Numerical Analysis of Tip Leakage Flows in Axial Flow Turbine Rotors

축류터빈 동익 내부의 누설유동에 관한 수치해석

  • 정희택 (경상대학교 기계항공공학부 항공기부품기술연구센터)
  • Published : 2005.02.28

Abstract

Numerical analysis of three-dimensional viscous flow-fields in the turbine rotor passages was carried out to investigate flow physics including the interaction between secondary vortices, tip leakage vortex, and the rotor wake. The blade tip geometry was accurately modeled adopting the embedded H grid system. An explicit four-stage Runge-Kutta scheme was used for the time integration of both the mean flow and turbulence equations. The computational results for the entire turbine rotor flows, particularly the tip clearance flow and the secondary flows, were interpreted and compared with the experimental data from the Penn State turbine stage. The predictions for major features of the flow field have been found to be in good agreement with the experimental data.

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