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Finite volumes simulations of aerodynamic flows based on velocity-vorticity formulations

机译:基于速度涡度公式的空气动力学流动的有限体积模拟

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In small disturbance theories of aerodynamics, the flow field is decomposed into two regions consisting of an inviscid outer region and a viscous inner region of a boundary or shear layer. In both outer and inner regions the governing equations can be written in terms of the divergence and the curl of the velocity. In the outer region, the flow is assumed to be irrotational. In addition, to account for compressibility effects, the flow is assumed to be isentropic. In the inner region, the vorticity equation is obtained by taking the curl of the momentum equation. Furthermore, the governing equations are simplified using boundary layer approximations. Viscous-inviscid interaction procedures are implemented to implicitly couple the calculations in the two regions. Several finite volumes calculations based on the above velocity-vorticity formulations of the two- and three-dimensional incompressible and compressible flows are presented and the results are discussed together with some concluding remarks. The present work provides the results of a unified physical approach for main aerodynamics calculations.
机译:在空气动力学的小扰动理论中,流场被分解为两个区域,包括边界层或剪切层的无粘性外部区域和粘性内部区域。在外部和内部区域,控制方程都可以用速度的发散和卷曲来表示。在外部区域,假定流动是无旋流的。另外,考虑到可压缩性效应,假定流动是等熵的。在内部区域,通过采取动量方程的卷曲来获得涡度方程。此外,使用边界层近似简化了控制方程。实施粘性-无粘相互作用程序以隐式耦合两个区域中的计算。基于上述二维和三维不可压缩和可压缩流动的速度涡度公式,提出了几种有限体积计算方法,并对结果进行了讨论,并附有结论。本工作为主要的空气动力学计算提供了统一物理方法的结果。

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