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Journal of Shanghai University（Natural Science Edition）

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Simulation of Active Flow Control on Viscous Flow around Airfoil under Low Reynolds Number

ZHOU Xin,YANG Ai-ming,WENG Pei-fen   

  1. Shanghai Institute of Applied Mathematics and Mechanics, Shanghai University, Shanghai 200072, China
  • Received:2006-05-23 Revised:1900-01-01 Online:2007-04-30 Published:2007-04-30
  • Contact: WENG Pei-fen

Cited

1

Abstract: The control effect of zero-net-mass-flux jet on the viscous flow around airfoil has been simulated using N-S equation. In the solver, the cell-centered finite volume method in space and dual-time stepping method in time is used. The results show that active flow control can enhance aerodynamic performance by reducing the adverse effects of separated flow.

Key words: active flow control, N-S equation, zero-net -mass-flux jet, MAV

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