Fatigue crack propagation in the wing to fuselage connection of the new trainer aircraft M346-Reference-Cited by-同舟云学术

Fatigue crack propagation in the wing to fuselage connection of the new trainer aircraft M346

Published:2006-12 Issue:12 Volume:29 Page:1000-1009
ISSN:8756-758X
Container-title:Fatigue & Fracture of Engineering Materials and Structures
language:en
Short-container-title:Fat Frac Eng Mat Struct

Author:

LANCIOTTI A.,NIGRO F.,POLESE C.

Publisher

Wiley

Subject

Mechanical Engineering,Mechanics of Materials,General Materials Science

Link

http://onlinelibrary.wiley.com/wol1/doi/10.1111/j.1460-2695.2006.01062.x/fullpdf

Reference15 articles.

1. 1 JSSG-2006 (1998 ) Joint service specification guide, aircraft structures . Department of Defence.

2. 2 NASGRO 4.02 (2002 ) Fracture mechanics and fatigue crack growth analysis software . NASA Johnson Space Center and Southwest Research Institute.

3. 4 A. Lanciotti, F. Nigro, and C. Polese, Damage tolerance characterization of the wing to fuselage connection of the aircraft M346 . (In Italian). Roma, 15-19 September 2003.

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