Books on the topic 'Aluminum alloys – Fatigue'

Piascik, Robert S. Environmental fatigue in aluminum-lithium alloys. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

Piascik, Robert S. Environmental fatigue of an Al-Li-Cu alloy. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.

Piascik, Robert S. Environmental fatigue of an Al-Li-Cu alloy. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

Lameris, J. The effect of the environment on the fatigue properties of ARALL-3. Amsterdam: National Aerospace Laboratory, 1994.

Lü, Shengli. Lü he jin jie gou fu shi sun shang yan jiu yu ping jia. Xian: Xi bei gong ye ta xue chu ban she, 2009.

Schwarmann, L. Material data of high-strength aluminium alloys for durability evaluation of structures: Fatigue strength, crack propagation, fracture toughness. Düsseldorf: Aluminium-Verlag, 1986.

Bucci, R. J. Aluminum alloy forgings property/performance attributes: Focus: fatigue and durability service capabilities = Les pièces forgées en alliage d'aluminium les attributs de performance/caractéristiques thèmes : fatigue et durabilité capacités en service. Neuilly-sur-Seine, France: AGARD, North Atlantic Treaty Organization, 1998.

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

Wanhill, R. J. H. Corrosion fatigue crack arrest in aluminium alloys: Basic data. Amsterdam: National Aerospace Laboratory, 1987.

Properties of aluminum alloys: Fatigue data and the effects of temperature, product form, and processing. Materials Park, Ohio: ASM International, 2008.

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

Kaufman, J. G. Properties of aluminum alloys: Fatigue data and the effects of temperature, product form, and processing. Materials Park, Ohio: ASM International, 2008.

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.

Wanhill, R. J. H. The influence of starter notches on flight simulation fatigue crack growth. Amsterdam: National Aerospace Laboratory, 1995.

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

Mann, J. Y. Influence of hole surface finish, cyclic frequency and spectrum severity on the fatigue behaviour of thick section aluminium alloy pin joints (U). Melbourne, Victoria: Aeronautical Research Laboratory, 1987.

Finney, J. M. Cold expansion and interference for extending the fatigue life of multi-layer metal joints. Melbourne, Australia: Aeronautical Research Laboratory, 1993.

Hoeven, W. van der. Fatigue and residual strength behaviour of ARALL3 panels with bonded on doublers. Amsterdam: National Aerospace Laboratory, 1992.

Wanhill, R. J. H. Fatigue and fracture of aerospace aluminium alloys: A short course. Amsterdam: National Aerospace Laboratory, 1994.

Wanhill, R. J. H. Damage tolerance property comparisons for 2000 and 8000 series aluminium plate alloys. Amsterdam: National Aerospace Laboratory, 1995.

Schra, L. Influence of gust spectrum variations on fatigue crack growth behaviour of damage tolerant aluminium-lithium sheet materials (NLR contribution to BREU 3250, Task 4). Amsterdam: National Aerospace Laboratory, 1992.

Dawicke, D. S. Through-the-thickness fatigue crack closure behavior in an aluminum alloy. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

Hart, W. G. J. 't. Evaluation of 6013-T6 sheet for damage tolerance applications. Amsterdam: National Aerospace Laboratory, 1992.

W, Smith Stephen. Simulation of fatigue crack initiation at corrosion pits with EDM notches. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 2003.

Smith, Stephen W. Simulation of fatigue crack initiation at corrosion pits with EDM notches. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 2003.

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

Hunt, Anthony William. Fatigue of commercial aluminium alloys. Birmingham: Aston University. Department of Mechanical and Production Engineering, 1986.

Mann, J. Y. Variations in the static properties, unnotched and notched fatigue life behaviour of 13 batches of 2L.65 aluminium alloy extruded bar. Melbourne, Victoria: Aeronautical Research Laboratory, 1987.

Nosair, Shawky Ibrahim Mohamed. Fatigue crack growth in aluminium alloy structures. Salford: University of Salford, 1986.

Birt, Michael J. The fatigue response of high-strength powder route aluminium alloys. Birmingham: University of Birmingham, 1988.

Sawalha, Kameel. The fatigue properties of pressure diecast zinc-aluminium based alloys. Birmingham: Aston University. Department of Mechanical and Production Engineering, 1991.

Gangloff, R. P. NASA-UVa light aerospace alloy and structures technology program (LA²ST). [Washington, D.C: National Aeronautics and Space Administration, 1996.

Gangloff, R. P. NASA-UVa light aerospace alloy and structures technology program (LA²ST). [Washington, D.C: National Aeronautics and Space Administration, 1996.

Gangloff, R. P. NASA-UVa light aerospace alloy and structures technology program (LA²ST). [Washington, D.C: National Aeronautics and Space Administration, 1996.

Byczynski, Glenn Edwin. The strength and fatigue performance of 319 aluminium alloy castings. Birmingham: University of Birmingham, 2002.

Bin, Liu. Surface cleaning of high strength aluminium alloys and its effect on fatigue. Birmingham: University of Birmingham, 2003.

Mulvihill, Paul. The initiation and growth of short fatigue cracks in an aluminium copper alloy. Birmingham: University of Birmingham, 1986.

Maddox, S. J. Treatment of low stresses when applying Miner's rule in the fatigue design of welded aluminium alloys. Cambridge: TWI, 1996.

Moulinier, Flavie. The surface treatment of high strength aluminium alloys and its effect on the fatigue crack growth. Birmingham: University of Birmingham, 1999.

Environmental fatigue in aluminum-lithium alloys. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

Prediction of fatigue-crack growth in a high-strength aluminum alloy under variable-amplitude loading. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1989.

S, Dawicke D., and Langley Research Center, eds. Prediction of fatigue-crack growth in a high-strength aluminum alloy under variable-amplitude loading. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1989.

1926-, Liu H. W., Lewis Research Center, and Syracuse University. Dept. of Mechanical and Aerospace Engineering., eds. Resolved shear stress intensity coefficient and fatigue crack growth in large crystals. Syracuse, N.Y: Syracuse University, [Dept. of Mechanical and Aerospace Engineering] ; [Cleveland, Ohio], 1988.

Prediction of fatigue-crack growth in a high-strength aluminum alloy under variable-amplitude loading. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1989.

Center, Langley Research, ed. Constant amplitude and post-overload fatigue crack growth behavior in PM aluminum alloy AA 8009. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, [1991], 1991.

I, Stephens R., and Society of Automotive Engineers, eds. Fatigue and fracture toughness of A356-T6 cast aluminum alloy. Warrendale, PA: Society of Automotive Engineers, 1988.

N, Sharpe William, and Langley Research Center, eds. Short fatigue crack behavior in notched 2024-T3 aluminum specimens. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1987.

A, Willard S., and Langley Research Center, eds. The growth of small corrosion fatigue cracks in alloy 2024. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.

S, Dawicke D., Bigelow C. A, and Langley Research Center, eds. Finite-element analyses and fracture simulation in thin-sheet aluminum alloy. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

S, Dawicke D., Bigelow C. A, and Langley Research Center, eds. Finite-element analyses and fracture simulation in thin-sheet aluminum alloy. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.