• Title/Summary/Keyword: Trunk rear edge

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Effects on Aerodynamic Drag Reduction of a Passenger Car by Rear Body Shape Modifications (승용차의 후면 형상 변형이 공기저항 감소에 미치는 영향)

  • Song, Ki-Sun;Kang, Seung-On;Jun, Sang-Ook;Park, Hoon-Il;Kee, Jung-Do;Kim, Kyu-Hong;Lee, Dong-Ho
    • Transactions of the Korean Society of Automotive Engineers
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    • v.19 no.4
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    • pp.137-145
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    • 2011
  • This paper suggests possible rear body shape modifications of a passenger car for the improvement of aerodynamic performance, based on the CFD analysis results. YF SONATA, a passenger car of Hyundai Motors Company, plays a major role as the baseline car in this research. Representatively, three parts(trunk rear edge, side rear edge and rear undercover) are modified in a small range in order for the total outer shapes not to be changed enough so that the modified car is not considered different, compared with the baseline. Specifically, using computational fluid dynamics, aerodynamic drag reduction is accomplished maximally about 11% in this research. Finally, it is proved that although the range of changes of the rear body shapes of a passenger car is very strictly confined, by changing a small range of rear body shapes alone the enhancement of aerodynamic performance of a passenger car can be significantly accomplished.

On Flow Separation Delineated with Surface Flow Visualization (표면유동가시화를 통한 박리유동의 고찰)

  • Chun Chung-Hwan
    • 한국전산유체공학회:학술대회논문집
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    • 1998.11a
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    • pp.1-6
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    • 1998
  • From surface flow visualization on a MIRA notchback reference model using oil flow technique, the topology of the singular points of the skin friction lines are delineated. Separation and reattachment lines at the front screen, at the A-pillar, at the C-pillar and on the rear side of the car including the trunk have been identified. It is worth to mention that two vortices emerging from the top of the trunk coil in the opposite direction as that vortices starting from the C-pillar edge. The positions of the singular points and the separation and reattachment lines and the foci of the vortices provide a sensitive database for validation of CFD-codes

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