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A Computational Fluid Dynamic Study for Temperature Uniformity at a Wind Tunnel Outlet with Effects of Heat Transfer along Tunnel Walls

机译:隧道壁传热效应的风洞出口温度均匀性的计算流体动力学研究

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A Computational Fluid Dynamics (CFD) Modelling was carried out to investigate temperature uniformity at a wind tunnel outlet region to benefit its design and construction. Low temperate (11 OK) nitrogen entered the wind tunnel at inlet, passed through two turning area with 18 turning vanes and went into expansion session, stable session and congestion session, finally towards outlet discharge nozzle session. The model considered static nitrogen isolation layer in physical model and three more isolation layer outside the tunnel as well as possible heat transfer from ambient environment. Two case scenario for supersonic and subsonic at outlet (Mach Number 0.9 and 1.3) were conducted with a uniform temperature imposed at inlet, as well a 3rd case scenario (Mach Number 0.9) with a non-uniform temperature distribution at inlet. Existence of porous zone (to model honeycomb session) and porous interfaces (to model damping interfaces) at the stable session were also included. Contours of temperature and velocity on representative cross sections were presented, and effects of Mach number, total pressure and initial temperature distribution at inlet on temperature uniformity at outlet were discussed. Based on the numerical results, improvement of tunnel geometry for better flow uniformity at outlet regions were also suggested.
机译:进行计算流体动力学(CFD)建模,以研究风洞出口区域的温度均匀性,使其设计和结构有益。低温(11 OK)氮进入入口的风洞,通过两个转动区域,带有18个转向叶片,进入扩展会话,稳定的会话和拥塞会话,最后朝向出口放电喷嘴会话。该模型认为物理模型中的静态氮隔离层和隧道之外的三个更多隔离层以及来自环境环境的可能热传递。在出口(Mach编号0.9和1.3)中的两种情况下为超音速和子系统(Mach编号0.9和1.3),其在入口施加均匀的温度,以及在入口处的3个案例场景(Mach编号0.9),入口处是非均匀的温度分布。还包括多孔区(以模型蜂窝会话)和多孔接口(在稳定的会议上进行多孔界面(在模型阻尼界面)。提出了横截面上的温度和速度的轮廓,并讨论了入口在出口温度均匀性的入口处的马赫数,总压力和初始温度分布的影响。基于数值效果,还提出了在出口区域的更好流动均匀性的隧道几何形状的改进。

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