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Problem of the Flow around a Jet Source

机译:喷射源周围的流动问题

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The problem of the steady plane-parallel flow of an ideal incompressible fluid around a point jet source, i.e., a source from which a fluid with the parameters (density and total pressure) different from the respective free-flow parameters is blown in the presence of a dead zone near the flow separation point, has been solved. The necessity of solving this problem arises in connection with the study of jet collision problems. The solution to similar problems for the case in which the parameters of the fluids in the jet and free flow are the same can be found in [1, 2], If the parameters of the jets are different, the solution of the problem is complicated, because the complex potential function has a discontinuity at the interface between the media and a rather complex iteration process is necessary for determining this interface. The authors of [3] analyzed the problem of the collision of jets that have different Bernoulli constants and flow around a wedge with angle an, but the case of a = 1 was excluded from the analysis, because an essential singularity arises near the flow separation point. In this case, in view of the equality condition for pressures, the angle internal to one of the jets vanishes; i.e., a return-type singular point appears at the boundary of this jet.
机译:理想的不可压缩流体围绕点射流源(即,吹出参数(密度和总压力)与各自的自由流参数不同的流体的源)周围稳定地平行于平面流动的问题解决了分离点附近的死区问题。解决该问题的必要性与喷射碰撞问题的研究有关。在[1,2]中可以找到针对射流中的流体参数和自由流相同的情况的类似问题的解决方案。 ,因为复杂的势函数在介质之间的界面处不连续,因此确定此界面需要相当复杂的迭代过程。 [3]的作者分析了具有不同伯努利常数并且绕着角度为a的楔形流流动的射流的碰撞问题,但是分析中排除了a = 1的情况,因为在流动分离附近会产生本质奇异性点。在这种情况下,鉴于压力相等的条件,其中一个射流的内部角度消失了;即,返回类型的奇异点出现在该射流的边界处。

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