Determination of the influence of the incoming flow on the vortex zones at the entrance to the suction sockets. Part 1. The Axisymmetric problem

A. K. Logacheva, O. Averkova, A. Ziganshin, K. Logachev, E. Popov
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Abstract

The features of the construction of a computational algorithm for calculating circular suction sockets in the conditions of an incoming flow by the method of discrete vortex rings are considered. Flow patterns are given at different ratios of the incoming and intake air flow velocities. The dependences of the characteristic sizes of vortex zones arising at the inlet to the suction-sockets on the velocity of the incoming flow, the length and angle of inclination of the socket are determined. Expressions are obtained for the critical velocity of the incoming flow, at which the flow separation mode for the first vortex zone changes from separation inside the bell to separation outside it. The obtained results can be useful for the construction of local suction systems, profiled according to the found outlines of vortex zones.
确定流入气流对吸气口涡流区的影响。第 1 部分:轴对称问题轴对称问题
研究了在进气流条件下通过离散涡环法计算圆形吸气口的计算算法的构造特点。给出了不同进气流速和进气流速比率下的流动模式。确定了吸入口涡流区的特征尺寸与入流速度、吸入口长度和倾角的关系。得出了入流临界速度的表达式,在该速度下,第一个涡流区的流动分离模式从喇叭口内分离转变为喇叭口外分离。所获得的结果有助于根据所发现的涡流区轮廓建造局部抽吸系统。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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