반와류 홀의 형상 변화가 막냉각 효율에 미치는 영향

논문상세정보
' 반와류 홀의 형상 변화가 막냉각 효율에 미치는 영향' 의 주제별 논문영향력
논문영향력 선정 방법
논문영향력 요약
주제
  • 유체공학, 기력학, 진공학
  • anti-vortexholes(반와류홀)
  • blowingratio(분사율)
  • film-coolingeffectiveness(막냉각효율)
  • reynolds-averaged navier-stokes equations(레이놀즈 평균 나비어-스톡스 방정식)
동일주제 총논문수 논문피인용 총횟수 주제별 논문영향력의 평균
275 0

0.0%

' 반와류 홀의 형상 변화가 막냉각 효율에 미치는 영향' 의 참고문헌

  • Surrogate based optimization of a laidback fan-shaped hole for filmcooling
    Lee, K. D International Journal of Heat and Fluid Flow 32 (1) : 226 ~ 238 [2011]
  • Optimization of Ejection Angles of Double-jet Filmcooling Holes Using RBNN Model
    Lee, K. D International Journal of Thermal Sciences 73 : 69 ~ 78 [2013]
  • Japanese Patent Application No. 332530
  • Influence of Compound Angle on Adiabatic Film Cooling Effectiveness and Heat Transfer Coefficient for a Row of Shaped Film Cooling Holes
    Brauckmann, D ASME Turbo Expo [2005]
  • Influence of Blowing Ratio on The Double-Jet Ejection of Cooling Air
    Kusterer, K. ASME Turbo Expo 2007 [2007]
  • Film cooling effectiveness from trenched shaped and compound holes
    Baheri, S. Heat Mass Transfer 44 (8) : 989 ~ 998 [2008]
  • Film Cooling From A Row of Holes Supplemented With Anti Vortex Holes
    Dhungel, A. ASME Turbo Expo [2007]
  • Film Cooling Effectiveness Comparison Between Shaped and Double Jet Film Cooling Holes In A Row Arrangement
    Kusterer, K. ASME Turbo Expo 2010 [2010]
  • Effects of Axial Row-spacing For Double-jet Filmcooling On The Cooling Effectiveness
    Wang, Z. ASME Turbo Expo 2011 [2011]
  • Effect of Hole Geometry on the Thermal Performance of Fan-Shaped Film Cooling Holes
    Gritsch, M Journal of Turbomachinery 127 : 718 ~ 725 [2005]
  • Effect of Compound Angle Injection of Flat Surface Film Cooling with Large Streamwise Injection Angle
    Nasir, H. Experimental Thermal and Fluid Science 25 (1-2) : 23 ~ 29 [2001]
  • Double-Jet Film-Cooling for Highly Efficient Film-Cooling with Low Blowing Ratios
    Kusterer, K. ASME Turbo Expo 2008 [2008]
  • Double-Jet Ejection of Cooling Air for Improved Film-Cooling
    Kusterer, K. ASME Turbo Expo 2006 [2006]
  • CFX-11.0 Solver Theory
    Ansys inc [2008]
  • A Parametric Study on the Influence of the Lateral Ejection Angle of Double-Jet Holes on the Film Cooling Effectiveness for High Blowing Ratios
    Kusterer, K. ASME Turbo Expo 2009 [2009]
  • A Numerical Study of Antivortex Film Cooling Designs At High Blowing Ratio
    Heidmann, J. D ASME Turbo Expo [2008]
  • A Detailed Analysis of Film-Cooling Physics: Part I—Streamwise Injection With Cylindrical Holes
    Walters, D. K. Journal of Turbomachinery 112 (1) : 102 ~ 112 [2001]