[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] |
WANG Bin, WANG Haitao, WANG Yufeng, ZHANG Wenwu.
Water-assisted laser scanning machining test of thermal barrier coating
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(4): 525353-525353.
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[3] |
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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[4] |
XIA Kailong, HE Qing, ZHANG Yusheng.
Measurement method of turbine blade film aperture based on infrared thermal imaging and shrinkage law
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(12): 426271-426271.
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[5] |
LUO Shibin, MIAO Zhichao, SONG Jiawen.
Influencing factors of active cooling at leading edge of hypersonic vehicles
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(12): 627023-627023.
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[6] |
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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[7] |
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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[8] |
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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[9] |
LI Zuobiao, WEN Fengbo, TANG Xiaolei, SU Liangjun, WANG Songtao.
Prediction of single-row hole film cooling performance based on deep learning
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(4): 524331-524331.
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[10] |
ZHAO Yuanyuan, ZENG Fei, LI Yang, GAN Mingyu, SHI Shengxian.
3D measurement technique for film cooling holes based on light-field imaging
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(10): 524158-524158.
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[11] |
TANG Liang, HU Jinhua, LIU Jiwu, LI Ping, ZHOU Lixin, YANG Baoe.
Experimental study on oblique jet wall impingement and geometrical parameter modeling of liquid film
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(12): 124061-124061.
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[12] |
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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[13] |
ZHU Peiyuan, SONG Liming, LI Jun, FENG Zhenping.
Effects of location and geometry of slot on film cooling performance of end-wall
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2017, 38(9): 520942-520942.
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[14] |
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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[15] |
GUO Wei, DONG Lihong, WANG Huipeng, XU Binshi.
Research progress of damage estimation for turbine blades based on infrared thermographic technology
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016, 37(2): 429-436.
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