AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL-VTOL - Fatigue Crack Growth Prediction Under Spectrum Load Using Crack Driving Force DK* (TN)
AIAA journal ; 44 , 2 ; 396-398
2006
Aufsatz (Zeitschrift)
Englisch
AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL-VTOL - Multiple Crack Analysis in Finite Plates
Online Contents | 2006
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