题名 | A Crack-closure model for predicting fatigue crack growth under aircraft loading, methods and models for predicting fatigue crack growth under random loading |
链接 | http://www.scopus.com/inward/record.url?eid=2-s2.0-0019627111&partnerID=10&rel=R3.0.0&md5=cb26c32e4b8c31f275e62a9b9834229a |
本帖最后由 Okalo 于 2014-12-15 18:28 编辑
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