Blade Loading에 의한 팁와류의 특성

Characteristics of Tip Vortex by Blade Loading

  • 윤용상 (서울대 기계항공공학부 대학원) ;
  • 송성진 (서울대 기계항공공학부)
  • 발행 : 2002.12.01

초록

The characteristics of tip vortex within a blade tip region were examined experimentally in various flow coefficients by the way of changing tip clearance and blade stagger angle in an axial Low Speed Research Compressor(LSRC). The objective was to identify the unsteady pressure distribution in the blade passage by ensemble average technique acquired from high-frequency response pressure transducers and the tip vortex by root mean square value(RMS value). Data were reduced statistically using phase-lock technique for detailed pressure distributions.

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