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NUMERICAL SIMULATION METHOD FOR COMPRESSIBLE VORTEX FLOW FIELD

机译:可压缩涡流场的数值模拟方法

摘要

The present invention is a numerical simulation method for a compressible vortex flow field. The method is mainly characterized in that the flux of a vorticity diffusion compensation item is added to a computational grid boundary and used for compensating the excessive diffusion of the vorticity caused by separation of the diffusion direction of vorticity from the maximum change gradient direction of the modulus of the vorticity. The vorticity diffusion compensation item and an artificial diffusion item should be equivalent to each other and have opposite effects. The method is referred to as a vorticity diffusion compensation technology. The vorticity diffusion compensation item is added after the artificial diffusion item is added to a convection item, so a stability policy of the original numerical solution is not affected; the vorticity diffusion compensation item is caused by numerical viscosity, and is along the cross product direction of the diffusion item direction of the vorticity and the maximum gradient change direction of the modulus of the vorticity.
机译:本发明是用于可压缩涡流场的数值模拟方法。该方法的主要特征在于,将涡度扩散补偿项的通量添加到计算网格边界,并用于补偿由于涡度的扩散方向与模量的最大变化梯度方向分离而引起的涡度的过度扩散。涡度。涡度扩散补偿项和人工扩散项应彼此等效并且具有相反的效果。该方法称为涡度扩散补偿技术。在将人工扩散项添加到对流项之后再添加涡度扩散补偿项,因此不会影响原始数值解的稳定性。涡度扩散补偿项是由数值粘度引起的,并且沿着涡度扩散项方向和涡度模量的最大梯度变化方向的叉积方向。

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