| [1] |
Ming REN, Cunliang LIU, Kun DU, Li ZHANG, Huiren ZHU, Bolun ZHANG.
Film cooling with compound angle holes in leading edge of twisted turbine blade
[J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(18): 128315-128315.
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| [2] |
YANG Yuquan, LIU Cunliang, ZHANG Jie, HUANG Rong.
Effect of mass flow ratios on film cooling characteristics of endwall: Experimental study
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(7): 124399-124399.
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| [3] |
WANG Jin, SUN Jie, ZHAO Zhanming, ZHANG Bo, REN Xiaodong, XIE Gongnan.
Research on film cooling performance of sister hole based on structural parameter analysis
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(7): 124775-124775.
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| [4] |
CHEN Dawei, ZHU Huiren, LI Huatai, LIU Haiyong, ZHOU Daoen.
Effect of unsteady wake on full coverage film cooling effectiveness for a turbine blade
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2019, 40(3): 122651-122651.
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| [5] |
ZHOU Junhui, ZHANG Jingzhou.
Effects of partial blockage inside film holes on overall cooling effectiveness of an integrated impingement-fin-film cooling configuration on blade pressure side
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016, 37(9): 2729-2738.
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| [6] |
ZHU Xingdan, TAN Xiaoming, GUO Wen, ZHANG Jingzhou, WANG Yongming.
Investigation of Airflow Allocation Inside High Pressure Turbine Rotor Blade
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2014, 35(12): 3273-3782.
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| [7] |
DING Yang, CHANG Haiping, DU Zhineng.
Investigation on Characteristics of Multiple Rows of Opposite Lateral Ejection Angle Film Cooling
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2013, 34(11): 2472-2481.
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| [8] |
DING Yang, CHANG Haiping.
Analysis of Turbine Blade Cooling Effectiveness
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2013, 34(1): 46-51.
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| [9] |
Li Guangchao;Zhang Wei;Peng Dawei;Wang Chengjun.
Numerical Simulation of Film Cooling Effectiveness with Conical Expanded Branch Holes
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2010, 31(7): 1360-1365.
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| [10] |
Yao Yu;Zhang Jingzhou;He Fei;Guo Wen.
Numerical Investigation on Film Cooling Effectiveness of Converging Slot Hole at Turbine Blade Suction Surface
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2010, 31(6): 1115-1120.
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| [11] |
Liu Cunliang;Zhu Huiren;Bai Jiangtao;Xu Duchun.
Experimental Research on Film Cooling Characteristics of Converging-expandingHole Rows on Turbine Blade Surface
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2010, 31(4): 687-693.
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| [12] |
You Liangping;Tao Yujia;Cai Jun;Liang Shiqiang;Huai Xiulan;Gu Weizao.
Experiment of Composite Cooling on Leading Edge of Turbine Blade
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2009, 30(9): 1618-1623.
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| [13] |
Liu Cunliang;Zhu Huiren;Bai Jiangtao;Xu Duchun.
Film Cooling Characteristics of Converging-xpanding Hole with Transient Liquid Crystal Measurement Technique
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2009, 30(5): 812-818.
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| [14] |
HAN Zhen-xing;Kiyoshi Suenaga;LIU Shi.
Experimental Research on Film Cooling Effectivenesses at Different Blowing Ratios
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2004, 25(6): 551-555.
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| [15] |
ZHU Hui-ren;XU Du-chun;LIU Song-ling.
EFFECTS OF HOLE SHAPE ON FILM COOLING EFFECTIVENESS
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2002, 23(1): 75-78.
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