Fatigue Crack Growth and Residual Strength Analysis of Twist Spectrum Loaded Integrally Stiffened Panels Simulating a Lower Wing Skin Two Bay Crack Scenario
Symposium; 20th, International Committee on Aeronautical Fatigue; ICAF '99 structural integrity for the next millennium ; 1999 ; Bellevue, WA
1999-01-01
2 pages
Conference paper
English
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