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Influence of tip clearance and cavity depth on heat transfer in a cutback squealer tip
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering ( IF 1.0 ) Pub Date : 2020-10-20 , DOI: 10.1177/0954410020964690 Weijie Wang 1 , Shaopeng Lu 1 , Hongmei Jiang 2 , Qiusheng Deng 1 , Jinfang Teng 1 , and Wensheng Yu 1
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering ( IF 1.0 ) Pub Date : 2020-10-20 , DOI: 10.1177/0954410020964690 Weijie Wang 1 , Shaopeng Lu 1 , Hongmei Jiang 2 , Qiusheng Deng 1 , Jinfang Teng 1 , and Wensheng Yu 1
Affiliation
Numerical simulations are conducted to present the aerothermal performance of a turbine blade tip with cutback squealer rim. Two different tip clearance heights (0.5%, 1.0% of the blade span) and t...
中文翻译：
叶尖间隙和空腔深度对缩窄式传热器叶尖传热的影响
进行了数值模拟，以展示具有缩减的啸叫轮缘的涡轮叶片尖端的空气热性能。两种不同的叶尖间隙高度（叶片跨度的 0.5%、1.0%）和 t...
更新日期：2020-10-20
中文翻译：
叶尖间隙和空腔深度对缩窄式传热器叶尖传热的影响
进行了数值模拟，以展示具有缩减的啸叫轮缘的涡轮叶片尖端的空气热性能。两种不同的叶尖间隙高度（叶片跨度的 0.5%、1.0%）和 t...
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