Research on the applicability of the Paris theory to aircraft riveted stiffened structures is reported. This research was carried out in two stages: evaluation of the stress intensity factor K in stiffened panels and measurement of crack growth rate in stiffened and unstiffened panels.
Theoretical and Experimental Research on the Fatigue Crack Propagation in Stiffened Panels. An Evaluation of the Paris Theory
1974
83 pages
Report
Keine Angabe
Englisch
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