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Bluff Body Drag Reduction Using Passive Flow Control of Jet Boat Tail

机译:使用喷射船尾部的无源流量控制减少诈唬身体阻力

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This paper conducts experimental study and numerical large eddy simulation for the drag reduction effect of jet boat-tail passive flow control on bluff body models. The jet boat-tail for bluff bodies operates by surrounding a converging duct around the end of a bluff body where the base surface is located. The duct captures free stream and forms a high speed jet angled toward the center of the bluff body base surface circumferentially to have the effect of a boat tail. A rectangular prism bluff body representative of various motor vehicle shapes such as trucks, vans, SUVs is used in this study. The numerical Large Eddy Simulation shows that the jet boat-tail sucks in the forebody boundary layer due to the low base pressure and significantly thins the boundary layer. The jet interacts with the shear layer and creates large vortex structures that entrain the freestream to base flow and energize it. The base pressure with the jet boat-tail is increased and the wake velocity deficit is reduced, resulting in a significant drag reduction. The Large Eddy Simulation indicates a significant drag reduction of 15%. The baseline and jet boat-tail configuration were also tested in a wind tunnel using 3D Stereo Particle Image Velocimetry at the speed of 10m/s and 30m/s. The wind tunnel testing shows a significant wake velocity deficit reduction by using jet boat-tail passive flow control, which is consistent with the drag reduction results of the Large Eddy Simulation.
机译:本文对吹船尾被动流量控制的减阻效果进行了实验研究和数值大涡模拟。用于诈唬物体的喷射船尾通过围绕底部表面的凹痕体的端部周围的会聚管道操作。管道捕获自由流,并形成朝向凹槽体基表面的中心成角度的高速射流,以具有船尾的效果。在本研究中使用了代表各种机动车辆形状的矩形棱镜Bluff身体,例如卡车,VANS,SUV。数值大涡模拟显示喷射船尾由于低碱压力而在前端边界层中吸入并显着粘附边界层。喷射与剪切层相互作用,并产生大的涡旋结构,使自由流夹住自由流动并激励它。随着喷射船尾的基础压力增加,减少了唤醒速度缺陷,导致减压减少。大型涡流模拟表明减少15%的显着减阻。基线和喷射船尾配置也使用3D立体粒子图像速度在100m / s和30m / s的速度下在风隧道中进行测试。风洞测试通过使用喷射船尾被动流量控制显示了显着的唤醒速度赤字缺陷,这与大涡模拟的减阻结果一致。

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