Książki na temat „Crack Propagation Analysis”

A, Meyers C., Stinson H. C i George C. Marshall Space Flight Center., red. 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.

Shimokawa, Toshiyuki. Analysis of fatigue fractographic data of a rod end housing using Monte Carlo simulation. Chofu, Tokyo: National Aerospace Laboratory, 1995.

Mendelson, Alexander. Analysis of mixed-mode crack propagation using the boundary integral method. [Washington, DC]: National Aeronautics and Space Administration, 1986.

Shivakumar, 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.

C, Newman J., i Langley Research Center, red. 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.

C, Newman J., i Langley Research Center, red. 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.

Kolkman, H. J. Microstructural and fractographic analysis of fatigue crack propagation in 2024-T351 and 2324-T39. Amsterdam: National Aerospace Laboratory, 1985.

S, Dawicke D., Newman J. C i Langley Research Center, red. 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.

United States. National Aeronautics and Space Administration., red. 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.

Kitamura, Takayuki. Stochastic modeling of crack initiation and short-crack growth under creep and creep-fatigue conditions. [Washington, D.C.]: NASA, 1989.

Center, Langley Research, red. Fracture analysis of stiffened panels under biaxial loading with widespread cracking. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

Shamim, Ahmed, i United States. National Aeronautics and Space Administration., red. Local-global analysis of crack growth in continuously reinforced ceramic matrix composites. [Washington, D.C.?]: National Aeronautics and Space Administration, 1988.

Shamim, Ahmed, i United States. National Aeronautics and Space Administration., red. Local-global analysis of crack growth in continuously reinforced ceramic matrix composites. [Washington, D.C.?]: National Aeronautics and Space Administration, 1988.

Shamin, Ahmed, i United States. National Aeronautics and Space Administration, red. Local-global analysis of crack growth in continuously reinforced ceramic matrix composites. [Washington, D.C.?]: National Aeronautics and Space Administration, 1988.

S, Piascik Robert, Newman J. C i Langley Research Center, red. A practical engineering approach to predicting fatigue crack growth in riveted lap joints. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 2000.

Center, Langley Research, red. Advances in fatigue and fracture mechanics analyses for metallic aircraft structures. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 2000.

Center, Langley Research, red. Advances in fatigue and fracture mechanics analyses for metallic aircraft structures. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 2000.

F, Erdogan, i United States. National Aeronautics and Space Administration., red. Cracking of coated materials under transient thermal stresses. [Washington, DC]: National Aeronautics and Space Administration, 1988.

C, Newman J., i Langley Research Center, red. Residual strength analyses of riveted lap-splice joints. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 2000.

Koning, A. V. de. Finite element analyses of stable crack growth in thin sheet material. Amsterdam: National Aerospace Laboratory, 1985.

C, Newman J., i Langley Research Center, red. Methodology for predicting the onset of widespread fatigue damage in lap-splice joints. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.

Zhang, 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.

Barwell, 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.

Gürdal, 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.

K, Binienda W., Kreider K i NASA Glenn Research Center, red. 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.

1952-, Dodds R. H., i United States. National Aeronautics and Space Administration., red. Nonlinear analysis of thin fracture specimens using solid, isoparametric finite elements. [Washington, DC: National Aeronautics and Space Administration, 1997.

Harris, Charles E. NASA airframe structural integrity program. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

C, Newman J., i Langley Research Center, red. Analyses of buckling and stable tearing in thin-sheet materials. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.

L, Bradley Walter, Texas A & M University. Mechanics and Materials Center. i United States. National Aeronautics and Space Administration., red. Micromechanics of compression failures in open hole composite laminates: A report. College Station, Tex: Mechanics and Materials Center, Texas A&M University, 1987.

Center, Langley Research, red. 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.

Center, Langley Research, red. 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.

Jozef Cornelis Walterus van Vroonhoven. Dynamic crack propagation in brittle materials: Analyses based on fracture and damage mechanics. Eindhoven: Eindhoven University of Technology, 1996.

P, Phillips E., Everett R. A i Langley Research Center, red. Fatigue analyses under constant- and variable-amplitude loading using small-crack theory. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

Maymon, Giora. Stochastic Crack Propagation: Essential Practical Aspects. Elsevier Science & Technology Books, 2018.

Maymon, Giora. Stochastic Crack Propagation: Essential Practical Aspects. Elsevier Science & Technology Books, 2018.

Analysis of interface crack branching. [Washington, D.C.]: National Aeronautics and Space Administration, 1989.

Analysis of mixed-mode crack propagation using the boundary integral method. [Washington, DC]: National Aeronautics and Space Administration, 1986.

Fracture analysis of stiffened panels under biaxial loading with widespread cracking. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

An equivalent domain integral method for three-dimensional mixed-mode fracture problems. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.

Local-global analysis of crack growth in continuously reinforced ceramic matrix composites. [Washington, D.C.?]: National Aeronautics and Space Administration, 1988.

A practical engineering approach to predicting fatigue crack growth in riveted lap joints. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 2000.

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.

NASA airframe structural integrity program. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

Analyses of buckling and stable tearing in thin-sheet materials. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.

Han, Seog-young. Elastodynamic analysis of a propagating finite crack in a micropolar elastic solid. 1989.

ASTM 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) i T. Kevin O'Brien (Editor), red. Composite Materials: Fatigue and Fracture (Astm Special Technical Publication// Stp). American Society for Testing & Materials, 1989.