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Experimental Investigation of Leading Edge Jet Impingement with Varying Jet Geometries and Inlet Supply Conditions for Turbine Cooling Applications

机译：具有不同喷射几何和入口供应条件的前沿喷射冲击的实验研究

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作者
Jordan, C. Neil.;
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作者单位

Baylor University.;

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授予单位 Baylor University.;
学科
学位 M.S.M.E.
年度 2012
页码 163 p.
总页数 163
原文格式 PDF
正文语种 eng
中图分类 AAI1511728;
关键词
Gas turbine heat transfer; Leading edge impingement; Liquid crystal thermography; Shaped impinging jets;

机译：燃气轮机传热;前缘冲击;液晶热成像;形状撞击喷气机;
入库时间 2022-08-17 12:01:54

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2. TURBINE BLADE LEADING EDGE IMPINGEMENT COOLING FROM NORMAL OR TANGENTIAL JETS WITH CROSSFLOW EFFECT [J] . Wright Lesley, Wang Nian, Zhang Mingjie, Frontiers in Heat and Mass Transfer . 2019,第1期

机译：涡轮叶片前缘冲击从正常或切线喷射带有横流效果
3. Turbine Blade Leading Edge Cooling With One Row of Normal or Tangential Impinging Jets [J] . Nian Wang, Andrew F. Chen, Mingjie Zhang, Journal of Heat Transfer . 2018,第6期

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4. LEADING EDGE IMPINGEMENT WITH RACETRACK SHAPED JETS AND VARYING INLET SUPPLY CONDITIONS [C] . C. Neil Jordan, Cassius A. Elston, Lesley M. Wright, ASME turbo expo: turbine technical conference and exposition . 2013

机译：RACETRACK形状的凸出物和变化的进气口条件对前沿冲击
5. Jet Diameter Effect on Impingement Jet Cooling on the Leading Edge of a Turbine Blade. [D] . Haider, Syed Abbas. 2015

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6. Conjugate Heat Transfer Investigation on Swirl-Film Cooling at the Leading Edge of a Gas Turbine Vane [O] . Haifen Du, Ziyue Mei, Jiayao Zou, 2019

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7. TURBINE BLADE LEADING EDGE IMPINGEMENT COOLING FROM NORMAL OR TANGENTIAL JETS WITH CROSSFLOW EFFECT [O] . Lesley M. Wright, Nian Wang, Mingjie Zhang, 2019

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8. Engine Investigation of an Air-Cooled Turbine Rotor Blade Incorporating Impingement-Cooled Leading Edge, Chordwise Passages, and a Slotted Trailing Edge [R] . Dengler, R. P., Yeh, F. C., Gauntner, J. W., 1972

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Experimental Investigation of Leading Edge Jet Impingement with Varying Jet Geometries and Inlet Supply Conditions for Turbine Cooling Applications

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