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An Experimental Study of Coanda Effect on the Flapped Control Surfaces

콴다효과를 응용한 플랩이 달린 고양력 날개장치에 대한 실험적 연구

  • 안해성 (서울대학교 조선해양공학과, 해양시스템공학연구소) ;
  • 김효철 (서울대학교 조선해양공학과, 해양시스템공학연구소)
  • Published : 2003.10.01

Abstract

To investigate the jet effect on circulation control, a segment of model was prepared and inserted horizontally across the test section of the cavitation tunnel. The hydrodynamic forces acting on the model were measured under the 2 dimensional flow behavior. Circulation flow control requires higher flow rate of water jet than boundary layer control does. Jet injection is effective in increasing lift coefficient and the increments reach to 160% in a certain combination of parameters such as an angle of attack, jet flow rate and flap angle. The blown water jet not only reduces form drag but also thrust effect, which is sometimes greater than the form drag in specific conditions.

Keywords

References

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Cited by

  1. A Study to Improve the Performance of a Fixd Type Fin Stabilizer with Coanda Effect vol.37, pp.3, 2013, https://doi.org/10.5394/KINPR.2013.37.3.257