Books on the topic 'Fracture load'
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Chona, R., and WR Corwin, eds. Rapid Load Fracture Testing. 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959: ASTM International, 1992. http://dx.doi.org/10.1520/stp1130-eb.
Full textWanhill, R. J. H. Spacecraft sustained load fracture control. Amsterdam: National Aerospace Laboratory, 1989.
Find full textPapini, Marcello. Fracture load prediction of structural adhesive joints. Ottawa: National Library of Canada, 1993.
Find full textWanhill, R. J. H. A test plan for sustained load fracture control verification. Amsterdam: National Aerospace Laboratory, 1989.
Find full textMartin, Roderick H. Interlaminar fracture characterization: A current review. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.
Find full textRösler, Joachim. Mechanical behaviour of engineering materials: Metals, ceramics, polymers, and composites. Berlin: Springer, 2007.
Find full textMinnetyan, Levon. Progression of damage and fracture in composites under dynamic loading. [Washington, D.C.]: National Aeronautics and Space Administration, 1990.
Find full textGotsis, Pascal K. Progressive fracture of fiber composite thin shell structures under internal pressure and axial loads. [Washington, DC]: National Aeronautics and Space Administration, 1996.
Find full textGotsis, Pascal K. Progressive fracture of fiber composite thin shell structures under internal pressure and axial loads. [Washington, DC]: National Aeronautics and Space Administration, 1996.
Find full textSalem, J. A. Fracture toughness of Si₃N₄ measurement with short bar chevron-notched specimens. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1985.
Find full textLi, Jian. Simplified data reduction methods for the ECT test for mode III interlaminar fracture toughness. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.
Find full textCarden, Huey D. Unique failure behavior of metal/composite aircraft structural components under crash type loads. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.
Find full textRavinder, Chona, Corwin W. R, ASTM Committee E-24 on Fracture Testing., and Symposium on Rapid Load Fracture Testing (1990 : San Francisco, Calif.), eds. Rapid load fracture testing. Philadelphia, PA: ASTM, 1992.
Find full textFernlund, Göran Harald. Analysis and fracture load predictions of structural adhesive joints. 1994.
Find full textWilkowski, G. M. Advances in Fracture and Fatigue for the 1990's: Load History Effects of Fracture Resistance (Pvp, Vol 166). Amer Society of Mechanical, 1989.
Find full textJ. Singh, Parminder, and Rohit Kotnis. Injury and repair. Oxford University Press, 2011. http://dx.doi.org/10.1093/med/9780199550647.003.0004.
Full textBehavior of surface and corner cracks subjected to tensile and bending loads in Ti-6A1-4V alloy. Houston, Tex: National Aeronautics and Space Administration, Lyndon B. Johnson Space Center, 1990.
Find full textMcNally, Martin A., and Maurizio A. Catagni. Principles of circular external fixation in trauma. Oxford University Press, 2011. http://dx.doi.org/10.1093/med/9780199550647.003.012015.
Full textHenry, M. Stress fractures. Oxford University Press, 2011. http://dx.doi.org/10.1093/med/9780199550647.003.012017.
Full textCenter, Langley Research, ed. Test methods for textile composites. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.
Find full textUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Division., ed. Fracture toughness and crack growth of Zerodur. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.
Find full textS, Majumdar Bhaskar, and United States. National Aeronautics and Space Administration., eds. In-phase thermomechanical fatigue mechanisms in an unidirectional SCS-6/Ti 15-3 MMC. [Washington, DC]: National Aeronautics and Space Administration, 1995.
Find full textS, Majumdar Bhaskar, and United States. National Aeronautics and Space Administration., eds. In-phase thermomechanical fatigue mechanisms in an unidirectional SCS-6/Ti 15-3 MMC. [Washington, DC]: National Aeronautics and Space Administration, 1995.
Find full textS, Majumdar Bhaskar, and United States. National Aeronautics and Space Administration., eds. In-phase thermomechanical fatigue mechanisms in an unidirectional SCS-6/Ti 15-3 MMC. [Washington, DC]: National Aeronautics and Space Administration, 1995.
Find full textO, Harris David, Thomas Jerrell M, George C. Marshall Space Flight Center., and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. A review of fracture mechanics life technology. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.
Find full textTom, Cordes, Lease Kevin, and Society of Automotive Engineers. Fatigue Design and Evaluation Committee., eds. Multiaxial fatigue of an induction hardened shaft. Warrendale, Pennsylvania: SAE, 1999.
Find full textSociety of Automotive Engineers Fatigue Design and Evaluation committe (Corporate Author), Tom Cordes (Editor), and Kevin Lease (Editor), eds. Multiaxial Fatigue of an Induction Hardened Shaft: Ae-28 (Ae (Series)). Society of Automotive Engineers Inc, 1999.
Find full textC, Newman J., and Langley Research Center, eds. Stress-intensity factors for circumferential surface cracks in pipes and rods under tension and bending loads. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1985.
Find full textC, Newman J., and Langley Research Center, eds. Stress-intensity factors for circumferential surface cracks in pipes and rods under tension and bending loads. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1985.
Find full textStress-intensity factors for circumferential surface cracks in pipes and rods under tension and bending loads. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1985.
Find full text1951-, Scott P., Wilkowski G. M, U.S. Nuclear Regulatory Commission. Office of Nuclear Regulatory Research. Division of Engineering Technology., and Battelle Memorial Institute, eds. The effect of cyclic and dynamic loads on carbon steel pipe. Washington, DC: Division of Engineering Technology, Office of Nuclear Regulatory Research, U.S. Nuclear Regulatory Commission, 1996.
Find full textMechanical Behaviour of Engineering Materials: Metals, Ceramics, Polymers, and Composites. Springer, 2007.
Find full textProgression of damage and fracture in composites under dynamic loading. [Washington, D.C.]: National Aeronautics and Space Administration, 1990.
Find full textFracture analysis of stiffened panels under biaxial loading with widespread cracking. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.
Find full textCenter, Langley Research, ed. Fracture analysis of stiffened panels under biaxial loading with widespread cracking. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.
Find full textH, Hemann John, Gyekenyesi John P, and United States. National Aeronautics and Space Administration., eds. A review of failure models for unidirectional ceramic matrix composites under monotonic loads. [Washington, DC]: National Aeronautics and Space Administration, 1989.
Find full textHughes, Jim. Distal femur and knee. Oxford University Press, 2018. http://dx.doi.org/10.1093/med/9780198813170.003.0014.
Full textR, Mohan, Battelle Memorial Institute, and U.S. Nuclear Regulatory Commission. Office of Nuclear Regulatory Research. Division of Engineering Technology., eds. Effects of toughness anisotropy and combined tension, torsion, and bending loads on fracture behavior of ferritic nuclear pipe. Washington, DC: U.S. Nuclear Regulatory Commission, 1995.
Find full textA progressive damage methodology for residual strength predictions of notched composite panels. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.
Find full textC, Newman J., and Langley Research Center, eds. Analyses of buckling and stable tearing in thin-sheet materials. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.
Find full textAnalyses of buckling and stable tearing in thin-sheet materials. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.
Find full textP, Phillips E., Everett R. A, and Langley Research Center, eds. Fatigue analyses under constant- and variable-amplitude loading using small-crack theory. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.
Find full textKaufman, J. Gilbert, and Elwin L. Rooy. Aluminum Alloy Castings. ASM International, 2004. http://dx.doi.org/10.31399/asm.tb.aacppa.9781627083355.
Full textJ, Minguet Pierre, O'Brien T. Kevin, and Langley Research Center, eds. A method for calculating strain energy release rates in preliminary design of composite skin/stringer debonding under multi-axial loading. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.
Find full textA method for calculating strain energy release rates in preliminary design of composite skin/stringer debonding under multi-axial loading. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.
Find full textCenter, Langley Research, ed. A progressive damage methodology for residual strength predictions of center-crack tension composite panels. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1996.
Find full textAutomotive Control Systems: For Engine, Driveline and Vehicle. Society of Automotive Engineers, 2000.
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. College Station, Tex: Mechanics and Materials Center, Texas A&M University, 1987.
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