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《JOURNAL OF ENGINEERING THERMOPHYSICS》 1996-03
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EXPERIMENTAL INVESTIGATION ON THE FLOW AND HEAT TRANSFER IN A COOLING PASSAGE OF GAS TURBINE BLADE

GU Weizao; TU Jianping; LIU Wenyan(Institute of Engineering Thermophysics,Academia Sinica, Beijing 100080)LIU Xiaofeng; SHENG Rongchang ;ZHAO Dongmei; LING Jinru(Institute 608, Incorporation General of Aeronautical Industry,Zhuzhou 412002)  
In this paper the test results of Pressure distribution,resistance under heating and without heating flow fields,distribution of local heat transfer coefficient in the cooling passages ofa modeled gas turbine blade are presented.
【CateGory Index】: TK471
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【References】
Chinese Journal Full-text Database 5 Hits
1 CAO Zhi-ting,GUO Wen,PAN Bing-hua,LIU Song(China Gas Turbine Establishment,Chengdu 610500,China);Optimization of Turbine Blade Cooling Design with iSIGHT[J];燃气涡轮试验与研究;2012-04
2 LI Qing-gang,PENG Rong-qiang (School of Energy & Environment Xihua University,Chengdu 610039,China);U-shaped Channel Design of Turbine Blade Cooling[J];汽轮机技术;2008-02
3 ZHANG Qing,MENG Guang (School of Machinery Engineering,Shanghai Jiaotong University,Shanghai 200030,China);Numerical Simulation Progress on the Air-Cooling of Turbine Blade[J];燃气轮机技术;2004-04
4 QI Wen kai, CHEN Wei,GAO De ping (Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China);Analysis of turbine disc response in thermal-mechanical loads[J];机械设计与制造;2004-01
5 GU Weizao ;LIU Wenyan(Institute of Engineering Thermophysics, Chinese Academy of Sciences, Beijing 100080);EXPERIMENTAL INVESTIGATION ON THE COOLING PERFORMANCE OF THREE GAS TURBINE BLADE INTERNAL PASSAGES[J];工程热物理学报;1998-02
【Co-references】
Chinese Journal Full-text Database 10 Hits
1 YU Kua-hai1,2,YUE Zhu-feng1,Yang Xi3 (1.School of Mechanics Civil Engineering and Architecture,Northwestern Polytechnical University,Xi'an 710072,China;2.School of Planning and Archtectural Engineering,Henan University of Science and Technology,Luoyang 471003,China;3.School of Material,Northwestern Polytechnical University,Xi'an 710072,China);Aerodynamic and heat transfer design optimization for cooling turbine blade[J];计算力学学报;2010-02
2 NI Meng~(1,2),ZHU Hui-ren~2,QIU Yun~2,XU Du-chun~2,LIU Song-ling~2(1.Department of Mechanical Engineering,The University of Hong Kong,Hong Kong2.Northwestern Polytechnical University,Xi~,an,710072,China);Review of aero-turbine blade cooling technologies[J];燃气轮机技术;2005-04
3 ZHANG Qing,MENG Guang (School of Machinery Engineering,Shanghai Jiaotong University,Shanghai 200030,China);Numerical Simulation Progress on the Air-Cooling of Turbine Blade[J];燃气轮机技术;2004-04
4 XIANG Anding,Luo Xiaoqiang,ZHU Huiren,XU Duchun,LIU Songling(Northwestern Polytechnical University,Xi'an710072,China);Turbine Blade Surface Heat Transfer and Film Cooling Measurements in a Turbine Cascade with Injection on Surface[J];航空动力学报;2002-05
5 Gao Jin (Customer Representative in Xi'an Aero - Engine Corporation,Xi'an 710021);Calculation of 3D and Quasi - 3D Temperature Distribution in Air Cooling Turbine Blade[J];航空发动机;2002-03
6 DENG Hong wu, TAO Zhi, XU Guo qiang, DING Shui ting ( Dept. of Jet Propul., Beijing Univ. of Aeronaut. & Astronaut., Beijing 100083, China );Experimental investigation on heat transfer within a rotating ribbed serpentine passage with stagger angles[J];大连理工大学学报;2001-S1
7 WU Hong1,TAO Zhi2,XU Guo-qiang2DING Shui-ting2 1.Department of Engineering Mechanics,Tsinghua University,Beijing100084,China; 2.4th Dept.,Beijing University of Aeronautics and Astronautics,Beijing100083,China;Experiments of Impinging Cooling in Leading Edge of Rotating Blades with Outflow Film[J];航空动力学报;2000-04
8 Yang Huitao and Cao Yuzhang (4th Dept.Beijing University of Aeronautics and Astronautics,Beijing 210016);NUMERICAL SIMULATION OF FILM COOLING IN ROTATING BLADE TIP[J];航空动力学报;1998-03
9 Gao Chao Chu Xiaorong Wang Baoguan (Dept of Power Engineering,Nanjing Univ.of Aeronautics and Astronautics,Nanjing,210016);THE EXPERIMENTAL INVESTIGATION OF IMPINGING COOLING IN THE COMBUSTION CHAMBER[J];推进技术;1998-01
10 GU Weizao; TU Jianping; LIU Wenyan(Institute of Engineering Thermophysics,Academia Sinica, Beijing 100080)LIU Xiaofeng; SHENG Rongchang ;ZHAO Dongmei; LING Jinru(Institute 608, Incorporation General of Aeronautical Industry,Zhuzhou 412002);EXPERIMENTAL INVESTIGATION ON THE FLOW AND HEAT TRANSFER IN A COOLING PASSAGE OF GAS TURBINE BLADE[J];工程热物理学报;1996-03
【Secondary References】
Chinese Journal Full-text Database 10 Hits
1 QIU Fei;BU Kun;LI Shifeng;Ding Xiaoyi;Modern design and Manufacturing Technology Key Laboratory of the Ministry of Education,Northwestern Polytechnical University;Research Laboratory for Turbine,China Gas Turbine Establishment,Aviation Industry Corporation of China;;Structural optimization of a tenon intake window for a single crystal turbine blade based on residual stress[J];哈尔滨工程大学学报;2017-02
2 CHEN Lei;GUO Wen;SU Yun-liang;CAO Zhi-ting;China Gas Turbine Establishment;;Applications of iSIGHT optimization technology in blade cooling design[J];燃气涡轮试验与研究;2016-05
3 CAI Wenbo;LI Zhao;Equipment Department of Navy;;Research on Improving Testing System for the Water Flow of Aeroengine High-pressure Turbine Guide-vanes[J];计测技术;2015-04
4 LIU Yangpeng;XU Guoqiang;LI Haiwang;TIAN Yitu;National Key Laboratory of Science and Technology on Aero-Engines,Beijing University of Aeronautics and Astronautics;;Experiment of air flow behavior and heat transfer characteristics in microchannels with different aspect ratios[J];北京航空航天大学学报;2015-07
5 LI Shi-feng;WEI Gang;SUN Fei-yan;LIU Qiang-jun;HE Ai-jie;CHEN Yong-xi;Research Laboratory for Turbine,China Gas Turbine Establishment,Aviation Industry Corporation of China;;Detail-structure optimization of single crystal turbine blade under the condition of geometric and dynamic constraints[J];航空动力学报;2015-01
6 JIANG Dong-po;ZHAO Jun-ming;Harbin Turbine Company Limited;;Design for the Cooling Structure of Turbine Blades of a Certain Type Heavy-duty Gas Turbine[J];汽轮机技术;2014-05
7 WANG Qinglei;DONG Liping;Beijing Institute of Space Mechanics & Electricity;China University of Geosciences;;Flow field analysis on the erosion prone parts of the drilling equipment-stator and rotor[J];北京交通大学学报;2014-04
8 HAN Jun;WEN Fengbo;WANG Songtao;HONG Bowen;Engine Aerodynamic Research Center,Harbin Institute of Technology;;Heat transferring design for the first guide blade of a high pressure turbine[J];哈尔滨工业大学学报;2013-09
9 WU Yan-long,LI Tao,WANG Xiang-feng,HUANG Hong-yan,YAN Pei-gang,HAN Wan-jin(College of Energy Science and Engineering,Harbin Institute of Technology,Harbin 150001,China);Numerical Study on the Aerodynamic Performance of Three-stage Turbine Inner Flow Field with Cooling Air Mixing[J];汽轮机技术;2012-01
10 WANG Ying,YU Zhao-peng(AVIC Beijing KeeVen Aviation Instrument Co.,Ltd,Beijing 100086,China);Optimization design for the turbine disk of a gas engine[J];机械设计与制造;2010-05
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