AERODYNAMIC LOSS PENALTY PRODUCED BY FILM COOLING TRANSONIC TURBINE-BLADES

被引:31
|
作者
HALLER, BR [1 ]
CAMUS, JJ [1 ]
机构
[1] UNIV CAMBRIDGE,WHITTLE LAB,CAMBRIDGE,ENGLAND
关键词
D O I
10.1115/1.3239535
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
引用
收藏
页码:198 / 205
页数:8
相关论文
共 50 条
  • [41] Investigation of aerodynamic loss mechanism on turbine leading edge with slot film cooling based on entropy analysis
    Hu, Jingyu
    Zhang, Yanfeng
    Zhang, Jianshe
    Zhu, Miaoyi
    Zhu, Junqiang
    INTERNATIONAL JOURNAL OF THERMAL SCIENCES, 2025, 207
  • [42] Numerical investigation on aerodynamic loss of turbine cascade with converging slot hole film cooling at suction surface
    Yao, Yu
    Zhang, Jingzhou
    He, Fei
    Guo, Wen
    Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 2010, 31 (07): : 1312 - 1317
  • [43] EXPERIMENTAL INVESTIGATION OF SWEEPING JET FILM COOLING IN A TRANSONIC TURBINE CASCADE
    Hossain, Mohammad A.
    Asar, Munevver E.
    Gregory, James W.
    Bons, Jeffrey P.
    PROCEEDINGS OF THE ASME TURBO EXPO: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, 2019, VOL 5B, 2019,
  • [44] Process and analysis of cooling structure design for gas turbine rotor blades with film cooling
    Luo, Lei
    Chen, Shuo
    Liu, Wei
    Wang, Songtao
    Wang, Zhongqi
    Zhongguo Dianji Gongcheng Xuebao/Proceedings of the Chinese Society of Electrical Engineering, 2015, 35 (16): : 4112 - 4121
  • [45] THE INFLUENCE OF BOUNDARY LAYER STATE AND TRAILING EDGE WEDGE ANGLE ON THE AERODYNAMIC PERFORMANCE OF TRANSONIC TURBINE BLADES
    Rossiter, A. D.
    Pullan, G.
    Melzer, A. P.
    PROCEEDINGS OF ASME TURBO EXPO 2022: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, GT2022, VOL 10B, 2022,
  • [46] New Supersonic Loss Model for the Preliminary Design of Transonic Turbine Blades and the Influence of Pitch
    Teia, Luis
    JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2020, 142 (04):
  • [47] The Influence of Boundary Layer State and Trailing Edge Wedge Angle on the Aerodynamic Performance of Transonic Turbine Blades
    Rossiter, A. D.
    Pullan, G.
    Melzer, A. P.
    JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2023, 145 (04):
  • [48] Aerodynamic performance of a family of three high pressure transonic turbine blades at off-design incidence
    Corriveau, D.
    Sjolander, S. A.
    Proceedings of the ASME Turbo Expo 2005, Vol 6, Pts A and B, 2005, : 451 - 464
  • [49] EFFECT OF FILM COOLING HOLES SHAPE OF HELIUM TURBINE BLADES IN HTGR
    Sun, Xiaokai
    Peng, Wei
    PROCEEDINGS OF THE 24TH INTERNATIONAL CONFERENCE ON NUCLEAR ENGINEERING, 2016, VOL 3, 2016,
  • [50] Effect of coolant temperature and mass flow on film cooling of turbine blades
    Garg, VK
    Gaugler, RE
    INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 1997, 40 (02) : 435 - 445