연구동향 분석
박사

막냉각이 다양한 형상의 가스터빈 블레이드 팁 주변의 열유동에 미치는 영향에 대한 수치해석적 연구 = Numerical study of film cooling effects on flow and heat transfer near gas turbine blade tips with various shape

김대현 2016년

논문상세정보
인용/피인용
' 막냉각이 다양한 형상의 가스터빈 블레이드 팁 주변의 열유동에 미치는 영향에 대한 수치해석적 연구 = Numerical study of film cooling effects on flow and heat transfer near gas turbine blade tips with various shape' 의 주제별 논문영향력
논문영향력 선정 방법
논문영향력 요약
주제
  • Blade tip
  • Cutback squealer tip
  • Effectiveness
  • Film cooling
  • Multi cavity ? triangle groove tip
  • Multi cavity squealer tip
  • Plane tip
  • Squealer tip
  • Tip cavity
  • Total pressure coefficient
  • Triangle groove tip
  • gas turbine
  • heat transfer coefficient
동일주제 총논문수 논문피인용 총횟수 주제별 논문영향력의 평균
356 0

0.0%

' 막냉각이 다양한 형상의 가스터빈 블레이드 팁 주변의 열유동에 미치는 영향에 대한 수치해석적 연구 = Numerical study of film cooling effects on flow and heat transfer near gas turbine blade tips with various shape' 의 참고문헌

  • Z. Wang et al., 2014, “Impact of Cooling Injection on Transonic Overtip Leakage Flow and Squealer Aerothermal Design Optimization”, GT2014-26825
  • Yaras, M., Yingkang, Z., Sjolander, S.A., 1989, "Flow Field in the Tip Gap of a Planar Cascade of Turbine Blades," ASME Journal of Turbomachinery, Vol. 111, pp. 276-283
  • Yang, H., Chen, H. C., and Han J. C., 2002, “Numerical Prediction of Film Cooling and Heat Transfer with Different Film Hole Arrangements on the Plane and Squealer Tip of a Gas Turbine Blade,” GT -2004- 53249.
  • Yamamoto, A., 1989, "Endwall Flow/Loss Mechanisms in a Linear Turbine Cascade With Blade Tip Clearance," ASME Journal of Turbomachinery, Vol. 111, pp. 264-275
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  • Projektinfo, 09/2006
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  • Azad, G.S., Han, J.C., Boyle, R.J., "Heat Transfer and Flow on the Squealer Tip of a Gas Turbine Blade," Proceeding of: International Gas Turbine and Aeroengine Congress and Exposition, Munich, Germany, May 2000, 2000-GT-195
  • Annual energy Outlook 2012
  • Ahn, J. Y., Mhetras, S., and Han J. C., 2002, “Film-cooling effectiveness on a Gas Turbine Blade Tip using Pressure Sensitive Paint,” GT -2004-53249.