Fatigue Crack Growth in 2024-T3 Aluminum under Tensile and Transverse Shear Stresses
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 ; 891-910
NASA CONFERENCE PUBLICATION ; 3274//pt2
01.01.1994
20 pages
In 2 pts
Aufsatz (Konferenz)
Englisch
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Fatigue Crack Growth under Mixed Loading of Tensile and In-plane Shear Modes
Online Contents | 2003
|Fatigue Crack Growth under Mixed Loading of Tensile and In-plane Shear Modes
British Library Online Contents | 2003
|