Turbine Performance Degradation due to Blade Surface Roughness

블레이드 표면 거칠기에 따른 터빈 성능저하

  • 박일영 (서울대학교 기계항공공학부 대학원) ;
  • 윤용일 (서울대학교 기계항공공학부 대학원) ;
  • 송성진 (서울대학교 기계항공공학부)
  • Published : 2003.04.23

Abstract

This paper reports on the influence of blade surface roughness on turbine efficiency. The performance of a low speed one-stage axial turbine with roughened blade surfaces was evaluated. Sandpaper with equivalent sandgrain roughness ($k_s$) was used to roughen the blades. Efficiency (${\eta}/{\eta}_0$) decreases by 4.5 % with sandgrain size of 400 ${\mu}m$ on the stator suction surface.

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