Flow Past Airfoil Moving Reciprocally in a Channel by Vortex Method

  • Ro Ki-Deok (School of Mechanical and Aerospace Engineering.Institute of Marine Industry, Gyeongsang National University)
  • 발행 : 2006.08.01

초록

The velocity and pressure fields of a ship's propulsion mechanism of the Weis-Fogh type, in which a airfoil moves reciprocally in a channel, are studied in this paper using the advanced vortex method. The airfoil and the channel are approximated by a finite number of source and vortex panels, and the free vortices are introduced from the body surfaces. The viscous diffusion of fluid is represented using the core-spreading model to the discrete vortices. The velocity is calculated on the basis of the generalized Biot-Savart law and the pressure field is calculated from integrating the equation given by the instantaneous velocity and vorticity fields. Two-dimensional unsteady viscose flows of this propulsion mechanism are numerically clarified, and the calculated results agree well with the experimental ones.

키워드

참고문헌

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