FILM COOLING FROM SHORT HOLES WITH SISTER HOLE INFLUENCE

被引:0
|
作者
Ely, Marc J. [1 ]
Jubran, B. A. [1 ]
机构
[1] Ryerson Univ, Dept Aerosp Engn, Aerothermal Management Lab, Toronto, ON M5B 2K3, Canada
关键词
IN-CROSS-FLOW; JET;
D O I
暂无
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
This paper reports a computational analysis on the effect of sister hole control on film cooling from short holes. The proposed method includes surrounding a primary injection hole by two or four smaller sister holes to actively maintain flow adhesion along the surface of the blade. A numerical study using the realizable k-epsilon turbulence model led to the determination that the use of sister holes significantly improves adiabatic effectiveness by countering the primary vortical flow structure. Research was carried out to determine the optimum hole configuration, arriving at the conclusion that placing sister holes slightly downstream of the primary injection hole improves the near-hole effectiveness, while placing sister holes slightly upstream of the primary hole improves downstream effectiveness. Similar results were found in evaluating both long and short hole geometries with a significantly less coherent flow field arising from the short hole. However, on the whole, the sister hole approach to film cooling was found to offer viable improvements over standard cooling regimes.
引用
收藏
页码:1185 / 1196
页数:12
相关论文
共 50 条
  • [1] FILM COOLING FROM CIRCULAR AND ELLIPTICAL EXIT SHAPED HOLES WITH SISTER HOLE INFLUENCE
    Khajehhasani, Siavash
    Jubran, B. A.
    PROCEEDINGS OF THE ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2013, VOL 3B, 2013,
  • [2] A Numerical Evaluation of the Performance of Film Cooling from a Circular Exit Shaped Hole with Sister Holes Influence
    Khajehhasani, Siavash
    Jubran, Bassam Ali
    HEAT TRANSFER ENGINEERING, 2016, 37 (02) : 183 - 197
  • [3] Influence of Hole Inlet Geometry on the Film Cooling Effectiveness from Shaped Film Cooling Holes
    Watson, Travis B.
    Vinton, Kyle R.
    Wright, Lesley M.
    Crites, Daniel C.
    Morris, Mark C.
    Riahi, Ardeshir
    PROCEEDINGS OF THE ASME TURBO EXPO: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, 2019, VOL 5B, 2019,
  • [4] FILM COOLING FROM NOVEL SISTER SHAPED SINGLE-HOLES
    Khajehhasani, Siavash
    Jubran, Bassam
    PROCEEDINGS OF THE ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2014, VOL 5B, 2014,
  • [5] FILM COOLING OF COMPOUND ANGLE UPSTREAM SISTER HOLES
    Abd Alsalam, Sana
    Jubran, Bassam
    PROCEEDINGS OF THE ASME TURBO EXPO: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, 2019, VOL 5A, 2019,
  • [6] An Experimental Study of Sister Holes Film Cooling With Various Secondary-to-Primary Hole Diameter Ratios
    Zhu, Rui
    Lin, Enci
    Simon, Terrence
    Xie, Gongnan
    JOURNAL OF HEAT TRANSFER-TRANSACTIONS OF THE ASME, 2021, 143 (01):
  • [7] Influence of the hole length-to-diameter ratio on film cooling with cylindrical holes
    Lutum, E.
    Johnson, B.V.
    Journal of Turbomachinery, 1999, 121 (02): : 209 - 216
  • [8] Influence of the hole length-to-diameter ratio on film cooling with cylindrical holes
    Lutum, E
    Johnson, BV
    JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 1999, 121 (02): : 209 - 216
  • [9] Film cooling from a cylindrical hole with parallel auxiliary holes influences
    Dai, Sheng-ji
    Xiao, Yang
    He, Li-ming
    Jin, Tao
    Zhao, Zi-chen
    NUMERICAL HEAT TRANSFER PART A-APPLICATIONS, 2016, 69 (05) : 497 - 511
  • [10] Film cooling effectiveness for short film cooling holes fed by a narrow plenum
    Hale, CA
    Plesniak, MW
    Ramadhyani, S
    JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2000, 122 (03): : 553 - 557