Nonlinear Analysis of Damaged Stiffened Fuselage Shells Subjected to Combined Loads
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 ; 1045-1076
NASA CONFERENCE PUBLICATION ; 3274//pt2
01.01.1994
32 pages
In 2 pts
Aufsatz (Konferenz)
Englisch
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Nonlinear Response and Residual Strength of Damaged Stiffened Shells Subjected to Combined Loads
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