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Books on the topic 'Aluminum alloys – Cracking'

Author: Grafiati
Published: 4 June 2021
Last updated: 29 January 2023

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1

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.

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2

Gross, Jürgen. Eigenschaften von Aluminium-Silicium-Legierungen in unterschiedlichen Behandlungszuständen unter besonderer Beachtung des Gefügeeinflusses auf die Festigkeitswerte und auf das Bruchverhalten. Berlin: Wissenschaft und Technik Verlag, 1992.

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3

Kolkman, H. J. Stress corrosion resistance of damage tolerant aluminum-lithium sheet materials. Amsterdam: National Aerospace Laboratory, 1991.

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4

Schra, L. Long-term outdoor stress corrosion testing of overaged 7000 series aluminium alloys. Amsterdam: National Aerospace Laboratory, 1988.

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5

Schra, L. Effect of cooling rate on corrosion properties of high strength aluminium alloys under atmospheric conditions. Amsterdam: National Aerospace Laboratory, 1990.

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6

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

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7

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

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8

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

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9

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

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10

Moss, A. C. The correlation of acoustic electrochemical and mechanical transients during the environmentally assisted cracking of aluminium-zinc-magnesium alloys. Manchester: UMIST, 1989.

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11

Crack-tip opening angle measurements and crack tunneling under stable tearing in thin sheet 2024-T3 aluminum alloy. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.

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12

A, Sutton M., and Langley Research Center, eds. Crack-tip opening angle measurements and crack tunneling under stable tearing in thin sheet 2024-T3 aluminum alloy. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.

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13

A, Sutton M., and Langley Research Center, eds. Crack-tip opening angle measurements and crack tunneling under stable tearing in thin sheet 2024-T3 aluminum alloy. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.

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14

Center, Langley Research, ed. Fracture testing of 2324-T39 aluminum alloy. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

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15

Fracture testing of 2324-T39 aluminum alloy. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

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16

Center, Langley Research, ed. Fracture testing of 2324-T39 aluminum alloy. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

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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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18

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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19

Center, 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.

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20

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

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21

S, 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.

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22

Lampman, Steve, ed. Weld Integrity and Performance. ASM International, 1997. http://dx.doi.org/10.31399/asm.tb.wip.9781627083591.

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Abstract:
Weld Integrity and Performance is a convenient reference and sourcebook for anyone involved in the application, fabrication, or assessment of welded structures. It provides detailed information on relevant topics including weld solidification, weldability testing, weld characterization, discontinuities and imperfections, cracking phenomena, inspection and evaluation techniques, fatigue and fracture control, fracture mechanics, fitness-for-service testing, repair welding, and weld corrosion. An entire section, the largest by far in the book, covers the basic metallurgy and engineering properties of weldments made from carbon and low-alloy steels, stainless steels, aluminum alloys, titanium alloys, nickel-base alloys, and refractory metals, including tantalum, niobium, molybdenum, and tungsten alloys. The book also provides insights into the origins of failure associated with different welding processes and includes an appendix with information on the weldability of common alloys (including cast irons) as well as process selection guidelines, recommended preheat and interpass temperatures and postweld heat treatments for pipe welds and pressure vessels, and qualification codes and standards. For information on the print version, ISBN 978-0-87170-600-8, follow this link.
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23

A, Starke E., and United States. National Aeronautics and Space Administration., eds. NASA-UVa light aerospace alloy and structures technology program (LA²ST): Progress report January 1, 1995 to June 30, 1995. Charlottesville, VA: School of Engineering & Applied Center, University of Va., 1995.

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24

United States. National Aeronautics and Space Administration., ed. NASA-UVA light aerospace alloy and structures technology program (LA²ST): A progress report, January 1, 1994-June 30, 1994. Charlottesville, VA: Dept. of Materials Science and Engineering, School of Engineering & Applied Science, 1994.

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25

A, Starke E., and United States. National Aeronautics and Space Administration., eds. NASA-UVA Light Aerospace Alloy and Structures Technology Program (LA²ST): Progress report, July 1, 1996 through December 31, 1996, NASA-LaRC grant NAG-1-745. Charlottesville, VA: School of Engineering & Applied Science, University of Virginia, 1997.

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26

NASA-UVa light aerospace alloy and structures technology program (LA²ST): Progress report January 1, 1995 to June 30, 1995. Charlottesville, VA: School of Engineering & Applied Center, University of Va., 1995.

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27

A, Starke E., and United States. National Aeronautics and Space Administration., eds. NASA-UVA light aerospace alloy and structures technology program (LA²ST).: Research on materials for the high speed civil transport. Charlottesville, VA: School of Engineering & Applied Science, University of Virginia, 1997.

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28

NASA-UVA Light Aerospace Alloy and Structures Technology Program (LA²ST): Progress report, July 1, 1996 through December 31, 1996, NASA-LaRC grant NAG-1-745. Charlottesville, VA: School of Engineering & Applied Science, University of Virginia, 1997.

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29

United States. National Aeronautics and Space Administration., ed. NASA-UVA light aerospace alloy and structures technology program (LAST): A progress report, January 1, 1994-June 30, 1994. Charlottesville, VA: Dept. of Materials Science and Engineering, School of Engineering & Applied Science, 1994.

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30

A, Starke E., and United States. National Aeronautics and Space Administration., eds. NASA-UVA Light Aerospace Alloy and Structures Technology Program (LA²ST): Progress report, July 1, 1996 through December 31, 1996, NASA-LaRC grant NAG-1-745. Charlottesville, VA: School of Engineering & Applied Science, University of Virginia, 1997.

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31

A, Starke E., and United States. National Aeronautics and Space Administration., eds. NASA-UVA light aerospace alloy and structures technology program (LA²ST).: Research on materials for the high speed civil transport. Charlottesville, VA: School of Engineering & Applied Science, University of Virginia, 1997.

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32

NASA-UVA light aerospace alloy and structures technology program (LA²ST).: Research on materials for the high speed civil transport. Charlottesville, VA: School of Engineering & Applied Science, University of Virginia, 1997.

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33

A, Starke E., and United States. National Aeronautics and Space Administration., eds. NASA-UVa light aerospace alloy and structures technology program (LA²ST): Progress report January 1, 1995 to June 30, 1995. Charlottesville, VA: School of Engineering & Applied Center, University of Va., 1995.

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34

A, Starke E., and United States. National Aeronautics and Space Administration., eds. NASA-UVA Light Aerospace Alloy and Structures Technology Program (LA²ST): Progress report, July 1, 1996 through December 31, 1996, NASA-LaRC grant NAG-1-745. Charlottesville, VA: School of Engineering & Applied Science, University of Virginia, 1997.

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35

A, Starke E., and United States. National Aeronautics and Space Administration., eds. NASA-UVA light aerospace alloy and structures technology program (LA²ST).: Research on materials for the high speed civil transport. Charlottesville, VA: School of Engineering & Applied Science, University of Virginia, 1997.

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36

NASA-UVA light aerospace alloy and structures technology program (LAST): A progress report, January 1, 1994-June 30, 1994. Charlottesville, VA: Dept. of Materials Science and Engineering, School of Engineering & Applied Science, 1994.

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