Books on the topic 'Crack propagation'

Revill, G. W. An automatic crack measuring system using the direct-current potential-difference method. Melbourne: Aeronautical Research Laboratories, 1985.

Orange, Thomas W. Elevated temperature crack propagation. [Washington, DC: National Aeronautics and Space Administration, 1993.

Lewicki, David G. Gear crack propagation investigations. [Washington, DC]: National Aeronautics and Space Administration, 1996.

Hudak, S. J. A comparison of single-cycle versus multiple-cycle proof testing strategies. Huntsville, Ala: George C. Marshall Space Flight Center, 1990.

M, Fisher Douglas, Holka Donna, and Lewis Research Center, eds. Variables controlling fatigue crack growth of short cracks. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1986.

Sourcebook on fatigue crack propagation: Thresholds and crack closure. Warley, West Midlands: Engineering Materials Advisory Services, 1993.

Newman, J. C. Small-crack effects in high-strength aluminum alloys: A NASA/CAE Cooperative program. Hampton, Va: Langley Research Center, 1994.

Abdul-Salam, Ezzet Hameed. Fatigue crack propagation in mild steel. Salford: University of Salford, 1991.

Center, Langley Research, ed. Corrosion fatigue crack propagation in metals. Washington, D.C: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

G, Lewicki David, and Lewis Research Center, eds. Three-dimensional gear crack propagation studies. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.

G, Lewicki David, and Lewis Research Center, eds. Three-dimensional gear crack propagation studies. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.

G, Lewicki David, and Lewis Research Center, eds. Three-dimensional gear crack propagation studies. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.

Center, Langley Research, and United States. National Aeronautics and Space Administration., eds. Use of marker bands for determination of fatigue crack growth rates and crack front shapes in the pre-corroded coupons. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

Richmond, M. J. A stripyield model including effects of hold periods at constant load. Amsterdam: National Aerospace Laboratory, 1993.

Jie, Ouyang. A study of the mechanism of striation formation and fatigue crack growth in engineering alloys. [S.l.]: [s.n.], 1988.

Center, Langley Research, ed. Separation of crack extension modes in orthotropic delamination models. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

Center, Langley Research, ed. Separation of crack extension modes in orthotropic delamination models. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

Pommier, Sylvie, Anthony Gravouil, Alain Combescure, and Nicolas Moës. Extended Finite Element Method for Crack Propagation. Hoboken, NJ USA: John Wiley & Sons, Inc., 2013. http://dx.doi.org/10.1002/9781118622650.

Chudnovsky, A. On governing equations for crack layer propagation. [Washington, DC: National Aeronautics and Space Administration, 1988.

Gerhard, Welsch, Chudnovsky A, and United States. National Aeronautics and Space Administration, eds. Fatigue crack layer propagation in silicon-iron. [Washington, DC]: National Aeronautics and Space Administration, 1986.

C, 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.

Andrea, Carpinteri, ed. Handbook of fatigue crack propagation in metallic structures. Amsterdam [Netherlands]: Elsevier, 1994.

ATV, Korrosionscentralen. Environmental effects in fatigue crack initiation and propagation. Luxembourg: Commission of the European Communities, 1989.

Bos, M. J. Critical appraisal of the McDonnell Douglas closure model for predicting fatigue crack growth. Melbourne, Australia: Aeronautical Research Laboratory, 1991.

Zhao, W. Near-threshold fatigue crack propagation and closure behaviour in an aluminium alloy. U.K: Institution of Mechanical Engineers, 1985.

Pete, Kantzos, Telesman Jack, and United States. National Aeronautics and Space Administration., eds. Fatigue crack growth and crack bridging in SCS-6/Ti-24-11. [Washington, D.C: National Aeronautics and Space Administration, 1995.

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.

Edwards, P. R. Short-crack growth behaviour in various aircraft materials. Neuilly sur Seine: Agard, 1990.

Edwards, P. R. Short-crack growth behaviour in various aircraft materials. Neuilly sur Seine, France: AGARD, 1990.

Center, 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.

Center, 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.

Lof, C. J. Useful lifetime prediction software for plane semi-cracks in 3-D solid configurations. Amsterdam: National Aerospace Laboratory, 1986.

1928-, Sun C. T., and United States. National Aeronautics and Space Administration., eds. Dynamic delamination crack propagation in a graphite/epoxy laminate. [Washington, DC]: National Aeronautics and Space Administration, 1991.

Fouad, Fanous, Bluhm Delwyn, Ames Laboratory, and U.S. Nuclear Regulatory Commission. Office of Nuclear Reactor Regulation. Division of Engineering., eds. Crack propagation in high strain regions of Sequoyah containment. Washington, DC: Division of Engineering, Office of Nuclear Reactor Regulation, U.S. Nuclear Regulatory Commission, 1993.

Babiloglu, Erol. A numerical study of dynamic crack propagation in composites. Monterey, Calif: Naval Postgraduate School, 1992.

Lewicki, David G. Effect of rim thickness on gear crack propagation path. [Washington, DC: National Aeronautics and Space Administration, 1996.

Lewicki, David G. Effect of rim thickness on gear crack propagation path. [Washington, DC: National Aeronautics and Space Administration, 1996.

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. An assessment of fatigue damage and crack growth prediction techniques. Neuilly sur Seine, France: AGARD, 1994.

Wallace, William. Methods for crack growth testing in gas turbine engine disc materials. Ottawa: National Aeronautical Establishment, 1987.

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

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. An assessment of fatigue damage and crack growth prediction techniques: Papers presented at the 77th Meeting of the AGARD Structures and Materials Panel, held in Bordeaux, France 29th-30th September 1993. Neuilly sur Seine, France: AGARD, 1994.

Advisory Group for Aerospace Research and Development. Structures and Materials Panel. Meeting,, ed. An assessment of fatigue damage and crack growth prediction techniques: Papers presented at the 77th Meeting of the AGARD Structures and Materials Panel, held in Bordeaux, France, 29th-30th September 1993. Neuilly sur Seine: Agard, 1994.

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. AGARD engine disc cooperative test programme. Neuilly sur Seine, France: AGARD, 1993.

Hoeven, W. van der. The effect of fatigue crack length on the residual strength of ARALL3 panels with fingertip doublers. Amsterdam: National Aerospace Laboratory, 1994.

Qing, Li. The role of active corrosion in fatigue crack initiation and early stages of crack propagation. Manchester: UMIST, 1996.

United 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.

P, Gabb Timothy, Miner R. V, and United States. National Aeronautics and Space Administration., eds. Fatique crack propagation of nickel-base superalloys at 650 ̊C. [Washington, D.C.]: National Aeronautics and Space Administration, 1985.

Lewicki, David G. Effect of speed (centrifugal load) on gear crack propagation direction. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2001.

P, Gabb T., Miner R. V, and United States. National Aeronautics and Space Administration., eds. Fatique crack propagation of nickel-base superalloys at 650 C. [Washington, D.C.]: National Aeronautics and Space Administration, 1985.

Pete, Kantzos, Telesman Jack, and Lewis Research Center, eds. Modeling of crack bridging in a unidirectional metal matrix composite. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1991.