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1

Tack, Andrew J. The effect of microstructure and loading variables on fatigue crack propagation in three aerospace bearing steels anda low alloy steel. Birmingham: University of Birmingham, 1989.

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2

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

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3

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

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4

Trail, Stephen John. Fatigue of gamma based titanium aluminide alloys. Birmingham: University of Birmingham, 1996.

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5

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

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6

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

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7

Berkovits, Avraham. Modelling fatigue damage accumulation in nickel base superalloys: Final report. Haifa: Technion-Israel Institute of Technology, Faculty of Aerospace Engineering, 1992.

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8

Troshchenko, Valeriĭ Trokhymovych. Soprotivlenie ustalosti metallov i splavov: Spravochnik. Kiev: Nauk. dumka, 1987.

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9

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

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10

Grinʹberg, N. M. Struktura i ustalostnai͡a︡ prochnostʹ magnievykh splavov. Cheli͡a︡binsk: "Metallurgii͡a︡," Cheli͡a︡binskoe ot-nie, 1991.

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11

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

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12

Krupp, Ulrich. Fatigue crack propagation in metals and alloys: Microstructural aspects and modelling concepts. Weinheim, DE: Wiley-VCH, 2006.

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13

Kan, Nathan Yu-kwong. Fatigue failure from internal defects in nickel base alloys. Portsmouth: University of Portsmouth, Dept. of Mechanical and Manufacturing Engineering, 1996.

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14

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

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15

Michael, Turner. Brush plating of bearing alloys on aluminium alloy shells. Birmingham: Aston University. Department of Mechanical and Production Engineering, 1986.

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16

Beswick, John M., 1945- editor, ASTM International, and American Society for Testing and Materials. Committee A-1 on Steel, Stainless Steel, and Related Alloys, eds. Bearing steel technologies: 10th volume : advances in steel technologies for rolling bearings. West Conshohocken, PA: ASTM International, 2015.

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17

Beswick, John M., 1945- editor of compilation and American Society for Testing and Materials. Committee A-1 on Steel, Stainless Steel, and Related Alloys, eds. Bearing steel technologies: 9th volume : advances in rolling contact fatigue strength testing and related substitute technologies. West Conshohocken, PA: ASTM International, 2012.

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18

Zaretsky, Erwin V. Selection [of] rolling-element bearing steels for long-life application. [Washington, D.C.]: National Aeronautics and Space Administration, 1986.

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19

Zaretsky, Erwin V. Selection [of] rolling-element bearing steels for long-life application. [Washington, D.C.]: National Aeronautics and Space Administration, 1986.

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20

Zaretsky, Erwin V. Selection [of] rolling-element bearing steels for long-life application. [Washington, D.C.]: National Aeronautics and Space Administration, 1986.

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21

Zaretsky, Erwin V. Selection [of] rolling-element bearing steels for long-life application. [Washington, D.C.]: National Aeronautics and Space Administration, 1986.

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22

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.

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23

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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24

Halford, Gary R. Thermal fatigue durability for advanced propulsion materials. [Washington, DC]: National Aeronautics and Space Administration, 1990.

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25

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

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26

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

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27

Wanhill, Russell, and Simon Barter. Fatigue of Beta Processed and Beta Heat-treated Titanium Alloys. Dordrecht: Springer Netherlands, 2012. http://dx.doi.org/10.1007/978-94-007-2524-9.

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28

Jenkins, Nigel Barry. Fracture and fatigue of gamma based titanium aluminide intermetallic alloys. Birmingham: University of Birmingham, 1998.

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29

International Symposium on Fatigue Behavior of Titanium Alloys (1998 Chicago, Ill.). Fatigue behavior of titanium alloys: Proceedings of an international symposium. Warrendale, Pennsylvania: Minerals, Metals & Materials Society, 1999.

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30

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

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31

Bizon, Peter T. Thermal-fatigue and oxidation resistance of cobalt-modified Udimet 700 alloy. Cleveland, Ohio: Lewis Research Center, 1986.

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32

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

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33

Verrilli, Michael J. High temperature fatigue behavior of tungsten copper composites. [Washington, D.C.]: NASA, 1990.

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34

Taghani, Nourberdi. Crack growth in gas turbine alloys due to high cycle fatigue. Portsmouth: Portsmouth Polytechnic, Dept. of Mechanical Engineering, 1989.

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35

Erquicia, Rodney Antonio Balanza. Wear of high aluminium zinc-based alloys in plain bearing applications. Birmingham: Aston University. Department of Mechanical and Electrical Engineering, 1993.

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36

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

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37

Castelli, Michael G. Thermomechanical and isothermal fatigue behavior of a (90) titanium matrix composite. Cleveland, Ohio: Lewis Research Center, National Aeronautics and Space Administration, 1993.

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38

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

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39

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.

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40

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

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41

D, Henry Scott, Dragolich Kathleen S, DiMatteo Nikki D, and ASM International, eds. Fatigue data book: Light structural alloys. Materials Park, OH: ASM International, 1995.

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42

(Editor), Scott D. Henry, and Faith Reidenbach (Editor), eds. Fatigue Data Book: Light Structural Alloys. ASM International, 1995.

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43

United States. National Aeronautics and Space Administration., ed. Micromechanisms of thermomechanical fatigue--: A comparison with isothermal fatigue. [Washington, D.C.?]: National Aeronautics and Space Administration, 1986.

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44

E, Boyer Howard, and American Society for Metals, eds. Atlas of fatigue curves. Metals Park, Ohio: American Society for Metals, 1986.

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45

Henry, M. Stress fractures. Oxford University Press, 2011. http://dx.doi.org/10.1093/med/9780199550647.003.012017.

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Abstract:
♦ Stress fractures are fractures occurring as the result of repetitive, submaximal loads, in the absence of a specific precipitating traumatic event.♦ These fractures can be subdivided into two groups on the basis of aetiology. Whereas ‘fatigue fractures’ result from the excessive repetitive (i.e. abnormal) loading of normal bone, ‘insufficiency fractures’ are fractures resulting from normal forces acting on abnormal bone.♦ Early diagnosis allows the initiation of effective treatment that can prevent prolonged pain and disability, as well as avoiding the progression to displacement or a non-union.♦ While management decisions are generally focused on activity modification, protection of weight bearing, and immobilization, there is a subset of fractures at high risk for progression to complete fracture, non-union, or delayed union. These high-risk stress fractures, including tension-side femoral neck fractures and anterior tibial cortex fractures, require aggressive treatment to prevent the sequelae of poor healing.
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46

United States. National Aeronautics and Space Administration., ed. NASA-UVa light aerospace alloy and structures technology program (LAS2ST): A progress report, January 1, 1993 to June 30, 1993, NASA-LaRC grant NAG-1-745. Charlottesville, VA: School of Engineering & Applied Science, University of Virginia, 1993.

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47

United States. National Aeronautics and Space Administration., ed. NASA-UVa light aerospace alloy and structures technology program (LAS2ST): A progress report, January 1, 1993 to June 30, 1993, NASA-LaRC grant NAG-1-745. Charlottesville, VA: School of Engineering & Applied Science, University of Virginia, 1993.

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48

Effect of tensile mean stress on fatigue behavior of single-crystal and directionally solidified superalloys. [Washington, DC]: National Aeronautics and Space Administration, 1991.

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49

United States. National Aeronautics and Space Administration., ed. NASA-UVa light aerospace alloy and structures technology program (LAS2ST): A progress report, January 1, 1993 to June 30, 1993, NASA-LaRC grant NAG-1-745. Charlottesville, VA: School of Engineering & Applied Science, University of Virginia, 1993.

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50

Yang, Xiaofan. Corrosion and passivation of molybdenum-bearing alloys. 1995.

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