Equivalent initial flaw size testing and analysis of transport aircraft skin splices-Reference-Cited by-同舟云学术

Equivalent initial flaw size testing and analysis of transport aircraft skin splices

Published:2003-03 Issue:3 Volume:26 Page:279-290
ISSN:8756-758X
Container-title:Fatigue Fracture of Engineering Materials and Structures
language:en
Short-container-title:Fat Frac Eng Mat Struct

Author:

FAWAZ S. A.

Publisher

Wiley

Subject

Mechanical Engineering,Mechanics of Materials,General Materials Science

Link

http://onlinelibrary.wiley.com/wol1/doi/10.1046/j.1460-2695.2003.00637.x/fullpdf

Reference26 articles.

1. 1 R. Piascik, and S. Willard (1997 ) The characterization of widespread fatigue damage in the fuselage riveted lap splice joint. NASA-TP-97-206257.

2. 2 J. Newman (1992 )FASTRAN-II-A fatigue crack growth structural analysis program. NASA TM-104159.

3. 3 J. Harter (1999 )AFGROWUsers guide and technical manual. AFRL-VA-WP-TR-1999-3016.

4. 4 J. Rudd, and T. Gray (1976 ) Equivalent initial quality method. AFFDL-TM-76-83-FBE.

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