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1

Richard, Hans Albert, and Manuela Sander. Fatigue Crack Growth. Cham: Springer International Publishing, 2016. http://dx.doi.org/10.1007/978-3-319-32534-7.

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2

M, Fisher Douglas, Holka Donna, and Lewis Research Center, eds. Variables controlling fatigue crack growth of short cracks. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1986.

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3

Krausz, A. S., and K. Krausz. Fracture Kinetics of Crack Growth. Dordrecht: Springer Netherlands, 1988. http://dx.doi.org/10.1007/978-94-009-1381-3.

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4

Recho, Naman. Fracture Mechanics and Crack Growth. Hoboken, NJ, USA: John Wiley & Sons, Inc., 2012. http://dx.doi.org/10.1002/9781118387184.

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5

Krausz, A. S. Fracture Kinetics of Crack Growth. Dordrecht: Springer Netherlands, 1988.

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6

K, Krausz, ed. Fracture kinetics of crack growth. Dordrecht: Kluwer Academic Publishers, 1988.

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7

Recho, Naman. Fracture mechanics and crack growth. London: ISTE Ltd., 2012.

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8

Prasad, N. N. V. Thermomechanical crack growth using boundary elements. Southampton: WIT Press, 1998.

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9

Heinrich, Gert, Reinhold Kipscholl, and Radek Stoček, eds. Fatigue Crack Growth in Rubber Materials. Cham: Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-030-68920-9.

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10

Mi, Yaoming. Three-dimensional analysis of crack growth. Southampton, UK: Computational Mechanics Publications, 1996.

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11

Mi, Y. Three-dimensional analysis of crack growth. Southampton: Computational Mechanics, 1995.

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12

Monahan, C. C. Early fatigue crack growth at welds. Southampton, UK: Computational Mechanics Publications, 1995.

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13

1947-, Yau Jen-Fu, and United States. National Aeronautics and Space Administration, eds. Elevated temperature crack growth: Annual report. Cincinnati, Ohio: General Electric, Aircraft Engine Business Group, Advanced Technology Programs Dept., 1985.

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14

Monahan, Craig C. Early fatigue crack growth at welds. Ashurst: Computational Mechanics, 1995.

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15

H, Van Stone R., and United States. National Aeronautics and Space Administration., eds. Elevated temperature crack growth: Final report. [Washington, DC]: National Aeronautics and Space Administration, 1992.

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16

Kubair, D. V. Crack growth: Rates, prediction, and prevention. New York: Nova Science Publishers, 2012.

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17

N, Malik S., and United States. National Aeronautics and Space Administration, eds. Elevated temperature crack growth: Annual report. Cincinnati, Ohio: General Electric, Aircraft Engine Business Group, Advanced Technology Programs Dept., 1987.

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18

N, Nemeth Noel, Gyekenyesi John P, and NASA Glenn Research Center, eds. Slow crack growth of brittle materials with exponential crack-velocity formulation. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2002.

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19

H, Swain M., and Langley Research Center, eds. Fatigue crack initiation and small crack growth in several airframe alloys. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

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20

Center, Langley Research, and United States. National Aeronautics and Space Administration., eds. Use of marker bands for determination of fatigue crack growth rates and crack front shapes in the pre-corroded coupons. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

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21

Song, Ji-Ho, and Chung-Youb Kim. Expert System for Fatigue Crack Growth Predictions Based on Fatigue Crack Closure. Singapore: Springer Singapore, 2022. http://dx.doi.org/10.1007/978-981-16-8036-6.

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22

Pete, Kantzos, Telesman Jack, and United States. National Aeronautics and Space Administration., eds. Fatigue crack growth and crack bridging in SCS-6/Ti-24-11. [Washington, D.C: National Aeronautics and Space Administration, 1995.

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23

J, Hudak S., Dexter R. J, and Langley Research Center, eds. Measurement and analysis of critical crack tip processes during fatigue crack growth. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1985.

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24

J, Hudak S., Dexter R. J, and Langley Research Center, eds. Measurement and analysis of critical crack tip processes during fatigue crack growth. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1985.

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25

Tang, Ping, and Jm Leor Zhang. Fatigue crack growth: Mechanisms, behavior, and analysis. Hauppauge, N.Y: Nova Science Publishers, 2012.

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26

Reuter, WG, JH Underwood, and JC Newman, eds. Surface-Crack Growth: Models, Experiments, and Structures. 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959: ASTM International, 1990. http://dx.doi.org/10.1520/stp1060-eb.

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27

Carpinteri, Alberto. Mechanical damage and crack growth in concrete. Dordrecht: Springer Netherlands, 1986. http://dx.doi.org/10.1007/978-94-009-4350-6.

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28

Ellyin, Fernand. Fatigue Damage, Crack Growth and Life Prediction. Dordrecht: Springer Netherlands, 1996. http://dx.doi.org/10.1007/978-94-009-1509-1.

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29

Radu, Vasile. Stochastic Modeling of Thermal Fatigue Crack Growth. Cham: Springer International Publishing, 2015. http://dx.doi.org/10.1007/978-3-319-12877-1.

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30

F, Lignelli Alphonse, ed. Fatigue crack growth: Mechanics, behavior, and prediction. Hauppauge, NY: Nova Science Publishers, 2009.

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31

Nosair, Shawky Ibrahim Mohamed. Fatigue crack growth in aluminium alloy structures. Salford: University of Salford, 1986.

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32

Healy, Joseph Cornelius. Short fatigue crack growth at elevated temperature. Birmingham: Universityof Birmingham, 1989.

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33

Ellyin, Fernand. Fatigue damage, crack growth, and life prediction. London: Chapman & Hall, 1997.

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34

N, Brewer David, United States. National Aeronautics and Space Administration., and United States. Army Aviation Systems Command., eds. Controlled crack growth specimen for brittle systems. [Washington, D.C.]: NASA, 1990.

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35

Portela, A. Dual boundary element analysis of crack growth. Southampton, UK: Computational Mechanics Publications, 1993.

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36

Crack growth in concrete using boundary elements. Southampton, UK: Computational Mechanics Publications, 1997.

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37

United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., ed. Fracture toughness and crack growth of Zerodur. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

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38

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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39

1938-, Reuter Walter G., Underwood John H, Newman J. C, and Symposium on Surface-Crack Growth: Experiments, and Structures (1988 : Sparks, Nev.), eds. Surface-crack growth: Models, experiments, and structures. Philadelphia, PA: ASTM, 1990.

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40

P, Phillips E., Everett R. A, and Langley Research Center, eds. Fatigue life and crack growth prediction methodology. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.

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41

Fatigue Damage, Crack Growth and Life Prediction. Dordrecht: Springer Netherlands, 1996.

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42

A, Meyers C., Stinson H. C, and George C. Marshall Space Flight Center., eds. Comparison of two computer codes for crack growth analysis: NASCRAC versus NASA/FLAGRO. [Marshall Space Flight Center, Ala.]: National Aeronautics and Space Administration, George C. Marshall Space Flight Center, 1989.

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43

Edwards, P. R. Short-crack growth behaviour in various aircraft materials. Neuilly sur Seine: Agard, 1990.

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44

Edwards, P. R. Short-crack growth behaviour in various aircraft materials. Neuilly sur Seine, France: AGARD, 1990.

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45

Center, Langley Research, ed. Analyses of fatigue crack growth and closure near threshold conditions for large-crack behavior. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

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46

Center, Langley Research, ed. Analyses of fatigue crack growth and closure near threshold conditions for large-crack behavior. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

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47

Newman, JC, and RS Piascik, eds. Fatigue Crack Growth Thresholds, Endurance Limits, and Design. 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959: ASTM International, 2000. http://dx.doi.org/10.1520/stp1372-eb.

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48

Knee, N. The effects of microstructure on fatigue crack growth. Carnforth, Lancashire, England: Parthenon Press, 1986.

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49

Jack, Telesman, Kantzos Peter, and United States. National Aeronautics and Space Administration., eds. Fatigue crack growth in unidirectional metal matrix composite. [Washington, D.C.]: NASA, 1990.

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50

Portela, A. Dual boundary element incremental analysis of crack growth. Southampton: Wessex Institute of Technology, Damage Tolerance Division, 1992.

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