applied fracture mechanics

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Good Practice for Fatigue Crack Growth Curves Description 227Kłysz, S. (2001). Fatigue crack growth in aircraft materials and constructional steel withoverload consideration, (in Polish), Air Force Institute of Technology Publication, ISSN1234-3544, Warsaw, PolandKłysz, S. & Lisiecki, J. (2009). Report of fatigue crack growth rate testing, (in Polish),Laboratory for Material Strength Testing Report, No. 1d/09, Air Force Institute ofTechnology, Warsaw, PolandKłysz, S.; Lisiecki, J. & Bąkowski, T. (2010a). Modification of the east-squares method fordescription of fatigue crack propagation, Research Works of Air Force Institute ofTechnology, ISSN 1234-3544, No.27, pp. 85-91, Warsaw, PolandKłysz, S.; Lisiecki, J. & Klimaszewski, S. (2010b). Analysis of crack propagation curvedescription for ORLIK aircraft fuselage skin material, (in Polish), Technical News, No1(31), 2(32), pp.148-151, Lvov, UkraineKłysz, S.; Lisiecki, J.; Leski, A. & Bąkowski, T. (2012). Least squares method modification<strong>applied</strong> to the NASGRO equation, J. of Applied and Theoretical Mechanics, Warsaw,Poland (in printing)Kłysz, S.; Lisiecki, J.; Leski, A. & Bąkowski, T. (2012). Modification of the LSM criteriato approximate test data for fatigue crack growth rate, J. of Applied and TheoreticalMechanics, Warsaw, Poland (in printing)Lisiecki, J. & Kłysz, S. (2007). Report of fatigue crack growth rate testing, (in Polish),Laboratory for Material Strength Testing Report, No. 8c/07, Air Force Institute ofTechnology, Warsaw, PolandMurakami, Y. (Ed.). (1987). Stress Intensity Factors Handbook, The Society of MaterialsScience, Pergamon Press, JapanNASGRO® Fracture Mechanics and Fatigue Crack Growth Analysis Software. (2006). v5.0,NASA-JSC and Southwest Research InstituteNewman, J.C. jr. (1992). Fastran II – A fatigue crack growth structures analysis program,NASA TN 104159, Langley Res. Centre, Hampton, VAParis, P.C. & Erdogan, A. (1963). A critical analysis of crack propagation laws, J. Bas. Engng,No.85, pp. 528-534Skorupa, M. (1996). Empirical trends and prediction models for fatigue crack growthunder variable amplitude loading, ECN-R-96-007, Netherlands Energy ResearchFoundationSmith, R.A. (Ed.). (1986). Fatigue Crack Growth. 30 Years of Progress, Pergamon Press,Cambridge, UKTaheri, F.; Trask, D. & Pegg, N. (2003). Experimental and analytical investigation of fatiguecharacteristics of 350WT steel under constant and variable amplitude loadings, J. ofMarine Structure, No.16, pp. 69-91Wheeler, O.E. (1972). Spectrum loading and crack growth, Trans. ASME, J. Basic Eng., 94, 181White, P.; Molent, L. & Barter, S. (2005). Interpreting fatigue test results using a probabilistic<strong>fracture</strong> approach, Int. J. of Fatigue, No.27, pp. 752-767
228Applied Fracture MechanicsWillenborg, J.; Engle, R.M. & Wood, H.A. (1971). A crack growth retardation model using aneffective stress concept, AFFDL-TR-71-1Zhao, T. & Jiang Y. (2008). Fatigue of 7075-T651 aluminum alloy, Int. J. of Fatigue, No.30, pp.834-849
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Applied Fracture Mechanicshttp://dx
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PrefaceKnowledge accumulated in the
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Section 1Computational Methods of F
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Chapter 4Fracture of Dental Materia
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Fracture Mechanics Based Models of
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