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Effect of attack angle and jet height on impingement and film composite cooling of turbine blade leading edge

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Effect of attack angle and jet height on impingement and film composite cooling of turbine blade leading edge

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Title: Effect of attack angle and jet height on impingement and film composite cooling of turbine blade leading edge
Author: Liu, Zhao; Ye, Lv; Yang, Xing; Feng, Zhenping
Description: This paper is part of the conference proceedings from the 22nd International Symposium on Air Breathing Engines.
Bookmark: http://hdl.handle.net/2374.UC/745710
Date: 2015

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Attribution-NonCommercial-NoDerivs 3.0 United States Except where otherwise noted, this item's license is described as Attribution-NonCommercial-NoDerivs 3.0 United States

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