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Contribution of individual load cycles to crack growth under aircraft spectrum loading: Sunder, R. Proc. Conf. Advances in Fatigue Lifetime Predictive Techniques, San Francisco, California, USA, 24 Apr. 1990 176–190

Book ID: 107891601
Publisher: Elsevier Science
Year: 1993
Tongue: English
Weight: 182 KB
Volume: 15
Category: Article
ISSN: 0142-1123
DOI: 10.1016/0142-1123(93)90122-7

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