Aerodynamic optimal design of non-axisymmetric endwall for a turbine cascade

被引:0
|
作者
Key Laboratory for Thermal Science and Power Engineering, Department of Thermal Engineering, Tsinghua University, Beijing 100084, China [1 ]
机构
来源
Kung Cheng Je Wu Li Hsueh Pao | 2007年 / 4卷 / 589-591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
相关论文
共 50 条
  • [31] Effect of non-axisymmetric endwall contouring and swirling inlet flow on film cooling performance of turbine endwall
    Du, Kun
    Zhang, Rongxia
    Jia, Yihao
    Liu, Cunliang
    Sunden, Bengt
    INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 2024, 229
  • [32] Effects of non-axisymmetric endwall contouring on aerothermal performance of a gas turbine blade endwall with a purge flow
    Tao, Zhi
    Yu, Boyang
    Li, Yixing
    Song, Liming
    Li, Jun
    INTERNATIONAL JOURNAL OF THERMAL SCIENCES, 2021, 164
  • [33] The nonaxismmetric endwall aerodynamic optimization design for a large turbine cascade with a midgap
    He, Lei
    Liu, Hao
    Zhu, Xiaocheng
    Hua, Ouyang
    Du, Zhaohui
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2019, 233 (03) : 1000 - 1010
  • [34] ADVANCED NON-AXISYMMETRIC ENDWALL CONTOURING FOR AXIAL COMPRESSORS BY GENERATING AN AERODYNAMIC SEPARATOR - PART II: EXPERIMENTAL AND NUMERICAL CASCADE INVESTIGATION
    Hergt, Alexander
    Dorfner, Christian
    Steinert, Wolfgang
    Nicke, Eberhard
    Schreiber, Heinz-Adolf
    PROCEEDINGS OF ASME TURBO EXPO 2009, VOL 7, PTS A AND B, 2009, : 121 - 131
  • [35] THE AERODYNAMIC OPTIMIZATION DESIGN OF TURBINE CASCADE WITH NONAXISYMMETRIC ENDWALL AND EXPERIMENTAL VALIDATIONS
    Liu, Hao
    Shen, Xin
    Zhu, Xiaocheng
    Du, Zhaohui
    Yang, Hong
    Yang, Rui
    PROCEEDINGS OF THE ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2017, VOL 2A, 2017,
  • [36] GENERATIVE MODEL BASED PARAMETERIZATION FOR MORE EFFICIENT AERODYNAMIC OPTIMIZATION OF NON-AXISYMMETRIC ENDWALL
    Li, Cunxi
    Song, Liming
    Guo, Zhendong
    Li, Jun
    Feng, Zhenping
    PROCEEDINGS OF ASME TURBO EXPO 2024: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, GT2024, VOL 12D, 2024,
  • [37] A NEW TEST FACILITY TO INVESTIGATE FILM COOLING ON A NON-AXISYMMETRIC CONTOURED TURBINE ENDWALL, PART I: INTRODUCTION AND AERODYNAMIC MEASUREMENTS
    Puetz, Franz
    Kneer, Johannes
    Schulz, Achmed
    Bauer, Hans-Joerg
    ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2015, VOL 2A, 2015,
  • [38] Numerical Investigation of the Effect of Purge Flow on Aerodynamic Performance and Film Cooling Effectiveness on a Rotating Turbine with Non-Axisymmetric Endwall Contouring
    Schobeiri, M. T.
    Lu, K.
    Han, J. C.
    PROCEEDINGS OF THE ASME TURBO EXPO 2012, VOL 4, PTS A AND B, 2012, : 413 - 423
  • [39] Application of non-axisymmetric endwall contouring to conventional and high-lift turbine airfoils
    Praisner, T. J.
    Allen-Bradley, E.
    Grover, E. A.
    Knezevici, D. C.
    Sjolander, S. A.
    Proceedings of the ASME Turbo Expo 2007, Vol 6, Pts A and B, 2007, : 653 - 661
  • [40] Experimental test of a 3D parameterized vane cascade with non-axisymmetric endwall
    Guo, Zhendong
    Bu, Hongyan
    Song, Liming
    Li, Jun
    Feng, Zhenping
    AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 85 : 429 - 442