FEM-DBEM approach for crack propagation in a low pressure aeroengine turbine vane segment

出版年份 2016 全文链接

标题

作者

关键词

FEM-DBEM, Crack growth, Thermo-mechanical fatigue, Superposition principle, Turbine vane

出版物

Volume 86, Issue -, Pages 143-152

出版商

Elsevier BV

发表日期

2016-06-19

DOI

10.1016/j.tafmec.2016.05.004

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