Books on the topic 'Tensile and compressive composite'
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T, Herakovich Carl, Sykes George F, and Langley Research Center. Applied Materials Branch., eds. Space environmental effects on graphite-epoxy compressive properties and epoxy tensile properties. Applied Materials Branch, National Aeronautics and Space Administration, Langley Research Center, 1987.
Find full textC, Pauly Christopher, Pindera M. J. 1951-, and United States. National Aeronautics and Space Administration., eds. Experimental characterization and micromechanical modeling of woven carbon/copper composites. National Aeronautics and Space Administration, 1997.
Find full textR, Veazie David, Brinson L. Catherine, and Langley Research Center, eds. A comparison of tension and compression creep in a polymeric composite and the effects of physical aging on creep. National Aeronautics and Space Administration, Langley Research Center, 1996.
Find full textHyer, M. W. Innovative design of composite structures: The use of curvilinear fiber format in composite structure design. College of Engineering, Virginia Polytechnic Institute and State University, 1990.
Find full textCenter, Langley Research, ed. Test methods for textile composites. National Aeronautics and Space Administration, Langley Research Center, 1994.
Find full textL, Bradley Walter, Texas A & M University. Mechanics and Materials Center., and United States. National Aeronautics and Space Administration., eds. Micromechanics of compression failures in open hole composite laminates: A report. Mechanics and Materials Center, Texas A&M University, 1987.
Find full textHyer, M. W. Innovative design of composite structures: The use of curvilinear fiber format to improve buckling resistance of composite plates with central circular holes. College of Engineering, Virginia Polytechnic Institute and State University, 1990.
Find full textHyer, M. W. Innovative design of composite structures: The use of curvilinear fiber format to improve buckling resistance of composite plates with central circular holes. College of Engineering, Virginia Polytechnic Institute and State University, 1990.
Find full textHyer, M. W. Innovative design of composite structures: Axisymmetric deformations of unsymmetrically laminated cylinders loaded in axial compression : semiannual status report. College of Engineering, Virginia Polytechnic Institute and State University, 1990.
Find full textHyer, M. W. Innovative design of composite structures: Further studies in the use of a curvilinear fiber format to improve structural efficiency. College of Engineering, Virginia Polytechnic Institute and State University, 1988.
Find full textHyer, M. W. Innovative design of composite structures: Design, manufacturing, and testing of plates utilitzing [sic] curvilinear fiber trajectories : final report for NASA. College of Engineering, Virginia Polytechnic Institute and State University ; Hampton, VA, 1994.
Find full textL, Link Carol, and United States Forest Service, eds. Tensile and compressive MOE of flakeboards. U.S. Forest Service, 1988.
Find full textCarli, Charles G. Tensile and compressive MOE of flakeboards. U.S. Forest Service, 1988.
Find full textPoon, C. Tensile fracture of notched composite laminates. National Research Council Canada, 1991.
Find full textLevon, Minnetyan, and United States. National Aeronautics and Space Administration., eds. Discontinuously stiffened composite panel under compressive loading. National Aeronautics and Space Administration, 1995.
Find full textNational Institute of Standards and Technology (U.S.), ed. Tensile strength of an interlocking composite connection. U.S. Dept. of Commerce, Technology Administration, National Institute of Standards and Technology, 2000.
Find full text1958-, Gabb Timothy Paul, and Lewis Research Center, eds. High temperature tension-compression fatigue behavior of a tungsten copper composite. National Aeronautics and Space Administration, Lewis Research Center, 1991.
Find full text1958-, Gabb Timothy Paul, and Lewis Research Center, eds. High temperature tension-compression fatigue behavior of a tungsten copper composite. National Aeronautics and Space Administration, Lewis Research Center, 1991.
Find full textG, Ifju Peter, and Langley Research Center, eds. Through-the-thickness tensile strength of textile composites. National Aeronautics and Space Administration, Langley Research Center, 1994.
Find full textG, Ifju Peter, and Langley Research Center, eds. Through-the-thickness tensile strength of textile composites. National Aeronautics and Space Administration, Langley Research Center, 1994.
Find full textCenter, Langley Research, ed. Baseline tensile tests of composite materials for LDEF exposure. National Aeronautics and Space Administration, Langley Research Center, 1987.
Find full textCenter, Langley Research, ed. Comparison of the compressive strengths for stitched and toughened composite systems. National Aeronautics and Space Administration, Langley Research Center, 1994.
Find full textF, Saltsman James, and United States. National Aeronautics and Space Administration., eds. Tensile deformation damage in SiC reinforced Ti-15V-3Cr-3Al-3Sn. National Aeronautics and Space Administration, 1991.
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 textUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. Optimization of composite sandwich cover panels subjected to compressive loadings. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991.
Find full textT, Bhatt Ramakrishna, United States. Army Aviation Research and Technology Activity., and United States. National Aeronautics and Space Administration., eds. In-situ x-ray monitoring of damage accumulation in SiC/RBSN tensile specimens. National Aeronautics and Space Administration, 1991.
Find full textT, Bhatt Ramakrishna, United States. Army Aviation Research and Technology Activity., and United States. National Aeronautics and Space Administration., eds. In-situ x-ray monitoring of damage accumulation in SiC/RBSN tensile specimens. National Aeronautics and Space Administration, 1991.
Find full textMoore, Thomas J. Tensile strength of simulated and welded butt joints in W-Cu-composite sheet. Lewis Research Center, 1994.
Find full text1954-, Salpekar Satish A., United States. Army Aviation Research and Technology Activity., and Langley Research Center, eds. Scale effects on the transverse tensile strength of graphite epoxy composites. National Aeronautics and Space Administration, Langley Research Center, 1992.
Find full textAbhisak, Chulya, and United States. National Aeronautics and Space Administration., eds. Acousto-ultrasonic analysis of failure in ceramic matrix composite tensile specimens. National Aeronautics and Space Administration, 1993.
Find full textAbhisak, Chulya, and United States. National Aeronautics and Space Administration., eds. Acousto-ultrasonic analysis of failure in ceramic matrix composite tensile specimens. National Aeronautics and Space Administration, 1993.
Find full textAbhisak, Chulya, and United States. National Aeronautics and Space Administration., eds. Acousto-ultrasonic analysis of failure in ceramic matrix composite tensile specimens. National Aeronautics and Space Administration, 1993.
Find full textAbhisak, Chulya, and United States. National Aeronautics and Space Administration., eds. Acousto-ultrasonic analysis of failure in ceramic matrix composite tensile specimens. National Aeronautics and Space Administration, 1993.
Find full textCenter, Langley Research, ed. Manual for LDEF tensile tests. National Aeronautics and Space Administration, Langley Research Center, 1985.
Find full textWalker, Sandra P. Evaluation of composite honeycomb sandwich panels under compressive loads at elevated temperatures. National Aeronautics and Space Administration, Langley Research Center, 1998.
Find full textCenter, Langley Research, and United States. Army Aviation Systems Command., eds. Mechanical property characterization and impact resistance of selected graphite/PEEK composite materials. National Aeronautics and Space Administration, Langley Research Center, 1991.
Find full textHahn, H. Thomas. Compression failure mechanisms of composite structures. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.
Find full textA, Lerch Bradley, and United States. National Aeronautics and Space Administration., eds. A preliminary characterization of the tensile and fatigue behavior of tungsten-fiber/waspaloy-matrix composite. National Aeronautics and Space Administration, 1992.
Find full text1959-, Gates Thomas S., and Langley Research Center, eds. Thermal/mechanical response of a polymer matrix composite at cryogenic temperatures. National Aeronautics and Space Administration, Langley Research Center, 2003.
Find full text1959-, Gates Thomas S., and Langley Research Center, eds. Thermal/mechanical response of a polymer matrix composite at cryogenic temperatures. National Aeronautics and Space Administration, Langley Research Center, 2003.
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 textUnited States. National Aeronautics and Space Administration., ed. Effect of impact damage and open hole on compressive strength of hybrid composite laminates. National Aeronautics and Space Administration, 1993.
Find full textK, Hill Eric v., and United States. National Aeronautics and Space Administration., eds. Characterization of longitudinal splitting and fiber breakage in Gr/Ep using acoustic emission data. National Aeronautics and Space Administration, 1993.
Find full textK, Hill Eric v., and United States. National Aeronautics and Space Administration., eds. Characterization of longitudinal splitting and fiber breakage in Gr/Ep using acoustic emission data. National Aeronautics and Space Administration, 1993.
Find full textLance, Richards W., and Dryden Flight Research Facility, eds. Yeh-Stratton criterion for stress concentrations on fiber-reinforced composite materials. National Aeronautics and Space Administration, Dryden Flight Research Center, 1996.
Find full textLance, Richards W., and Dryden Flight Research Facility, eds. Yeh-Stratton criterion for stress concentrations on fiber-reinforced composite materials. National Aeronautics and Space Administration, Dryden Flight Research Center, 1996.
Find full textLance, Richards W., and Dryden Flight Research Facility, eds. Yeh-Stratton criterion for stress concentrations on fiber-reinforced composite materials. National Aeronautics and Space Administration, Dryden Flight Research Center, 1996.
Find full textKevin, O'Brien T., and Langley Research Center, eds. Influence of specimen preparation and specimen size on composite transverse tensile strength and scatter. National Aeronautics and Space Administration, Langley Research Center, 2001.
Find full textUnited States. National Aeronautics and Space Administration., ed. Microcracking in composite laminates under thermal and mechanical loading. National Aeronautics and Space Administration, 1995.
Find full textKo, William L. Compressive and shear buckling analysis of metal matrix composite sandwich panels under different thermal environments. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.
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