Numerical simulation of film cooling effectiveness with one inlet and double outlet hole on leading edge

被引：0
|
作者：
Li, Guang-Chao [1 ]
Zhang, Wei [1 ]
Wang, Cheng-Jun [1 ]
Peng, Da-Wei [1 ]
Wang, Jian-Ming [1 ]
Xu, Zhi-Hui [1 ]
机构：
[1] Liaoning Key Laboratory of Digital Technology Simulation and Test Technique, School of Aero Dynamics and Energy Engineering, Shenyang Aerospace University, Shenyang 110136, China
来源：
Hangkong Dongli Xuebao/Journal of Aerospace Power | 2010年 / 25卷 / 10期
关键词：
D O I：
暂无
中图分类号：
学科分类号：
摘要：
引用
收藏
页码：2255 / 2260
相关论文
共 50 条
  • [31] Numerical simulation on impingement and film composite cooling of blade leading edge model for gas turbine
    Liu, Zhao
    Ye, Lv
    Wang, Changyee
    Feng, Zhenping
    APPLIED THERMAL ENGINEERING, 2014, 73 (02) : 1432 - 1443
  • [32] Experimental research on film cooling characteristics of cylindrical hole and expanding hole on the leading edge
    Zhu, Hui-Ren
    Zhang, Xia
    Liu, Cun-Liang
    Hangkong Dongli Xuebao/Journal of Aerospace Power, 2010, 25 (07): : 1464 - 1470
  • [33] Film temperature and effectiveness measurements on a cylindrical leading edge film cooling model
    Sohn, DK
    Teng, SY
    Han, JC
    HEAT TRANSFER 1998, VOL 6: GENERAL PAPERS, 1998, : 571 - 576
  • [34] Experimental investigation on film cooling of expanded hole at both inlet and outlet with various injection angles
    Li, Guang-Chao
    Zhu, Hui-Ren
    Fan, Hui-Ming
    Hangkong Dongli Xuebao/Journal of Aerospace Power, 2009, 24 (05): : 1000 - 1005
  • [35] NUMERICAL SIMULATION OF IMPINGING COOLING ON THE LEADING EDGE OF A TURBINE BLADE
    Cheng, Keyong
    Huai, Xiulan
    Cai, Jun
    Guo, Zhixiong
    PROCEEDINGS OF THE ASME INTERNATIONAL MECHANICAL ENGINEERING CONGRESS AND EXPOSITION, 2011, VOL 10, PTS A AND B, 2012, : 1077 - 1085
  • [36] Influence of film cooling jet inlet boundary condition on large eddy simulation of model turbine blade leading edge
    Bazdidi-Tehrani, Farzad
    Bohlooli, Nima
    Jadidi, Mohammad
    PROGRESS IN COMPUTATIONAL FLUID DYNAMICS, 2015, 15 (04): : 214 - 227
  • [37] EXPERIMENTAL AND NUMERICAL STUDIES ON LEADING EDGE FILM COOLING PERFORMANCE: EFFECTS OF HOLE EXIT SHAPE AND FREESTREAM TURBULENCE
    Funazaki, Ken-ichi
    Kawabata, Hirokazu
    Takahashi, Daichi
    Okita, Yoji
    PROCEEDINGS OF THE ASME TURBO EXPO 2012, VOL 4, PTS A AND B, 2012, : 1223 - +
  • [38] A NUMERICAL INVESTIGATION OF NEW FILM COOLING HOLE CONFIGURATION AT THE LEADING EDGE OF ASYMMETRICAL TURBINE BLADE: PART B
    Benabed, Mustapha
    COMPUTATIONAL THERMAL SCIENCES, 2016, 8 (05): : 429 - 443
  • [39] Experimental investigation of film cooling effectiveness on leading edge with various geometries
    School of Power and Energy, Northwestern Polytechnical Univ., Xi'an 710072, China
    Tuijin Jishu, 2008, 2 (153-157):
  • [40] Influence of aerodynamic parameters on film cooling effectiveness on the vane leading edge
    School of Power and Energy, Northwestern Polytechnical University, Xi'an 710072, China
    Hangkong Dongli Xuebao, 2008, 2 (215-220):
12345