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E. S. Folias, Int. J. Fracture Mech., 1 (1965) 104.
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R. W. Nichols, W. H. Irvine, A. Quirk and E. Bevitt, Proc. First Int. Conf. on Fracture, Sendai, Japan, 1673, 1966.
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W. J. Crichlow and R. H. Wells, Crack Propagation and Residual Static Strength of Fatigue-Cracked Titanium and Steel Cylinders, ASTM STP 415, 25, 1967.
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R. G. Forman, Experimental Program to Determine Effect of Crack Buckling and Specimen Dimensions on Fracture Toughness of Thin Sheet Materials, AF Flight Dynamics Lab Report AFFDL-TR 65-146, Wright Patterson AFB, Ohio, 1965.
W. G. Degnan, P. D. Dripchak and C. J. Matvsovitch, Fatigue Crack Propagation in Aircraft Materials, U.S. Army Aviat. Mat. Lab. Fort Eustis, Va., Technical Report 66-9, March 1966.
G. T. Hahn and A. R. Rosenfield, Sources of Fracture Toughness: The Relation Between K 1c and the Ordinary Tensile Properties of Metals, ASTM STP 432, 5, 1968.
A. Quirk, A Maximum Stress Theory for the Failure of Pressure Components Containing Through Thickness Defects, UKAEA Report AHSB(S) R 134, 1967.
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G. T. Hahn and A. R. Rosenfield, Acta Met., 13 (1965) 293.
A. R. Rosenfield, P. K. Dai and G. T. Hahn, Proceedings of the First International Conference on Fracture, T. Yokobori, et al., eds., 1 (1966) 223.