Combined effects of blowing ratio and mist diameter with mainstream turbulence intensity in mist-assisted film cooling

被引:0
|
作者
Jeong, Yoonhyeong [1 ]
Baek, Seung Il [2 ]
Vo, Duy-Tan [3 ]
Kim, Seunggi [3 ]
Kim, Dokyun [4 ]
Lee, Hyoungsoon [3 ]
Ryu, Jaiyoung [1 ]
机构
[1] Korea Univ, Sch Mech Engn, Seoul, South Korea
[2] Agcy Def Dev, Ground Technol Inst, Daejeon, South Korea
[3] Chung Ang Univ, Dept Mech Engn, Seoul, South Korea
[4] Hongik Univ, Dept Mech & Syst Design Engn, Seoul, South Korea
关键词
Gas turbine; film cooling; film cooling effectiveness; mist-assisted film cooling; Mainstream turbulence; FREE-STREAM TURBULENCE; SIMULATION; HOLES;
D O I
10.1080/19942060.2023.2253296
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Advanced cooling techniques are essential in modern gas turbines to improve the efficiency of the Brayton cycle by raising the turbine inlet temperature. Mist-assisted film cooling offers an innovative solution for cooling high-temperature gas turbine blades. When mist particles with various momenta are injected through the cooling holes, the interplay between mainstream turbulence intensity (Tu) and mist momentum plays a crucial role in mist-assisted film cooling under high Tu conditions. Hence, this numerical study investigates the relationship between mainstream Tu and mist characteristics for the first time, considering the blowing ratio and mist diameter as controlling parameters. Film effectiveness and particle distribution statistics are analysed to understand their correlation. The results demonstrate that mist-assisted film effectiveness follows the trend of air-only film cooling with varying blowing ratios and Tu; however, the magnitude is amplified. The influence of the mist diameter on film effectiveness is determined by the surface-area-to-volume ratio and Stokes number. These factors impact the sensitivity of particles to Tu and subsequently affect film effectiveness. This study provides a novel quantitative analysis of the combined effect of mainstream Tu and mist on film cooling effectiveness, revealing the correlation between mist and mainstream parameters.HighlightsCombined effect of mainstream turbulence intensity (Tu) and mist characteristics is investigated. High mainstream Tu significantly increases the cooling enhancement induced by mist. Mist-assisted film cooling exhibits similar trends to varying mainstream Tu and blowing ratio. Mist diameter significantly influences the response to Tu, governed by surface-area-to-volume ratio and Stokes number. Small particles demonstrate the highest cooling effectiveness and variation by Tu.
引用
收藏
页数:21
相关论文
共 50 条
  • [31] Effect of coolant-mainstream blowing ratio on leading edge film cooling flow and heat transfer - LES investigation
    Rozati, Ali
    Tafti, Danesh K.
    [J]. INTERNATIONAL JOURNAL OF HEAT AND FLUID FLOW, 2008, 29 (04) : 857 - 873
  • [32] EFFECTS OF OSCILLATIONS IN THE MAIN FLOW ON FILM COOLING AT VARIOUS FREQUENCIES AT A LOW BLOWING RATIO
    Baek, Seung Il
    Yavuzkurt, Savas
    [J]. PROCEEDINGS OF THE ASME TURBO EXPO: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, 2018, VOL 5A, 2018,
  • [33] Effects of soot deposition and slot erosion on the mist film-cooling of a flat plate in the presence of upstream ramp
    Handique, Jishnu
    Singh, Kuldeep
    Singh, Dushyant
    [J]. THERMAL SCIENCE AND ENGINEERING PROGRESS, 2021, 22
  • [34] The effects of high mainstream turbulence and turbine vane film cooling on the dispersion of a simulated hot streak
    Jenkins, S
    Varadarajan, K
    Bogard, DG
    [J]. JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2004, 126 (01): : 203 - 211
  • [35] Effects of the mainstream turbulence intensity and slot injection angle on the endwall cooling and phantom cooling of the vane suction side surface
    Du, Kun
    Song, Liming
    Li, Jun
    Sunden, Bengt
    [J]. INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 2017, 112 : 427 - 440
  • [36] Measurements in film cooling flows: Hole L/D and turbulence intensity effects
    Burd, SW
    Kaszeta, RW
    Simon, TW
    [J]. JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 1998, 120 (04): : 791 - 798
  • [37] EFFECTS OF VELOCITY RATIO ON TRENDS IN FILM-COOLING ADIABATIC EFFECTIVENESS AND TURBULENCE
    Stratton, Zachary T.
    Shih, Tom I-R
    [J]. PROCEEDINGS OF THE ASME TURBO EXPO: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, 2019, VOL 5A, 2019,
  • [38] Effect of leading edge diameter ratio and mainstream Reynolds number on film cooling performance of rotating blade leading edge
    Xie, Gang
    Tao, Zhi
    Zhou, Zhi-yu
    You, Ru-quan
    Li, Hai-wang
    [J]. APPLIED THERMAL ENGINEERING, 2021, 186
  • [39] Effects of Blowing Ratio and Land Extension on Blade Trailing Edge Cutback Film Cooling Effectiveness
    He, Kun
    Wang, Xi
    Yan, Xin
    [J]. Hsi-An Chiao Tung Ta Hsueh/Journal of Xi'an Jiaotong University, 2024, 58 (05): : 99 - 110
  • [40] A PRELIMINARY NUMERICAL STUDY ON THE EFFECT OF HIGH FREESTREAM TURBULENCE ON ANTI-VORTEX FILM COOLING DESIGN AT HIGH BLOWING RATIO
    Hunley, Benson K.
    Nix, Andrew C.
    Heidmann, James D.
    [J]. PROCEEDINGS OF THE ASME TURBO EXPO 2010, VOL 4, PTS A AND B, 2010, : 1313 - 1322