Effects of squealer rim height on aerodynamic losses downstream of a high-turning turbine rotor blade

Author:

Lee Sang Woo,Chae Byoung Joo

Publisher

Elsevier BV

Subject

Fluid Flow and Transfer Processes,Mechanical Engineering,Aerospace Engineering,Nuclear Energy and Engineering,General Chemical Engineering

Reference18 articles.

Cited by 66 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

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3. A study of angle parametric optimization of the composite honeycomb on turbine blade tip;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2024-04-22

4. Uncertainty quantification in effects of geometric deviations on heat transfer and film cooling of blade squealer tip with pressure-side coolant;International Communications in Heat and Mass Transfer;2024-04

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