Damage Tolerance in Aircraft Structures: A Symposium Presented at the 73rd Annual Meeting, American Society for Testing and Materials

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ASTM International, 1971
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Elber W The significance of fatigue crack closure, vol 486, ASTM STP; 1971, p. 230-42

Contents

Effect of Thickness on the Fracture Toughness of 7075 Aluminum in the
16
The Influence of Curvature on Stress Intensity at the Tip of a Circumferential
39
Fatigue Crack Propagation in Stiffened Panelsc c poe jr
79
Material Toughness and Residual Strength of Damage Tolerant Aircraft
98
An Approach to Predicting the Growth to Failure of Fatigue Cracks Sub
122
Initiation and Growth of Fatigue Cracks in and Residual Strength of
144
Development of the Failsafe Design Features of the DC10t swift
164
The Ballistic Damage Characteristics and Damage Tolerance of Wing Struc
215
The Significance of Fatigue Crack Closurewolf elber
230
Crack Propagation in Helicopter Rotor Bladesm j rich
243
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