLarry, Sobel, and Langley Research Center, eds. Novel composites for wing and fuselage applications: Speedy Nonlinear Analysis of Postbuckled Panels in Shear (SNAPPS) : under contract NAS1-18784. National Aeronautics and Space Administration, Langley Research Center, 1997.
Find full textLarry, Sobel, and Langley Research Center, eds. Novel composites for wing and fuselage applications: Speedy Nonlinear Analysis of Postbuckled Panels in Shear (SNAPPS) : under contract NAS1-18784. National Aeronautics and Space Administration, Langley Research Center, 1997.
Find full textHoeven, W. van der. Effect of cooling rate on interlaminar fracture energy and shear strength of APC-2 laminates. National Aerospace Laboratory, 1993.
Find full textMcWilliams, P. C. Estimation of shear strength using fractals as a measure of rock fracture roughness. U.S. Dept. of the Interior, Bureau of Mines, 1993.
Find full textMcWilliams, P. C. Estimation of shear strength using fractals as a measure of rock fracture roughness. U.S. Dept. of the Interior, Bureau of Mines, 1993.
Find full textA, Biaglow James, and United States. National Aeronautics and Space Administration., eds. Rhenium mechanical properties and joining technology. National Aeronautics and Space Administration, 1996.
Find full textA, DiCarlo James, and United States. National Aeronautics and Space Administration., eds. Thermomechanical behavior of advanced SiC fiber multifilament tows. National Aeronautics and Space Administration, 1997.
Find full textMoss, A. C. Fracture characteristics of carbon and aramis unidirectional composites in interlaminar shear and open hole tensile tests. National Aerospace Laboratory, 1986.
Find full textM, Yun H., DiCarlo James A, and United States. National Aeronautics and Space Administration., eds. Creep and rupture strength of an advanced CVD SiC fiber. National Aeronautics and Space Administration, 1997.
Find full textJ, Biss Emily, and George C. Marshall Space Flight Center., eds. Low temperature mechanical testing of carbon-fiber/epoxy-resin composite materials. National Aeronautics and Space Administration, George C. Marshall Space Flight Center, 1996.
Find full textC, Newman J., and Langley Research Center, eds. Analyses of buckling and stable tearing in thin-sheet materials. National Aeronautics and Space Administration, Langley Research Center, 1998.
Find full textMasters, John E. Translaminar fracture toughness of a composite wing skin made of stitched warp-knit fabric: Under contract NAS1-96014. National Aeronautics and Space Administration, Langley Research Center, 1997.
Find full textCenter, Langley Research, ed. Translaminar fracture toughness of a composite wing skin made of stitched warp-knit fabric: Under contract NAS1-96014. National Aeronautics and Space Administration, Langley Research Center, 1997.
Find full textFrancois, Nicot, and Wan Richard, eds. Micromechanics of failure in granular geomaterials. ISTE, 2009.
Find full textFrancois, Nicot, and Wan Richard, eds. Micromechanics of failure in granular geomaterials. ISTE, 2009.
Find full textFrancois, Nicot, and Wan Richard, eds. Micromechanics of failure in granular geomaterials. ISTE, 2009.
Find full textSerikov, Sergey. Impact on impact strength. INFRA-M Academic Publishing LLC., 2024. http://dx.doi.org/10.12737/2161513.
Full textLi, Jian. Simplified data reduction methods for the ECT test for mode III interlaminar fracture toughness. National Aeronautics and Space Administration, Langley Research Center, 1995.
Find full textThe mechanisms of dispersion strengthening and fracture in Al-based XD[superscript TM]alloys. National Aeronautics and Space Administration, Scientific and Technical Information Division, 1990.
Find full textAnalyses of buckling and stable tearing in thin-sheet materials. National Aeronautics and Space Administration, Langley Research Center, 1998.
Find full textBehavior of surface and corner cracks subjected to tensile and bending loads in Ti-6A1-4V alloy. National Aeronautics and Space Administration, Lyndon B. Johnson Space Center, 1990.
Find full textHybrid effect of tensile strength and impact fracture energy of glass fibre/nylon fibre-based hybrid composite materials (from Japan). Institute of Metals, 1987.
Find full textZamirian, Salma, and Mohammad Reza Shirfath. Comparative Study of Mechanical Properties of Zinc Acrylate Epoxy Nanocomposites Reinforced by AL2O3 and Cloisite®30B and Their Mixture : Tensile Strength and Fracture Toughness : A Comparative Study of Mechanical Properties of Zinc Acrylate Epoxy Nanocomposites Reinforced by AL2O3 and Cloisite®30B and Their Mixture: Tensile Strength and Fracture Toughness. Lulu Press, Inc., 2020.
Find full textZydroń, Tymoteusz. Wpływ systemów korzeniowych wybranych gatunków drzew na przyrost wytrzymałości gruntu na ścinanie. Publishing House of the University of Agriculture in Krakow, 2019. http://dx.doi.org/10.15576/978-83-66602-46-5.
Full textThe main objective of this project is to be produce copper reinforced metal matrix composite (MMC) layers using micron sized AlN particles via friction stir processing (FSP) in order to enhance surface mechanical properties. Micro structural evaluation using Optical Microscopy (OM) and Scanning Electron Microscopy (SEM) indicated that an increase in traverse speed and a decrease in rotational speed cause a reduction in the grain size of different groove width (0,0.4,0.8,1.2 mm) of stir zone (SZ) for the specimens friction stir processed (FSPed) without AlN particles. It was found that upon addition of AlN particles, wear properties were improved. This behavior was further supported by SEM images of wear surfaces. Results demonstrated that the micro composite produced by FSP exhibited enhanced wear resistance and higher average friction coefficient in comparison with pure copper. Tensile properties and fracture characteristics of the specimens FSPed with and without AlN particles and pure copper were also evaluated. According to the results, the MMC layer produced by FSP showed higher strength and lower elongation than pure copper while a remarkable elongation was observed for FSPed specimen without AlN particles and been greatly developed by the use of AlN. Association of Scientists, Developers and Faculties, 2016.
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