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1

Fracture resistance of aluminum alloys: Notch toughness, tear resistance, and fracture toughness. Washington, D.C: Aluminum Association, 2001.

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2

Beaver, P. W. Experimental and theoretical determination of J(IC) for 2024-T351 aluminium alloy. Melbourne, Australia: Aeronautical Research Laboratories, 1986.

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3

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

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4

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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5

1950-, Cheng Shu-hong, and Mobley Carroll E. 1941-, eds. A fractography atlas of casting alloys. Columbus, Ohio: Battelle Press, 1992.

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6

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

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7

Höhne, Volker. Mechanische und bruchmechanische Bewertung des Bruchverhaltens von WIG-Schweissverbindungen der Aluminiumlegierung A1Mg4,5Mn bei statischer, dynamischer und zyklischer Beanspruchung. Leipzig: Deutscher Verlag für Grundstoffindustrie, 1991.

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8

Materials Solutions Conference 2001 (2001 Indianapolis, Ind.). Advances in the metallurgy of aluminum alloys: Proceedings from Materials Solutions Conference 2001 : the James T. Staley honorary symposium on aluminum alloys, 5-8 November 2001, Indianapolis, Indiana. Materials Park, Ohio: ASM International, 2001.

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9

Idziak, Adam. Anizotropia prędkości fal sejsmicznych i jej związek z orientacją systemów spękań masywów skalnych. Katowice: Uniwersytet Śląski, 1992.

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10

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

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11

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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12

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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13

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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14

Aluminum-Silicon Casting Alloys: Atlas of Microstructures. A S M International, 2016.

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15

Warmuzek, Malgorzata. Aluminum-Silicon Casting Alloys: Atlas of Microfractographs. ASM International, 2004.

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16

Warmuzek, Malgorzata. Aluminum-Silicon Casting Alloys: An Atlas of Microfractographs. A S M International, 2004.

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17

Liu, Yi. Crack growth behavior during LME of high strength aluminum alloy by mercury. 1988.

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18

Benson, Brad. Crack growth behavior of high strength aluminum alloy during liquid metal embrittlement by gallium. 1990.

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19

Liu, Yi. A study of liquid metal embrittlement of aluminum by mercury and gallium via crack growth analysis and atomistic modeling. 1992.

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20

Feng, Xiaoxin. Mixed I/III mode fracture toughness of a 2034 aluminum alloy. 1992.

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21

Kaufman, J. Gilbert. Fracture Resistance of Aluminum Alloys: Notch Toughness, Tear Resistance, and Fracture Toughness. A S M International, 2001.

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22

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.

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23

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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24

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

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25

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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26

Metals and Materials Society Structural Materials Division Minerals (Corporate Author), W. O. Soboyejo (Editor), T. S. Srivatsan (Editor), and H. L. Fraser (Editor), eds. Deformation and Fracture of Ordered Intermetallic Materials III: Proceedings of a Symposium Sponsored by the Structural Materials Division (Smd) of the ... Fracture of Ordered Intermetallic Materials). Minerals, Metals, & Materials Society, 1996.

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27

O, Soboyejo W., Srivatsan T. S, Fraser H. L, and Minerals, Metals and Materials Society. Structural Materials Division., eds. Deformation and fracture of ordered intermetallic materials III: Proceedings of a symposium sponsored by the Structural Materials Division (SMD) of the Minerals, Metals & Materials Society (TMS), held during Materials Week '96, in Cincinnati, Ohio, October 6-10, 1996, hosted by the Minerals, Metals & Materials Society and the Materials Information Society (ASM International). Warrendale, Pa: Minerals, Metals & Materials Society, 1996.

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28

Deformation and fracture of ordered intermetallic materials III: Proceedings of a symposium ... held during Materials Week '96 in Cincinnati Ohio October 6-10 1996 ... Warrendale, PA: TMS, 1996.

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29

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.

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30

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.

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31

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.

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32

Yoshisada, Ueda, Mori Hideshi, and United States. National Aeronautics and Space Administration., eds. Effect of Zr or Cr content on the fracture toughness of high purity Al-Zn-Mg alloys. Washington, DC: National Aeronautics and Space Administration, 1988.

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33

Center, Langley Research, ed. Fracture tests on thin sheet 2024-T3 aluminum alloy for specimens with and without anti-buckling guides. Hampton, Va: National Aeronautics and Science Administration, Langley Research Center, 2001.

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34

O, Soboyejo W., Srivatsan T. S, Davidson D. L, and Minerals, Metals and Materials Society. Structural Materials Division., eds. Fatigue and fracture of ordered intermetallic materials I: Proceedings of a symposium sponsored by the Structural Materials Division (SMD) of the Minerals, Metals & Materials Society (TMS), held during Materials Week '93 in Pittsburgh, PA, October 17-21, 1993 hosted by the Materials, Metals & Materials Society (TMS), and the Materials Information Society (ASM International). Warrendale, Pa: Minerals, Metals & Materials Society, 1994.

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35

N, Shenoy R., and Langley Research Center, eds. Microstructural characterization of aluminum-lithium alloys 1460 and 2195. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.

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36

N, Shenoy R., and Langley Research Center, eds. Microstructural characterization of aluminum-lithium alloys 1460 and 2195. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.

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37

Kaufman, J. Gilbert, and Elwin L. Rooy. Aluminum Alloy Castings. ASM International, 2004. http://dx.doi.org/10.31399/asm.tb.aacppa.9781627083355.

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Aluminum Alloy Castings: Properties, Processes and Applications is a practical guide to the process, structure, property relationships associated with aluminum alloy castings and casting processes. It covers a wide range of casting methods, including variations of sand casting, permanent mold casting, and pressure die casting, showing how key process variables affect the microstructure, properties, and performance of cast aluminum parts. Other chapters provide similar information on the effects of alloying and heat treating and the influence and control of porosity and inclusions. A significant portion of the book contains curated collections of property and performance data, including many previously unpublished aging response curves, growth curves, and fatigue curves; tensile properties at high and low temperatures and at room temperature after high-temperature exposure; the results of creep rupture tests conducted at temperatures from 212 to 600 °F (100 to 315 °C); and stress-strain curves obtained from casting alloys in various tempers under tensile or compressive loads. The book also discusses the factors that contribute to corrosion and fracture resistance and includes test specimen drawings as well as a glossary of terms. For information on the print version, ISBN 978-0-87170-803-8, follow this link.
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38

J, Birt M., and Langley Research Center, eds. Characterization of Al-Cu-Li alloy 2090 near net shape extrusion. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.

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39

Shashidhar, S. R. Fracture toughness of Al-Li alloy Weldalite(TM) 049 at ambient and cryogenic temperatures. 1992.

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40

United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., Martin Marietta Laboratories, and Langley Research Center, eds. The mechanisms of dispersion strengthening and fracture in Al-based XDM[superscript TM] alloys. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1991.

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41

A new aging treatment for improving cryogenic toughness of the main structural alloy of the super lightweight tank. MSFC, Ala: National Aeronautics and Space Administration, Marshall Space Flight Center, 1996.

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42

P, Stanton W., and George C. Marshall Space Flight Center., eds. A new aging treatment for improving cryogenic toughness of the main structural alloy of the super lightweight tank. MSFC, Ala: National Aeronautics and Space Administration, Marshall Space Flight Center, 1996.

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43

Staley, James T., Indiana) Materials Solutions Conference 200 (2001 Indianapolis, and James T. Staley Honorary Symposium on Aluminum Alloys. Advances in the Metallurgy of Aluminum Alloys: Proceedings of the James T. Staley Honorary Symposium on Aluminum Alloys, November 5-7, 2001, Indianapolis, Indiana. American Society for Metals, 2001.

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44

Center, Langley Research, ed. Fracture test results for 0.5, 0.7 and 0.9 inch thick 2324-T39 aluminum alloy material. Hampton, Va: National Aeronautics and Science Administration, Langley Research Center, 2001.

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45

Fracture test results for 0.5, 0.7 and 0.9 inch thick 2324-T39 aluminum alloy material. Hampton, Va: National Aeronautics and Science Administration, Langley Research Center, 2001.

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46

Processing, properties, and applications of iron aluminides: Proceedings of a symposium sponsored by the ASM/MSD Flow and Fracture Committee, the SMD Physical Metallurgy Committeee and the TMS-SMD/ASM-MSD Corrosion and Environmental Effects Committee held at the Annual Meeting of the Minerals, Metals & Materials Society in San Francisco, California, February 27-March 3, 1994. Warrendale, Pa: TMS, 1994.

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47

R, Johnson D., and United States. National Aeronautics and Space Administration., eds. NiAl-based polyphase in situ composites in the NiAl-Ta-X (X = Cr, Mo, or V) systems. [Washington, D.C: National Aeronautics and Space Administration, 1995.

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48

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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49

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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50

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

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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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