The comparison of complex load sequences tested at several stress levels by fractographic examination-Reference-Cited by-同舟云学术

The comparison of complex load sequences tested at several stress levels by fractographic examination

Published:2005-08 Issue:4 Volume:12 Page:586-603
ISSN:1350-6307
Container-title:Engineering Failure Analysis
language:en
Short-container-title:Engineering Failure Analysis

Author:

Pell R.A.,Mazeika P.J.,Molent L.

Publisher

Elsevier BV

Subject

General Engineering,General Materials Science

Reference14 articles.

1. Molent L, Ogden R, Pell R. F/A-18 FS488 bulkhead fatigue coupon test program. Defence Science and Technology Organisation, DSTO-TR-0941, Australia; 2000

2. Molent L, Mills T, Pell R. F/A-18 FS488 bulkhead fatigue coupon test program – part 2. Defence Science and Technology Organisation, DSTO-TR-1464, July; 2003

3. Pell RA, Molent L, Green AJ. The fractographical comparison of F/A-18 aluminium alloy 7050-T7451 bulkhead representative coupons tested under two fatigue load spectra at several stress levels. DSTO-TR-1547, February; 2004

4. Dickinson T, Molent L. Validation of fatigue damage models used for F/A-18 life assessment using fatigue coupon test results. Defence Science and Technology Organisation, DSTO-TR-0940, Australia; 2000

5. White P, Barter S, Molent L. Probabilistic fracture prediction based on aircraft specific fatigue test data. In: Proceedings of the 6th joint FAA/DoD/NASA aging aircraft conference, San Diego; 2002

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