Studies of effect of thickness on fatigue crack growth under single-overloading conditions
ACTA AERONAUTICA ET ASTRONAUTICA SINICA -SERIES A AND B- ; 18 , 2 ; 153-156
1997-01-01
4 pages
Article (Journal)
Unknown
DDC: | 629.13 |
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Online Contents | 2001
Engineering Index Backfile | 1928
The effect of overloading sequences on landing gear fatigue damage
Tema Archive | 2009
|Modelling of initial fatigue crack growth and crack branching under fretting conditions
Tema Archive | 1999
|