Prediction of Fatigue Crack Growth under Flight-Simulation Loading with the Modified Corpus Model
International symposium, Advanced structural integrity methods for airframe durability and damage tolerance ; 1994 ; Hampton; VA
Advanced structural integrity methods for airframe durability and damage tolerance ; 3274//pt2 ; 547-562
NASA CONFERENCE PUBLICATION ; 3274//pt2
1994-01-01
16 pages
In 2 pts
Conference paper
English
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