Numerical investigation on the effect of upstream ramps on film cooling performance with compound angles

被引:0
|
作者
D. Zheng
X. Wang
Q. Yuan
机构
[1] Xi’an Jiaotong University,
[2] University of Toronto,undefined
来源
关键词
film cooling; upstream ramps; compound angles; adiabatic cooling effectiveness;
D O I
暂无
中图分类号
学科分类号
摘要
This paper presents a numerical investigation on the concept for improving film cooling performance by placing a ramp upstream the film hole with compound angle. Eight cases with different geometry models are investigated, including the compound angles of 15°, 30°, 45° and the distances between the upstream ramps and film holes (upstream distances) of 5 mm, 10 mm, and 15 mm. The effect of compound angle and upstream distance on film cooling performance is studied. The cases of film cooling on a flat plate, film cooling with compound angle, and film cooling with an upstream ramp are also presented as a contrast. The film cooling performance is evaluated at the density ratio of 0.97 with the blowing ratios ranging from 1.0 to 2.0. Results obtained show that the film cooling performance with compound angle is greatly improved by the upstream ramp, especially in the region downstream the film hole. Both the entrainment of coolant and modified kidney vortices are observed in the case of the novel geometry. The film cooling performance is greatly improved by the dual effect of coolant entrainment and modified kidney vortices. In addition, the film cooling performance is influenced by compound angle and upstream distance. With the increase of compound angle, the lateral adiabatic cooling effectiveness rises. With the increase of the upstream distance, the lateral adiabatic cooling effectiveness goes down.
引用
收藏
页码:195 / 208
页数:13
相关论文
共 50 条
  • [21] COOLING EFFECTIVENESS FOR A SHAPED FILM COOLING HOLE AT A RANGE OF COMPOUND ANGLES
    Haydt, Shane
    Lynch, Stephen
    PROCEEDINGS OF THE ASME TURBO EXPO: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, 2018, VOL 5C, 2018, : 281 - 295
  • [22] Cooling Effectiveness for a Shaped Film Cooling Hole at a Range of Compound Angles
    Haydt, Shane
    Lynch, Stephen
    JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2019, 141 (04):
  • [23] Numerical Investigation on Supersonic Film Cooling Performance with Discrete Film Holes
    Zhou, Junfei
    AIAA JOURNAL, 2023, 61 (01) : 48 - 62
  • [24] Direct numerical simulation of the 7-7-7 film cooling at a range of compound angles
    Bin, Yuanwei
    Yang, Xiang I. A.
    INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 2024, 231
  • [25] Investigation on the Film Cooling Performance of Diffuser Shaped Holes with Different Inclination Angles
    Zhai, Ying-Ni
    Liu, Cun-Liang
    He, Yi-Hong
    Zhou, Zhi-Xiang
    INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES, 2017, 34 (02) : 123 - 139
  • [26] Effects of upstream ramp on the performance of film cooling
    Chen, Shuping P.
    Chyu, Minking K.
    Shih, Tom I-P
    INTERNATIONAL JOURNAL OF THERMAL SCIENCES, 2011, 50 (06) : 1085 - 1094
  • [27] Numerical investigation on the effects of the divided steps on film cooling performance
    Zheng, Daren
    Wang, Xinjun
    Zhang, Feng
    Yuan, Qi
    APPLIED THERMAL ENGINEERING, 2017, 124 : 652 - 662
  • [28] Numerical Investigation on Film Cooling Performance of Fusiform Diffusion Holes
    An, Bai-Tao
    Liu, Jian-Jun
    JOURNAL OF HEAT TRANSFER-TRANSACTIONS OF THE ASME, 2018, 140 (12):
  • [29] Numerical investigation of adiabatic film cooling effectiveness through compound angle variations
    Tamang, Sajan
    Kwon, Hwabhin
    Choi, Jaehun
    Ligrani, Phillip
    Lee, Je-Hyun
    Jung, Yeon-Gil
    Park, Heesung
    NUMERICAL HEAT TRANSFER PART A-APPLICATIONS, 2020, 78 (10) : 595 - 618
  • [30] EXPERIMENTAL AND NUMERICAL INVESTIGATION ON FILM COOLING PERFORMANCE AND FLOW STRUCTURE OF FILM HOLES
    Cao, Nan
    Li, Xue
    Wu, Ze-yu
    Luo, Xiang
    PROCEEDINGS OF THE ASME TURBO EXPO: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, 2019, VOL 5B, 2019,