Effect of Vortex Generators on Film Cooling Effectiveness

被引:0
|
作者
Sarkar, S. [1 ]
Ranakoti, Ganesh [1 ,2 ]
机构
[1] Indian Inst Technol, Dept Mech Engn, Kanpur 208016, Uttar Pradesh, India
[2] Galgotias Univ, Greater Noida, India
关键词
Film Cooling; Vortex Generator; CRVP; Jets-in-crossflow; HEAT-TRANSFER; 2; ROWS; HOLES; DOWNSTREAM; JETS; TEMPERATURE; TURBULENCE;
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
Film cooling is often adopted, where coolant jets are ejected to form a protective layer on the surface against the hot combustor gases. The bending of jets in crossflow results in Counter Rotating Vortex Pair (CRVP), which is a cause for high jet lift-off and poor film cooling effectiveness in the near field. There are efforts to mitigate this detrimental effect of CRVP and thus to improve the film cooling performance. In the present study, the effects of both downwash and upwash type of vortex generator on film cooling are numerically analysed A series of discrete holes on a flat plate with 3.5 degrees streamwise orientation and connected to a common delivery plenum is used here, where the vortex generators are placed upstream of the holes. The blowing ratio and the density ratio are considered as 0.5 and 1.2 respectively with a Reynolds number based on free-stream velocity and diameter of hole being 15885. The computations are performed by ANSYS Fluent 13.0 using k-epsilon realizable turbulence model. The results show that vortices generated by downwash vortex generator (DWVG) counteracts the effect of CRVP preventing the jet lift-off which results in increased effectiveness in streamwise as well as in spanwise directions. However, upwash vortex generator (UWVG) augments the effect of CRVP, resulting in poor performance of film cooling.
引用
收藏
页数:11
相关论文
共 50 条
  • [21] Effect of stagnation regions on film cooling effectiveness
    Rodriguez, S.
    Kersten, S.
    Zuniga, H. A.
    Ling, J. C.
    Kapat, J. S.
    PROCEEDINGS OF THE ASME TURBO EXPO 2007, VOL 4, PTS A AND B, 2007, : 781 - 788
  • [22] EFFECT OF PULSED FILM COOLING ON LEADING EDGE FILM EFFECTIVENESS
    El-Gabry, Lamyaa A.
    Rivir, Richard B.
    PROCEEDINGS OF THE ASME INTERNATIONAL MECHANICAL ENGINEERING CONGRESS AND EXPOSITION - 2010, VOL 7, PTS A AND B, 2012, : 1403 - 1409
  • [23] Effect of Pulsed Film Cooling on Leading Edge Film Effectiveness
    El-Gabry, Lamyaa A.
    Rivir, Richard B.
    JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2012, 134 (04):
  • [24] Heat transfer in a cooling channel with vortex generators
    Chyu, MK
    Ding, H
    JOURNAL OF HEAT TRANSFER-TRANSACTIONS OF THE ASME, 1997, 119 (02): : 206 - 206
  • [25] IMPLEMENTATION OF VORTEX GENERATOR AND RAMP TO IMPROVE FILM COOLING EFFECTIVENESS ON BLADE ENDWALL
    Hussain, Sadam
    Yan, Xin
    PROCEEDINGS OF ASME TURBO EXPO 2021: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, VOL 5A, 2021,
  • [26] IMPROVED FILM COOLING EFFECTIVENESS BY PLACING A VORTEX GENERATOR DOWNSTREAM OF EACH HOLE
    Rigby, David L.
    Heidmann, James D.
    PROCEEDINGS OF THE ASME TURBO EXPO 2008, VOL 4, PTS A AND B, 2008, : 1161 - 1174
  • [27] NUMERICAL INVESTIGATION OF FILM COOLING EFFECTIVENESS USING THE ANTI-VORTEX CONCEPTION
    Nemdili, Fadela
    Nemdili, Saliha
    Azzi, Abbes
    IRF2018: PROCEEDINGS OF THE 6TH INTERNATIONAL CONFERENCE ON INTEGRITY-RELIABILITY-FAILURE, 2018, : 1061 - 1062
  • [28] FILM COOLING EFFECTIVENESS
    GARTSHORE, I
    SALCUDEAN, M
    MATYS, P
    TRANSACTIONS OF THE CANADIAN SOCIETY FOR MECHANICAL ENGINEERING, 1991, 15 (01) : 43 - 56
  • [29] Effect of continuous or discrete shock wave generators on supersonic film cooling
    Peng, Wei
    Sun, Xiaokai
    Jiang, Peixue
    Wang, Jie
    INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 2017, 108 : 770 - 783
  • [30] EFFECT OF UNCERTAINTY IN BLOWING RATIO ON FILM COOLING EFFECTIVENESS
    Babaee, Hessam
    Wan, Xiaoliang
    Acharya, Sumanta
    PROCEEDINGS OF THE ASME SUMMER HEAT TRANSFER CONFERENCE - 2013, VOL 3, 2014,