Книги з теми "Crack Propagation Analysis"
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Ознайомтеся з топ-46 книг для дослідження на тему "Crack Propagation Analysis".
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A, Meyers C., Stinson H. C, and George C. Marshall Space Flight Center., eds. Comparison of two computer codes for crack growth analysis: NASCRAC versus NASA/FLAGRO. [Marshall Space Flight Center, Ala.]: National Aeronautics and Space Administration, George C. Marshall Space Flight Center, 1989.
Знайти повний текст джерелаShimokawa, Toshiyuki. Analysis of fatigue fractographic data of a rod end housing using Monte Carlo simulation. Chofu, Tokyo: National Aerospace Laboratory, 1995.
Знайти повний текст джерелаMendelson, Alexander. Analysis of mixed-mode crack propagation using the boundary integral method. [Washington, DC]: National Aeronautics and Space Administration, 1986.
Знайти повний текст джерелаShivakumar, K. N. Three-dimensional elastic-plastic analysis of shallow cracks in single-edge-crack-tension specimens. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.
Знайти повний текст джерелаC, Newman J., and Langley Research Center, eds. Three-dimensional elastic-plastic analysis of shallow cracks in single-edge-crack-tension specimens. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.
Знайти повний текст джерелаC, Newman J., and Langley Research Center, eds. Three-dimensional elastic-plastic analysis of shallow cracks in single-edge-crack-tension specimens. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.
Знайти повний текст джерелаKolkman, H. J. Microstructural and fractographic analysis of fatigue crack propagation in 2024-T351 and 2324-T39. Amsterdam: National Aerospace Laboratory, 1985.
Знайти повний текст джерелаS, Dawicke D., Newman J. C, and Langley Research Center, eds. Orientation effects on the measurement and analysis of critical CTOA in an aluminum alloy sheet. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration., ed. Determination of stress intensity factor distributions for "interface" cracks in incompressible, dissimilar materials: Summary report : reporting period - 8/15/94 - 12/31/97 : grant no. NAG-1-1622-Supl. 1-5*. [Washington, DC: National Aeronautics and Space Administration, 1997.
Знайти повний текст джерелаKitamura, Takayuki. Stochastic modeling of crack initiation and short-crack growth under creep and creep-fatigue conditions. [Washington, D.C.]: NASA, 1989.
Знайти повний текст джерелаCenter, 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.
Знайти повний текст джерелаShamim, Ahmed, and United States. National Aeronautics and Space Administration., eds. Local-global analysis of crack growth in continuously reinforced ceramic matrix composites. [Washington, D.C.?]: National Aeronautics and Space Administration, 1988.
Знайти повний текст джерелаShamim, Ahmed, and United States. National Aeronautics and Space Administration., eds. Local-global analysis of crack growth in continuously reinforced ceramic matrix composites. [Washington, D.C.?]: National Aeronautics and Space Administration, 1988.
Знайти повний текст джерелаShamin, Ahmed, and United States. National Aeronautics and Space Administration, eds. Local-global analysis of crack growth in continuously reinforced ceramic matrix composites. [Washington, D.C.?]: National Aeronautics and Space Administration, 1988.
Знайти повний текст джерелаS, Piascik Robert, Newman J. C, and Langley Research Center, eds. A practical engineering approach to predicting fatigue crack growth in riveted lap joints. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 2000.
Знайти повний текст джерелаCenter, Langley Research, ed. Advances in fatigue and fracture mechanics analyses for metallic aircraft structures. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 2000.
Знайти повний текст джерелаCenter, Langley Research, ed. Advances in fatigue and fracture mechanics analyses for metallic aircraft structures. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 2000.
Знайти повний текст джерелаF, Erdogan, and United States. National Aeronautics and Space Administration., eds. Cracking of coated materials under transient thermal stresses. [Washington, DC]: National Aeronautics and Space Administration, 1988.
Знайти повний текст джерелаC, Newman J., and Langley Research Center, eds. Residual strength analyses of riveted lap-splice joints. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 2000.
Знайти повний текст джерелаKoning, A. V. de. Finite element analyses of stable crack growth in thin sheet material. Amsterdam: National Aerospace Laboratory, 1985.
Знайти повний текст джерелаC, Newman J., and Langley Research Center, eds. Methodology for predicting the onset of widespread fatigue damage in lap-splice joints. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.
Знайти повний текст джерелаZhang, Jia Zhen. Finite element analysis and experimental study of short amd long fatigue crack propagation in aluminium alloy IN 9052. Birmingham: University of Birmingham, 1991.
Знайти повний текст джерелаBarwell, Craig A. A study of failure in small pressurized cylindrical shells containing a crack. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.
Знайти повний текст джерелаGürdal, Zafer. Progress report for the research performed under NASA Research Grant NAG-1-643: By Zafer Gürdal. [Washington, DC: National Aeronautics and Space Administration, 1986.
Знайти повний текст джерелаK, Binienda W., Kreider K, and NASA Glenn Research Center, eds. Analysis of a generally oriented crack in a functionally graded strip sandwiched between two homogeneous half planes. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.
Знайти повний текст джерела1952-, Dodds R. H., and United States. National Aeronautics and Space Administration., eds. Nonlinear analysis of thin fracture specimens using solid, isoparametric finite elements. [Washington, DC: National Aeronautics and Space Administration, 1997.
Знайти повний текст джерелаHarris, Charles E. NASA airframe structural integrity program. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.
Знайти повний текст джерелаC, 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.
Знайти повний текст джерелаL, 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.
Знайти повний текст джерелаCenter, Langley Research, ed. Analyses of fatigue crack growth and closure near threshold conditions for large-crack behavior. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.
Знайти повний текст джерелаCenter, Langley Research, ed. Analyses of fatigue crack growth and closure near threshold conditions for large-crack behavior. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.
Знайти повний текст джерелаJozef Cornelis Walterus van Vroonhoven. Dynamic crack propagation in brittle materials: Analyses based on fracture and damage mechanics. Eindhoven: Eindhoven University of Technology, 1996.
Знайти повний текст джерелаP, 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.
Знайти повний текст джерелаMaymon, Giora. Stochastic Crack Propagation: Essential Practical Aspects. Elsevier Science & Technology Books, 2018.
Знайти повний текст джерелаMaymon, Giora. Stochastic Crack Propagation: Essential Practical Aspects. Elsevier Science & Technology Books, 2018.
Знайти повний текст джерелаAnalysis of interface crack branching. [Washington, D.C.]: National Aeronautics and Space Administration, 1989.
Знайти повний текст джерелаAnalysis of mixed-mode crack propagation using the boundary integral method. [Washington, DC]: National Aeronautics and Space Administration, 1986.
Знайти повний текст джерелаFracture analysis of stiffened panels under biaxial loading with widespread cracking. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.
Знайти повний текст джерелаAn equivalent domain integral method for three-dimensional mixed-mode fracture problems. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.
Знайти повний текст джерелаLocal-global analysis of crack growth in continuously reinforced ceramic matrix composites. [Washington, D.C.?]: National Aeronautics and Space Administration, 1988.
Знайти повний текст джерелаA practical engineering approach to predicting fatigue crack growth in riveted lap joints. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 2000.
Знайти повний текст джерелаAnalysis of a generally oriented crack in a functionally graded strip sandwiched between two homogeneous half planes. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.
Знайти повний текст джерелаNASA airframe structural integrity program. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.
Знайти повний текст джерелаAnalyses of buckling and stable tearing in thin-sheet materials. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.
Знайти повний текст джерелаHan, Seog-young. Elastodynamic analysis of a propagating finite crack in a micropolar elastic solid. 1989.
Знайти повний текст джерелаASTM Committee D-30 on High Modulus Fibers and Their Composites (Corporate Author), Astm Committee E-24 on Fracture Testing (Corporate Author), Symposium on Composite Materials: Fatigue and Fracture (Corporate Author), H. Thomas Hahn (Editor), Paul A. Lagace (Editor), and T. Kevin O'Brien (Editor), eds. Composite Materials: Fatigue and Fracture (Astm Special Technical Publication// Stp). American Society for Testing & Materials, 1989.
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