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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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YE Lin, LIU Cunliang, ZHU Andong, ZHOU Tianliang.
Influence of compact-ribbed passage on trailing-edge cutback film cooling performance
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(3): 125174-125174.
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YE Lin, LIU Cunliang, YANG Yuquan, HUANG Rong, ZHU Andong.
Effect of V-shaped ribs on film cooling characteristics of trailing-edge cutback
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(6): 124181-124181.
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DU Yufeng, LIN Jun, WANG Xunnian, XIONG Neng.
Analysis of modes of disturbances in compressible fluid in subsonic wind tunnel
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(6): 124424-124424.
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GAO Limin, JIANG Heng, GE Ning, YANG Guanhua, CHEN Shun.
Experiment on static/dynamic characteristics of fast-response pressure sensitive paint based on lifetime method
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(3): 124120-124120.
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GAO Limin, JIANG Heng, GE Ning, YANG Guanhua, ZHAO Chongxiang.
A high frequency dynamic pressure optical calibration system based on sinusoidal wave and its application
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(10): 123667-123667.
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LIN Jingzhou, XIE Futian, ZHONG Jun, CHEN Lei, CHEN Liusheng.
Pressure sensitive paint test technique in hypersonic wind tunnel
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2017, 38(7): 120890-120890.
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JU Lian, BAI Junqiang, GUO Bin, CUI Xiaochun, LI Xinglong.
Effect of geometry parameters on flow field quality in a transonic slotted wind tunnel
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016, 37(5): 1440-1453.
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XU Lincheng, WANG Gang, WU Jie, YE Zhengyin.
Uncertainty Analysis of Airfoil Wind Tunnel Tests with Automatic Differentiation
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2014, 35(8): 2102-2111.
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GAO Limin, WU Ya'nan, HU Xiaoquan, GAO Jie, LIU Bo.
Intensity-based Fast Response PSP Technique and Its Applications
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2014, 35(3): 607-623.
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LI Guoshuai, ZHOU Qiang, LIU Xiang, JIN Biqing, GAO Limin, MA Husheng, XIONG Jian.
Experimental Research of Pressure Sensitive Paint Performance and Calibration Technique
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2013, 34(2): 227-234.
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Fanzhaolin;Cui Naiming;Yun qilin;Yin Luping.
TRANSONIC WALL INTERFERENCE CORRECTIONS FOR CIVIL AIRCRAFT MODEL TESTS
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1994, 15(2): 129-135.
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Li Hua-xing;He Jia-ju;Zuo Pei-chu;Xu Min.
EXPERIMENTAL TECHNIQUE RESEARCH ON LOW SUPERSONIC TESTING WITH AN ADAPTIVE FLEXIBLE-WALLED WIND TUNNEL
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1993, 14(7): 381-387.
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Cui Naiming.
AN ENGINEERING CORRECTION METHOD FOR TUNNEL WALL INTERFERENCE AND STING-SUPPORT INTERFERENCE IN HIGH SPEED WIND TUNNELS
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1990, 11(12): 523-527.
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Liu Xiaorong;Fan Jiechuan;Yang Qiusheng .
A WALL CORRECTION AT HIGH ANGLE OF ATTACK IN LOW-SPEED WIND TUNNEL USING WALL PRESSURE SIGNATURE METHOD
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1988, 9(6): 277-283.
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