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Gust response of a rotating circular cylinder in the vortex suppression regime

机译:旋转圆柱体在涡流抑制状态下的阵风响应

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Numerical investigation is carried out to observe the effect of a single gust impulse on free stream flow and forced convection heat transfer across a two-dimensional steadily rotating circular cylinder. The non-dimensional rotation rate α is varied within the vortex suppression regime i.e. 2 ≤α ≤5 at a Reynolds number of 140 and Prandtl number of 7. Seven different gust profiles in the order of increasing differential kinetic energy imparted to the mean flow; are implemented and their effects are compared. Constant wall temperature (CWT) boundary condition is used to solve the governing equations i.e. continuity, momentum and energy equations. This study notes vortex detachment and asymmetric convection of vortical structures even in the otherwise typical vortex suppression regime of the dimensionless rotation rate due to the inclusion of the gust impulse. Moreover, vortical structure detachment takes place at varying frequencies and only for a very short duration of time. Further evidence pertaining to the average Nusselt number and shear layer stretching and distortion is presented and discussed.
机译:进行了数值研究,以观察单个阵风冲动对二维稳定旋转的圆柱体上自由流和强迫对流换热的影响。无量纲旋转速率α在涡旋抑制范围内变化,即雷诺数为140且普朗特数为7时为2≤α≤5。按照赋予平均流的动能增加的顺序,存在七个不同的阵风分布。实施并比较其效果。恒定壁温(CWT)边界条件用于求解控制方程,即连续性,动量和能量方程。这项研究注意到,即使在由于包含阵风脉冲而导致的无量纲旋转速率的其他典型涡旋抑制机制中,涡旋结构的涡旋脱离和不对称对流。此外,涡旋结构的分离发生在不同的频率,并且仅持续了很短的时间。提出并讨论了有关平均努塞尔数和剪切层拉伸和变形的更多证据。

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