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1

Schra, L. Outdoor corrosion testing of aluminium-lithium alloys. National Aerospace Laboratory, 1990.

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2

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

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3

Agarwala, VS, and GM Ugiansky, eds. New Methods for Corrosion Testing of Aluminum Alloys. ASTM International, 1992. http://dx.doi.org/10.1520/stp1134-eb.

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4

Holmes, Andrew. Rapid spot testing of metals, alloys and coatings. ASM International, 2002.

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5

S, Agarwala Vinod, Ugiansky G. M, and International Symposium on Corrosion Testing of Aluminum Alloys (1990 : San Francisco, Calif.), eds. New methods for corrosion testing of aluminum alloys. ASTM, 1992.

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6

Tylczak, J. H. Correlating abrasive wear to alloy additions in low-alloy steels. U.S. Dept. of the Interior, Bureau of Mines, 1986.

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7

Matsuoka, Saburō. Kikai kōzōyō kinzoku zairyō no hirō ni kansuru shihyō tokusei. Kagaku Gijutsuchō Kinzoku Zairyō Gijutsu Kenkyūjo, 1997.

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8

Huang, F. H. Fracture properties of irradiated alloys. Avante Pub., 1995.

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9

Dammer, Rainer. Beitrag zur Bewertung mechanischer Eigenschaften hochtemperaturgelöteter Superlegierungen. Deutscher Verlag für Schweisstechnik, 1986.

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10

Gayda, John. Burst testing of a superalloy disk with a dual grain structure. National Aeronautics and Space Administration, Glenn Research Center, 2002.

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11

Pete, Kantzos, and NASA Glenn Research Center, eds. Burst testing of a superalloy disk with a dual grain structure. National Aeronautics and Space Administration, Glenn Research Center, 2002.

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12

L, Long Donald, Rummel Ward D, and United States. National Aeronautics and Space Administration., eds. NDE detectability of fatigue-type cracks in high-strength alloys: NDE reliability assessments, final report. Martin Marietta Astronautics Group, Space Launch Systems Company, 1989.

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13

Bäumel, A. Materials data for cyclic loading. Elsevier, 1990.

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14

Boller, Chr. Materials data for cyclic loading. Elsevier, 1987.

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15

Wanhill, Russell, and Michael Windisch. Corrosion and Stress Corrosion Testing of Aerospace Vehicle Structural Alloys. Springer International Publishing, 2018. http://dx.doi.org/10.1007/978-3-319-89530-7.

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16

Canada, Atomic Energy of. Acoustic Emission From Zirconium Alloys During Mechanical and Fracture Testing. s.n, 1985.

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17

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

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18

Bryan, Chin, Cohron Jon, and George C. Marshall Space Flight Center., eds. Final report for hot hydrogen testing of refractory metals and ceramics. Materials Engineering Program, Auburn University, 1993.

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19

Dawicke, D. S. Biaxial testing of 2219-T87 aluminum alloy using cruciform specimens. National Aeronautics and Administration, Langley Research Center, 1997.

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20

Lanagan, T. J. Microstructure-property relationships in Al-Cu-Li-Ag-Mg Weldalite[superscript TM] alloys. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1991.

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21

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

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22

Henkel, Daniel P. A Study of aluminum-lithium alloy solidification using acoustic emission techniques. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

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23

Henkel, Daniel P. A study of aluminum-lithium alloy solidification using acoustic emission techniques. Langley Research Center, 1992.

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24

Henkel, Daniel P. A Study of aluminum-lithium alloy solidification using acoustic emission techniques. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

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25

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

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26

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

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27

1951-, Stoller R. E., U.S. Nuclear Regulatory Commission. Office of Nuclear Regulatory Research. Division of Engineering Technology., and Oak Ridge National Laboratory, eds. Microstructural characterization of selected AEA/UCSB model FeCuMn alloys. Division of Engineering Technology, Office of Nuclear Regulatory Research, U.S. Nuclear Regulatory Commission, 1996.

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28

Hafley, Robert A. Fatigue crack growth rate test results for Al-Li 2195 parent metal, variable polarity, plasma arc welds and friction stir welds. National Aeronautics and Space Administration, Langley Research Center, 2000.

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29

J, Pargeter R., Edison Welding Institute, and Welding Institute, eds. Quantifying weldability: Papers presented at a seminar held in Coventry, 10 October 1985 and organized by The Welding Institute. The Welding Institute, 1988.

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30

Beavers, J. A. Pitting, galvanic, and long-term corrosion studies on candidate container alloys for the tuff repository. Division of Regulatory Applications, Office of Nuclear Regulatory Research, U.S. Nuclear Regulatory Commission, 1992.

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31

Beavers, J. A. Pitting, galvanic, and long-term corrosion studies on candidate container alloys for the tuff repository. Division of Regulatory Applications, Office of Nuclear Regulatory Research, U.S. Nuclear Regulatory Commission, 1992.

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32

K, Soppett W., Kassner T. F, U.S. Nuclear Regulatory Commission. Office of Nuclear Regulatory Research. Division of Engineering Technology., and Argonne National Laboratory, eds. Corrosion fatigue of alloys 600 and 690 in simulated LWR environments. Division of Engineering Technology, Office of Nuclear Regulatory Research, U.S. Nuclear Regulatory Commission, 1996.

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33

Robinson, David N. On thermomechanical testing in support of constitutive equation development for high-temperature alloys. National Aeronautics and Space Administration, 1985.

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34

United States. National Aeronautics and Space Administration, ed. On thermomechanical testing in support of constitutive equation development for high-temperature alloys. National Aeronautics and Space Administration, 1985.

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35

P, Kaplar E., ed. Mechanical properties of unirradiated and irradiated Zr-1% Nb cladding: Procedures and results of low temperature biaxial burst tests and axial tensile tests. Office of Nuclear Regulatory Research, U.S. Nuclear Regulatory Commission, 2001.

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36

P, Kaplar E., ed. Mechanical properties of unirradiated and irradiated Zr-1% Nb cladding: Procedures and results of low temperature biaxial burst tests and axial tensile tests. Office of Nuclear Regulatory Research, U.S. Nuclear Regulatory Commission, 2001.

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37

Frąckowiak, Janusz E. Badania nadstruktur typu B2 i DO3 metodą efektu Mössbauera. Uniwersytet Śląski, 1993.

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38

Chatterjee, S. Measurement and application of fracture toughness properties of ZR-2.5NB pressure tube removed from KAPS-2. Bhabha Atomic Research Centre, 2008.

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39

Blickensderfer, Robert. Laboratory tests of spalling, breaking, and abrasion of wear-resistant alloys used in mining and mineral processing. U.S. Dept. of the Interior, Bureau of Mines, 1985.

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40

United States. National Aeronautics and Space Administration. Scientific and Technical Information Division. and Failure Analysis Associates, eds. Nonequilibrium phase chemistry in high temperature structural alloys. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1991.

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41

1960-, Bonacuse Peter J., United States. National Aeronautics and Space Administration., and U.S. Army Research Laboratory., eds. An axial-torsional, thermomechanical fatigue testing technique. National Aeronautics and Space Administration, 1996.

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42

1960-, Bonacuse Peter J., United States. National Aeronautics and Space Administration., and U.S. Army Research Laboratory., eds. An axial-torsional, thermomechanical fatigue testing technique. National Aeronautics and Space Administration, 1996.

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43

1960-, Bonacuse Peter J., United States. National Aeronautics and Space Administration., and U.S. Army Research Laboratory., eds. An axial-torsional, thermomechanical fatigue testing technique. National Aeronautics and Space Administration, 1996.

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44

Thompson, N. G. Potentiodynamic polarization studies on candidate container alloys for the tuff repository. Division of Regulatory Applications, Office of Nuclear Regulatory Research, U.S. Nuclear Regulatory Commission, 1992.

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45

Singleton, D. J. Wear and corrosion of 12 alloys during laboratory milling of phosphate rock in phosphoric acid waste water. U.S. Dept. of the Interior, Bureau of Mines, 1985.

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46

Workshop on Corrosion Modeling for Life Prediction (2nd 2010 Rome). Light weight metal corrosion and modeling for corrosion prevention, life prediction and assessment: Selected peer reviewed papers from the 2nd Workshop on Corrosion Modeling for Life Prediction (CMLP 2010), Rome, Italy, 18 to 20 April 2010, held under the auspices of the Office of Naval Research Global and the Università degli Studi di Milano. Trans Tech Publications, 2010.

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47

Joyce, J. A. Development of an engineering definition of the extent of J singularity controlled crack growth. Division of Engineering, Office of Nuclear Regulatory Research, U.S. Nuclear Regulatory Commission, 1989.

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48

Institute of Materials (London, England) and European Federation of Corrosion, eds. A Working party report on corrosion resistant alloys for oil and gas production: Guidance on general requirements and test methods for Hb2sS service. Published for the European Federation of Corrosion by the Institute of Materials, 1996.

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49

J, Schneider Steven, and United States. National Aeronautics and Space Administration., eds. Testing of wrought iridium/chemical vapor deposition rhenium rocket. National Aeronautics and Space Administration, 1997.

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50

J, Schneider Steven, and United States. National Aeronautics and Space Administration., eds. Testing of wrought iridium/chemical vapor deposition rhenium rocket. National Aeronautics and Space Administration, 1997.

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