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首页> 外文期刊>Bulletin of the American Physical Society >APS -APS March Meeting 2017 - Event - The generalized analytical model and DSMC simulations of high-speed rotating flow in polar $(r -- heta ) $coordinate
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APS -APS March Meeting 2017 - Event - The generalized analytical model and DSMC simulations of high-speed rotating flow in polar $(r -- heta ) $coordinate

机译:APS -APS 2017年3月会议-事件-极坐标$(r-heta)$坐标中的高速旋转流的广义分析模型和DSMC模拟

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The generalized analytical model for the radial boundary layer in a high-speed rotating cylinder is formulated for studying the gas flow field due to insertion of mass, momentum and energy into the rotating cylinder in the polar~ $(r - heta )$~plane. The analytical solution includes the sixth order differential equation for the radial boundary layer at the cylindrical curved surface in terms of master potential~($chi )$, which is derived from the equations of motion in a polar~$(r - heta )$~plane. The linearization approximation ((Pradhan {&} Kumaranextit{, J. Fluid Mech-}); (Kumaran {&} Pradhan, extit{J. Fluid Mech-})) is used, where the equations of motion are truncated at linear order in the velocity and pressure disturbances to the base flow, which is a solid-body rotation. Additional assumptions in the analytical model include constant temperature in the base state (isothermal condition), and high Reynolds number, but there is no limitation on the stratification parameter. The analytical solutions are compared with direct simulation Monte Carlo (DSMC) simulations and found good agreement (with a difference of less than 10{%}), provided the boundary conditions are accurately incorporated in the analytical solution. The slow down of the circumferential velocity of the bulk of the rotating fluid due to the presence of stationary intake tube is studied for stratification parameter in the range 0.707$-$3.535, and found significant slow down (between 8 to 28{%}), which induces the secondary radial flow towards the axis, and it further excites the secondary axial flow, which could be very important for the centrifugal gas separation processes.
机译:建立了高速旋转圆柱体径向边界层的通用解析模型,以研究由于质量,动量和能量在极地旋转到旋转圆柱体中而引起的气体流场。 。解析解包括以主势〜($ chi)$表示的圆柱曲面上径向边界层的六阶微分方程,该方程是从极坐标〜(r-heta)$的运动方程导出的〜飞机。使用线性近似((Pradhan {&} Kumaranextit {,J. Fluid Mech-});(Kumaran {&} Pradhan,extit {J。Fluid Mech-})),其中运动方程以线性顺序被截断速度和压力对基流的扰动,这是一个固体旋转。分析模型中的其他假设包括基本状态下的恒温(等温条件)和高雷诺数,但对分层参数没有限制。将分析解决方案与直接模拟蒙特卡洛(DSMC)仿真进行比较,并发现良好的一致性(相差小于10 {%}),前提是边界条件已准确地合并到分析解决方案中。对于分层参数在0.707 $-$ 3.535范围内的情况,研究了由于存在固定的进气管而导致的大部分旋转流体圆周速度的降低,并且发现显着降低(8至28 {%)之间) ,它会引起朝向轴的二次径向流,并进一步激发二次轴向流,这对于离心气体分离过程可能非常重要。

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