TY - JOUR
T1 - 沿流向微结构沟槽流场直接数值模拟
AU - Li, Chaoqun
AU - Li, Yi
AU - Zhang, Chenxi
AU - Tang, Shuo
N1 - Publisher Copyright:
© 2020, Beihang University Aerospace Knowledge Press. All right reserved.
PY - 2020/11/25
Y1 - 2020/11/25
N2 - To simulate the flow over the streamwise micro riblets of symmetric V shape, this paper applies a model of channel flow where the lower wall is mounted with riblets and the upper one is flat. The finite difference method is employed as the numerical method. To accurately obtain the flow of riblets, the 7th WENO (Weighted Essentially Non-Oscillatory) scheme, the fractional-step method combined with the Low-Dissipation and Dispersion Runge-Kutta scheme (LDDRK method) and the 6th central scheme are applied to the discretization of the space, the time advancing and viscous terms. In this paper, the Reynolds number is 5 000 (based on the half width of the channel), the range of the size of the riblets is from 13 to 44 and the inclination of the slope of riblets is 60°. Simulation results illustrate that the maximum of drag reduction is 9% and indicate that in the drag-reducing cases, the riblets can prevent the large-scale streamwise vortices from interacting with the surface directly, weakening the turbulent oscillation and decreasing the number of the streamwise vortices near riblet wall.
AB - To simulate the flow over the streamwise micro riblets of symmetric V shape, this paper applies a model of channel flow where the lower wall is mounted with riblets and the upper one is flat. The finite difference method is employed as the numerical method. To accurately obtain the flow of riblets, the 7th WENO (Weighted Essentially Non-Oscillatory) scheme, the fractional-step method combined with the Low-Dissipation and Dispersion Runge-Kutta scheme (LDDRK method) and the 6th central scheme are applied to the discretization of the space, the time advancing and viscous terms. In this paper, the Reynolds number is 5 000 (based on the half width of the channel), the range of the size of the riblets is from 13 to 44 and the inclination of the slope of riblets is 60°. Simulation results illustrate that the maximum of drag reduction is 9% and indicate that in the drag-reducing cases, the riblets can prevent the large-scale streamwise vortices from interacting with the surface directly, weakening the turbulent oscillation and decreasing the number of the streamwise vortices near riblet wall.
KW - Direct numerical simulation
KW - Finite difference method
KW - High-order WENO scheme
KW - Incompressible flow
KW - Micro riblets
KW - Turbulent drag reduction
UR - http://www.scopus.com/inward/record.url?scp=85098165566&partnerID=8YFLogxK
U2 - 10.7527/S1000-6893.2019.23628
DO - 10.7527/S1000-6893.2019.23628
M3 - 文章
AN - SCOPUS:85098165566
SN - 1000-6893
VL - 41
JO - Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica
JF - Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica
IS - 11
M1 - 123628
ER -