Analysis of working blade crack failure and optimal scheme for engine high pressure turbine

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Journal of Shenyang Aerospace University ›› 2016, Vol. 33 ›› Issue (1) : 18-23.

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{{article.zuoZheEn_L}}. {{article.title_en}}. {{journal.qiKanMingCheng_EN}}. 2016, 33(1): 18-23

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2015-04-14	2016-04-01	2016-02-25
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2016-02-25

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