• Title/Summary/Keyword: Spoiler Aerodynamics

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The study about aerodynamics according to the spoiler of the car (자동차 Spoiler의 유무에 따른 공력 특성 비교 분석)

  • Kim, Wang-Hyeon;Kim, In-Hyeon;Ryu, Gi-Myeong;Kim, Byeong-Su
    • Proceeding of EDISON Challenge
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    • 2013.04a
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    • pp.421-424
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    • 2013
  • 본 연구에서는 교육 및 연구를 위한 CFD 해석 프로그램인 EDISON_CFD를 이용하여 자동차 Spoiler의 장착 유무에 따른 공력 특성을 분석해보았다. Spoiler가 장착되지 않은 자동차의 공력 특성을 확인하고, Spoiler의 길이에 따라 공력 특성이 어떻게 차이가 나는지 비교하였다. HONDA S2000 차량의 압력 계수를 구하였고, 자동차 길이의 3.5%, 7%, 14%에 해당하는 길이의 Spoiler를 장착하여 어떠한 변화가 발생하는지 확인하였다. 그 결과 Spoiler의 길이가 길수록 짧을 때보다 상대적으로 좋은 효율을 보이는 것을 확인할 수 있었다.

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Parametric Study of Transient Spoiler Aerodynamics with Two-Equation Turbulence Models (2-방정식 난류모델을 이용한 스포일러 천이적 공력특성의 파라메트릭 연구)

  • Choi S. W.;Chang K. S.;Ok H. N.
    • 한국전산유체공학회:학술대회논문집
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    • 2000.10a
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    • pp.15-24
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    • 2000
  • The transient response of an airfoil to a rapidly deploying spoiler is numerically investigated using the turbulent compressible Navier-Stokes equations in two dimensions. Algebraic Baldwin-Lomax model, Wilcox $\kappa-\omega$ model, and SST $\kappa-\omega$ turbulence model are used to calculate the unsteady separated flow due to the rapid spoiler deployment. The spoiler motion relative to a stationary airfoil is treated by an overset grid hounded by a Dynamic Domain-Dividing Line which has been devised by the authors. The adverse effects of the spoiler influenced by the spoiler location and the hinge gap are expounded. The numerical results are in reasonably good agreement with the existing experimental data.

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Influence of a rear spoiler on a squareback car wake (리어 스포일러 장착에 의한 자동차 후류의 변화 연구)

  • Baek, Seung-Jin;Oh, Min-Soo;Lee, Jung-Ho;Kim, Moo-Sang
    • Proceedings of the KSME Conference
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    • 2004.04a
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    • pp.1825-1829
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    • 2004
  • A numerical simulation was performed of flow behind a squareback car with a rear spoiler. Influence of the rear spoiler on drag force has been studied. A lattice Boltzmann method was utilized to portray the unsteady aerodynamics of wake flows. The pressure distributions were employed to examine the vortex formation mode against the rear spoiler. It was found that the separation flow at roof end and c-pillar makes three dimensional vortex structures and the rear spoiler increases pressure on the rear glass surface.

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A Numerical Investigation on the Wake Flow Characteristics and Rear-Spoiler Effect of a Large-Sized Bus Body (대형버스 바디모델의 후류특성 및 후미 스포일러 효과에 관한 해석적 고찰)

  • 김민호;국종영;천인범
    • Transactions of the Korean Society of Automotive Engineers
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    • v.11 no.2
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    • pp.126-133
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    • 2003
  • The aerodynamic characteristics of automobiles have received substantial interest recently. Detailed knowledge of the vehicle aerodynamics is essential to improve fuel efficiency and enhance stability at high-speed cruising. In this study, a numerical simulation has been carried out for three-dimensional turbulent flows around a commercial bus body. Also, the effect of rear-spoiler attached at rear end of bus body was investigated. The Wavier-Stokes equation is solved with SIMPLE method in general curvilinear coordinates system. RNG $k-\varepsilon$ turbulence model with the MARS scheme was used for the evaluating aerodynamic forces, velocity and pressure distribution. The results showed details of the three-dimensional wake flow in the immediate rear of bus body and the effect of rear-spoiler on the wake structure. A maximum of 14% reduction in drag coefficient was achieved for a model with a rear-spoiler.

Computational Investigations of Adverse Effects of Deploying Spoilers on Airfoil Aerodynamic Characteristics (스포일러 동적 작동에 따른 에어포일 공력특성 역전현상 연구)

  • Chung, Hyoung-Seog
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.48 no.5
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    • pp.335-342
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    • 2020
  • Tailless aircraft designed for stealth efficiency uses spoilers instead of rudders for the directional control. When the spoiler is rapidly deployed, highly nonlinear and unsteady aerodynamic characteristics can be generated, resulting in adverse effects on aircraft flight performance. This paper investigates the aerodynamic characteristics of an airfoil with moving spoiler using dynamic mesh CFD technique. The effects of spoiler operation speed, mounting location, and deployment scheduling are analyzed to reduce the adverse effects of the spoiler's dynamic operation. The results shows that the adverse effects of dynamic spoiler can be reduced by appropriate selection of the spoiler mounting location and deployment scheduling.