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ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 2010, Vol. 31 ›› Issue (11): 2130-2138.

• Fluid Mechanics and Flight Mechanics • Previous Articles     Next Articles

Unsteady Numerical Simulation Investigation of Effect of Blade Profile Deviation on Turbine Performance

Zhang Weihao1,2, Zou Zhengping1,2, Li Wei3, Luo Jianqiao3, Pan Shangneng3
  

  1. 1. National Key Laboratory of Science & Technology on Aero-Engine Aero-Thermodynamics, Beijing University of Aeronautics and Astronautics, 2. Aeroengine Numerical Simulation Research Center, Beijing University of Aeronautics and Astronautics3. Chinese Aviation Powerplant Research Institute
  • Received:2009-12-31 Revised:2010-04-06 Online:2010-11-25 Published:2010-11-25
  • Contact: Zou Zhengping

Abstract: Turbine profile deviation can hardly be avoided in manufacturing practice, which may affect the behavior of the turbine. To investigate the effect of profile deviation on turbine performance and on details of the flow field, steady and unsteady numerical simulations of a turbine in combination with experiments on a complete engine are carried out and the numerical simulation results are also comprehensively compared. The findings indicate that profile deviation can weaken turbine performance considerably in the whole operating range. It also shows that the unsteady interaction between the blade rows and the structures of the flow field, such as the development of passage vortex and tip leakage flow, the intensity of the leading edge suction spike and the shape and intensity of shock waves, would all alter a great deal as the profile changes. In addition, the results demonstrate that unsteady numerical simulation can capture these influences more precisely.

Key words: profile deviation, turbine, aerodynamic performance, numerical simulation, unsteady

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