Numerical life estimation after fatigue failure of a complex component-Reference-Cited by-同舟云学术

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Numerical life estimation after fatigue failure of a complex component

Published:2005-06 Issue:6 Volume:28 Page:547-556
ISSN:8756-758X
Container-title:Fatigue Fracture of Engineering Materials and Structures
language:en
Short-container-title:Fat Frac Eng Mat Struct

Author:

OTEGUI J. L.,LOPEZ MONTENEGRO H.,MARQUEZ A. A.

Publisher

Wiley

Subject

Mechanical Engineering,Mechanics of Materials,General Materials Science

Link

http://onlinelibrary.wiley.com/wol1/doi/10.1111/j.1460-2695.2005.00897.x/fullpdf

Reference19 articles.

1. 1 Failure analysis of compressor C111 . Report GIE 2603-01/03, GIE S.A., Mar del Plata , Argentina, 2003 .

2. 3 "Standard Test Method for Measurement of Fatigue Crack Growth Rates," ASTM Designation E647-88. Vol. 03.01 , 1988 . ASTM Annual Standards , American Society for Testing and Materials. pp. 636 -654 .

3. Heat Transfer Characteristics of an Obliquely Impinging Circular Jet

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. A weight function method for the assessment of partially closed three-dimensional plane cracks;Engineering Fracture Mechanics;2008-10

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