Books on the topic 'Variable amplitude loading (VAL)'

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1

J, Petit, and Société française de métallurgie, eds. Fatigue crack growth under variable amplitude loading. London: Sole distributor in the USA and Canada, Elsevier Science Pub. Co., 1988.

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2

McKeighan, PC, and N. Ranganathan, eds. Fatigue Testing and Analysis Under Variable Amplitude Loading Conditions. 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959: ASTM International, 2005. http://dx.doi.org/10.1520/stp1439-eb.

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3

C, McKeighan P., and Ranganathan Narayanaswami, eds. Fatigue testing and analysis under variable amplitude loading conditions. West Conshohocken, PA: ASTM International, 2005.

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4

Crawford, D. G. Fatigue crack growth in medium scale tubular T-joints under variable amplitude loading. EastKilbride: National Engineering Laboratory, 1990.

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5

1931-, Fisher John W., American Association of State Highway and Transportation Officials., and United States. Federal Highway Administration., eds. Resistance of welded details under variable amplitude long-life fatigue loading. Washington, D.C: Transportation Research Board, National Research Council, 1993.

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6

Austen, I. M. Quantitative Assessment of Corrosion Fatigue Crack Growth Under Variable Amplitude Loading. European Communities / Union (EUR-OP/OOPEC/OPOCE), 1988.

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7

J, Bonacuse P., and Lewis Research Center, eds. Simulation of crack propagation in engine rotating components under variable amplitude loading. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.

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8

National Aeronautics and Space Administration (NASA) Staff. Fatigue Analyses under Constant- and Variable-Amplitude Loading Using Small-Crack Theory. Independently Published, 2018.

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9

P, 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.

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10

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.

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11

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.

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12

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.

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13

M, Hillberry B., and United States. National Aeronautics and Space Administration., eds. Observations of fatigue crack growth rate and closure behavior in 7475-T731 aluminum under variable amplitude loading. West Lafayette, IN: School of Mechanical Engineering, Purdue University, 1987.

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14

Corrosion fatigue crack growth in BS 4360 Grade 50D structural steel in seawater under narrow band variable amplitude loading. London: HMSO, 1986.

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15

Thorpe, T. W., and A. Rance. Corrosion Fatigue Crack Growth in BS 4360 Grade 50d Structural Steel in Seawater Under Narrow Band Variable Amplitude Loading. Stationery Office Books, 1986.

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16

Center, Langley Research, ed. Periodic overload and transport spectrum fatigue crack growth tests of Ti62222STA and Al2024T3 sheet. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

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17

Center, Langley Research, ed. Periodic overload and transport spectrum fatigue crack growth tests of Ti62222STA and Al2024T3 sheet. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

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