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The Elastic-Plastic Finite Element Alternating Method ... - Springer

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Application Predictions of the NIST Multiple Site DamageExperiments.ReferencesAtluri, S. N. (1982): Path Independent Integrals in <strong>Finite</strong> <strong>Elastic</strong>ityand Inelasticity, With Body Forces, Inertia, and ArbitraryCrack-Face Conditions. Engineering Fracture Mechanics 16, 341±364Atluri, S. N. (1986): Energetic Approaches and Path-IndependentIntegrals, In: Atluri, S. N. (ed): Computational <strong>Method</strong>s in theMechanics of Fracture, pp 123±165. North Holland PublishersAtluri, S. N.; Sampath, S. G.; Tong, P. (1992): Durability of MetalAir Frame Structures. Atlanta, GA: Technical PublicationsAtluri, S. N.; Sampath, S. G.; Tong, P. (1991): Structural Integrityof Aging Airplanes. Berlin, Heidelberg, New York: <strong>Springer</strong>Broek, D. (1993): <strong>The</strong> Effects of Multi-site Damage on the ArrestCapability of Aircraft Fuselage Structures. FractuREearch TechnicalReport No. 9302Brust, F. W.; Nishioka, T.; Nakagaki, M.; Atluri, S. N. (1985):Further Studies on <strong>Elastic</strong>-<strong>Plastic</strong> Stable Fracture Utilizing T Integral. Engineering Fracture Mechanics 22, 1079±1103Brust, F. W.; McGowan, J. J.; Atluri, S. N. (1986a): A combinedNumerical/Experimental Study of Ductile Crack Growth After aLarge Unloading Using T , J, and CTOA Criteria. EngineeringFracture Mechanics Vol. 23, No. 3, 537±550Brust, F. W.; Atluri, S. N. (1986b): Studies on Creep CrackGrowth Using the T Integral. Engineering Fracture MechanicsVol. 23, No. 3, 551±574Brust, F. W.; Nakagaki, M.; Spring®eld, C. W. (1989): IntegralParameters for <strong>The</strong>rmal Fracture. Engineering Fracture MechanicsVol. 33, No. 4, 561±579Brust, F. W.; Nakagaki, M.; Gilles, P. (1990): Comparison of<strong>Elastic</strong>-<strong>Plastic</strong> Fracture Mechanics Techniques. ASTM STP 1074,448±469Brust, F. W.; Majumdar, B. S. (1994): Load History Effects onCreep Crack Growth. Eng Fracture Mech Vol 49, No. 6, 809±837Brust, F. W. 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D.; Han, Y. F.; Yan, M. G. (1992): <strong>The</strong> T -Integral as aCharacteristic Parameter for Large Scale Creep Crack Growth.Engineering Fracture Mechanics, Vol. 43 (5), 827±836Nikishov, G. P.; Atluri, S. N. (1987): Calculation of fracture mechanicsparameters for arbitrary three-dimensional crack by theequivalent domain integral method. Int. J. Num. Meth. Engg. 24pp. 1801±1821Nishioka, T.; Atluri, S. N. (1983): Analytical Solution for Embeddedelliptical cracks, and <strong>Finite</strong> <strong>Element</strong> <strong>Alternating</strong> <strong>Method</strong>for Elliptical Surface Cracks, Subjected to Arbitrary Loadings.Engineering Fracture Mechanics 17, 247±268Okada, H.; Suzuki, Y.; Ma, L.; Lam, P. W.; Pyo, C. R.; Atluri, S. N.;Kobayashi, A. S.; Tan, P. (1995): Plane Stress Crack Growth andT Integral - An Experimental-Numerical Analysis. To be presentedat the ICES-95, Hawaii, August. Also to appear in theproceedingsPyo, C. R.; Okada, H.; Atluri, S. N. (1994a): Residual StrengthPrediction for Aircraft Panels with Multiple Site Damage, Usingthe EPFEAM for Stable Crack Growth Analysis. FAA Center ofExcellence Report by Georgia Institute of Technology, NovemberPyo, C. R.; Okada, H.; Atluri, S. N. (1994b): An <strong>Elastic</strong>-<strong>Plastic</strong><strong>Finite</strong> <strong>Element</strong> <strong>Alternating</strong> <strong>Method</strong> for Analyzing Wide-SpreadFatigue Damage in Aircraft Structures. FAA Center of ExcellenceReport by Georgia Institute of Technology, NovemberRice, J. R. (1968): A Path Independent Integral and ApproximateAnalysis of Strain Concentration by Notches and Cracks. Journalof Applied Mechanics, 35, 379±386Shenoy, V. B.; Potyondy, D. O.; Atluri, S.N. (1994): A <strong>Method</strong>ologyfor Computing Nonlinear Fracture Parameters for a BulgingCrack in a Pressurized Aircraft Fuselage. FAA Center of ExcellenceReport by Georgia Institute of Technology, MarchSingh, R.; Park, J. H.; Atluri, S. N. (1994): Residual Life andStrength Estimates of Aircraft Structural Components with MSD/MED. Proceedings of the FAA/NASA International Symposiumon Advanced Structural Integrity <strong>Method</strong>s for Airframe Durabilityand Damage Tolerance, Ed. C. E. Harris, pp. 771±784, Sept.Willis, J. R. (1975): Equations of Motion for Propagating Cracks.In <strong>The</strong> Mechanics and Physics of Fracture, <strong>The</strong> Metal Society, pp.57±67379Part III of this report will be published in a following issue.

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