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NTL Classification:NTL-AVIATION-AVIATION;NTL-AVIATION-Aviation Safety/Airworthiness;
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Abstract:The objective of the present investigation is to determine the mode I stress-intensity factors along two symmetric surface cracks emanating from a centrally located hole in a rectangular plate (the so-called Round Robin Problem) using the domain integral ;See also PB98-146186. Prepared in cooperation with Northwestern Univ., Evanston, IL. Center for Quality Engineering and Failure Prevention. Sponsored by Federal Aviation Administration, Washington, DC. Office of Aviation Research.;pg 16
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