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Books on the topic 'Crack initiation and propagation'

Author: Grafiati

Published: 4 June 2021

Last updated: 15 February 2022

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1

Newman, J. C. Small-crack effects in high-strength aluminum alloys: A NASA/CAE Cooperative program. Langley Research Center, 1994.

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2

ATV, Korrosionscentralen. Environmental effects in fatigue crack initiation and propagation. Commission of the European Communities, 1989.

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3

Qing, Li. The role of active corrosion in fatigue crack initiation and early stages of crack propagation. UMIST, 1996.

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4

Dessureault, Mia. Observations of fatigue crack initiation and propagation in structural adhesive joints. National Library of Canada, 1995.

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5

Kitamura, Takayuki. Stochastic modeling of crack initiation and short-crack growth under creep and creep-fatigue conditions. NASA, 1989.

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6

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

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7

Sih, G. C., ed. Multiscale Fatigue Crack Initiation and Propagation of Engineering Materials: Structural Integrity and Microstructural Worthiness. Springer Netherlands, 2008. http://dx.doi.org/10.1007/978-1-4020-8520-8.

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8

Castelli, Michael G. Characterization of damage progression in SCS-6/Timetal 21S [0]₄ under thermomechanical fatigue loadings. National Aeronautics and Space Administration, 1994.

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9

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

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10

Gotsis, Pascal K. Progressive fracture of fiber composite build-up structures. National Aeronautics and Space Administration, 1997.

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11

Gotsis, Pascal K. Progressive fracture of fiber composite build-up structures. National Aeronautics and Space Administration, 1995.

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12

Gotsis, Pascal K. Progressive fracture of fiber composite build-up structures. National Aeronautics and Space Administration, 1997.

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13

Gotsis, Pascal K. Progressive fracture of fiber composite build-up structures. National Aeronautics and Space Administration, 1995.

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14

Gotsis, Pascal K. Progressive fracture of fiber composite thin shell structures under internal pressure and axial loads. National Aeronautics and Space Administration, 1996.

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15

Gotsis, Pascal K. Progressive fracture of fiber composite thin shell structures under internal pressure and axial loads. National Aeronautics and Space Administration, 1996.

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16

Orange, Thomas W. Elevated temperature crack propagation. National Aeronautics and Space Administration, 1993.

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17

Lewicki, David G. Gear crack propagation investigations. National Aeronautics and Space Administration, 1996.

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18

Sourcebook on fatigue crack propagation: Thresholds and crack closure. Engineering Materials Advisory Services, 1993.

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19

Abdul-Salam, Ezzet Hameed. Fatigue crack propagation in mild steel. University of Salford, 1991.

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20

Sih, G. C. Mechanics of Fracture Initiation and Propagation. Springer Netherlands, 1991. http://dx.doi.org/10.1007/978-94-011-3734-8.

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21

Chudnovsky, A. On governing equations for crack layer propagation. National Aeronautics and Space Administration, 1988.

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22

Pommier, Sylvie, Anthony Gravouil, Alain Combescure, and Nicolas Moës. Extended Finite Element Method for Crack Propagation. John Wiley & Sons, Inc., 2013. http://dx.doi.org/10.1002/9781118622650.

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23

Richmond, M. J. A stripyield model including effects of hold periods at constant load. National Aerospace Laboratory, 1993.

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24

Jie, Ouyang. A study of the mechanism of striation formation and fatigue crack growth in engineering alloys. [s.n.], 1988.

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25

Revill, G. W. An automatic crack measuring system using the direct-current potential-difference method. Aeronautical Research Laboratories, 1985.

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26

Lewicki, David G. Effect of rim thickness on gear crack propagation path. National Aeronautics and Space Administration, 1996.

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27

Babiloglu, Erol. A numerical study of dynamic crack propagation in composites. Naval Postgraduate School, 1992.

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28

Lewicki, David G. Effect of rim thickness on gear crack propagation path. National Aeronautics and Space Administration, 1996.

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29

Edwards, P. R. Short-crack growth behaviour in various aircraft materials. AGARD, 1990.

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30

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

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31

Alfred, Buch. Ratio of crack initiation life to total fatigue life and use of local strain approach for prediction of fatigue life. Technion Israel Institute of Technology, Dept. of Aeronautical Engineering, 1988.

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32

Alfred, Buch. Prediction of fatigue life of notched specimens under aircraft loading and importance of the relative method in the case of local strain approach. Technion Israel Institute of Technology, Dept. of Aeronautical Engineering, 1986.

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33

Van Der Sluys, WA, RS Piascik, and R. Zawierucha, eds. Effects of the Environment on the Initiation of Crack Growth. ASTM International, 1997. http://dx.doi.org/10.1520/stp1298-eb.

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34

Bos, M. J. Critical appraisal of the McDonnell Douglas closure model for predicting fatigue crack growth. Aeronautical Research Laboratory, 1991.

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35

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

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36

Hudak, S. J. A comparison of single-cycle versus multiple-cycle proof testing strategies. George C. Marshall Space Flight Center, 1990.

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37

Lewicki, David G. Effect of speed (centrifugal load) on gear crack propagation direction. National Aeronautics and Space Administration, Glenn Research Center, 2001.

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38

Yan, M. G. Microscopic studies on fatigue crack propagation and fracture characteristic near crack tip region in engineering alloys. [s.n.], 1989.

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39

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. An assessment of fatigue damage and crack growth prediction techniques. AGARD, 1994.

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40

W, Smith Stephen. Simulation of fatigue crack initiation at corrosion pits with EDM notches. National Aeronautics and Space Administration, Langley Research Center, 2003.

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41

Smith, Stephen W. Simulation of fatigue crack initiation at corrosion pits with EDM notches. National Aeronautics and Space Administration, Langley Research Center, 2003.

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42

Lof, C. J. Useful lifetime prediction software for plane semi-cracks in 3-D solid configurations. National Aerospace Laboratory, 1986.

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43

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

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44

DuBois, Marc L. Action potential: Biophysical and cellular context, initiation, phases, and propagation. Nova Science, 2010.

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45

Wawrzynek, Paul. FRANC2D: a two-dimensional crack propagation simulator: Version 2.7 user's guide. Langley Research center, 1994.

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46

Wu, Xinhua. Microstructural effects on fatigue crack propagation in a strength titanium aluminide. University of Birmingham, 1996.

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47

Hegen, D. An element-free Galerkin method for crack propagation in brittle materials. Eindhoven University of Technology, 1997.

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48

Johannes Petrus Bernardus Nicolaas Derks. Cold fluid driven crack propagation: Thermo-mechanical behaviour of rock caverns. Delft University Press, 1997.

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49

Mendelson, Alexander. Analysis of mixed-mode crack propagation using the boundary integral method. National Aeronautics and Space Administration, 1986.

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50

Wallace, William. Methods for crack growth testing in gas turbine engine disc materials. National Aeronautical Establishment, 1987.

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