STRUCTURAL MECHANICS AND MATERIALS - Residual Strength Prediction of Aircraft Fuselages Using Crack-Tip Opening Angle Criterion
AIAA journal ; 40 , 3 ; 566-575
2002
Aufsatz (Zeitschrift)
Englisch
Prediction of residual strength and curvilinear crack growth in aircraft fuselages
Tema Archiv | 2002
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