不同斜角下艾哈迈德体空气动力学数值模拟

G. Kumar, Chanfiou Ahmed Mboreha, Yahya Al-fakih
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摘要

在本研究中,利用ANSYS FLUENT CFD程序研究了倾角为0°、30°和60°的艾哈迈德体的气动行为。所有情况下的流动条件是相同的,而艾哈迈德的身体后倾斜角度是不同的。气动参数;着重分析了升力系数和阻力系数对气动效率的影响。采用随时间变化的瞬态仿真方法研究了流体的流动特性。由于雷诺数为5x105in紊流状态,因此为了准确捕捉紊流效应,采用k-epsilon二方程模型
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Numerical simulations on the aerodynamics of the Ahmed body at different slant angles
In this research, the aerodynamic behavior of Ahmed’s body with slant angles of 0°, 30° and 60° is studied using ANSYS FLUENT CFD code. The flow conditions for all cases were same while the rear slant angle is varied for Ahmed’s body. The aerodynamic parameters; lift coefficient and drag coefficient were focused mainly to analyze the flow behavior, it tells the aerodynamics efficiency. The time dependent transient simulation is run to study the behavior of fluid flow. As the Reynold’s number lied 5x105in turbulent regime so to accurately capture the turbulent effects, k-epsilon two equation model with
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