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Development of a Counter-Rotating Vortex Pair (CVP) Mixer for Aerospace Applications

机译:航空航天应用的逆向涡旋对(CVP)混合器的开发

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Swirling motions induced by a counter-rotating vortex pair (CVP) provides a mechanism to entrain fluid from the periphery of this structure and mix surrounding fluids with those within the vortex structure. Eventually, the vortices act upon each other transporting molecularly mixed fluid into the core flow. This mechanism has potential to increase efficiency with more complete mixing. Therefore, a mixer is proposed which directly induces counter rotating vortices by a three dimensional geometry. The proposed swirl mixer is designed to induce counter rotating vortices based on the potential flow theory, Milne-Thomson's Circle Theorem and Rankine vortex. Twelve test models are developed during the optimization process. Design factors were examined using a seven-hole pressure probe to investigate velocity vector fields produced by the test models, thereby obtaining an optimum CVP mixer that maximized tangential velocity with uniform axial flow.
机译:由反向旋转涡流对(CVP)引起的旋流运动提供了一种机制,可以从该结构的外围夹带流体并将周围的流体与涡流结构内的流体混合。最终,涡旋相互作用,将分子混合的流体输送到岩心流中。这种机制有可能通过更完全的混合来提高效率。因此,提出了一种混合器,其通过三维几何形状直接引起反向旋转的涡旋。拟议的旋流混合器是根据势流理论,Milne-Thomson的圆定理和兰金旋涡设计的,以引起反向旋转的旋涡。在优化过程中开发了十二个测试模型。使用七孔压力探针检查设计系数,以研究由测试模型产生的速度矢量场,从而获得最佳的CVP混合器,该混合器可以使切线速度最大化且轴向流量均匀。

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