이차원 운송체 모형에서 후류 교란자를 이용한 항력 감소

Reduction of Drag on a Two-Dimensional Model Vehicle Using Wake Disrupter

  • 이동건 (서울대학교 대학원) ;
  • 최진 (서울대학교 대학원) ;
  • 전우평 (서울대학교 정밀기계설계공동연구소 난류제어연구단) ;
  • 김정래 (서울대학교 대학원) ;
  • 한성현 (서울대학교 정밀기계설계공동연구소 난류제어연구단) ;
  • 최해천 (서울대학교 기계항공공학부)
  • 발행 : 2003.11.05

초록

A wind-tunnel experiment is carried out to examine the applicability of a new passive device, wake disrupter, to flow over a model vehicle for drag reduction. The wake disrupter is a small-size rectangular body attached to a part of the trailing edge of the model vehicle, designed to perturb an essentially two-dimensional nature of wake. A pair of wake disrupter is mounted on the mid-span at the upper and lower trailing edges. From a parametric study about the size of wake disrupter, it is found that the optimum disrupter increases the base pressure by about 20%. Large eddy simulation is also conducted to confirm the experimental result, and shows that the wake is indeed disrupted by the present device.

키워드