• Title/Summary/Keyword: 레이놀즈평균 나비어-스톡스 해석

Search Result 22, Processing Time 0.015 seconds

A Numerical Study on Hydrodynamic Interactions between Dynamic Positioning Thrusters (동적위치제어용 스러스터 사이의 유체역학적 상호작용에 대한 수치해석 연구)

  • Jin, Doo Hwa;Lee, Sang Wook
    • Transactions of the Korean Society of Mechanical Engineers B
    • /
    • v.41 no.6
    • /
    • pp.373-380
    • /
    • 2017
  • In this study, we conducted computational fluid dynamics (CFD) simulations for the unsteady hydrodynamic interaction of multiple thrusters by solving Reynolds averaged Navier-Stokes equations. A commercial CFD software, STAR-CCM+ was used for all simulations by employing a ducted thruster model with combination of a propeller and No. 19a duct. A sliding mesh technique was used to treat dynamic motion of propeller rotation and non-conformal hexahedral grid system was considered. Four different combinations in tilting and azimuth angles of the thrusters were considered to investigate the effects on the propulsion performance. We could find that thruster-hull and thruster-thruster interactions has significant effect on propulsion performance and further study will be required for the optimal configurations with the best tilting and relative azimuth angle between thrusters.

Effects of Geometric Parameters of a Bobsleigh on Aerodynamic Performance (봅슬레이의 형상변화가 공력성능에 미치는 영향)

  • Shim, Hyeon-Seok;Jung, Hyo-Yeon;Kim, Jun-Hee;Kim, Kwang-Yong
    • Transactions of the KSME C: Technology and Education
    • /
    • v.3 no.3
    • /
    • pp.233-240
    • /
    • 2015
  • Analysis of the aerodynamic performance of a bobsleigh has been performed for various types of bobsleigh body shape. To analyze the aerodynamic performance of the bobsleigh, three-dimensional Reynolds-averaged Navier-Stoke equations were used with the standard k-${\varepsilon}$ model as a turbulence closure. Grid structure was composed of unstructured tetrahedral grids. The radii of curvature of cowling, and height and length of front bumper at the tip on the drag coefficient were selected as geometric parameters. And, the effects of these parameters on the aerodynamic performance, i.e., the drag coefficient, were evaluated. The results shows that the aerodynamic performance is significantly affected by the height of front bumper and radius of curvature.