首页> 外文会议>International conference on nuclear engineering >A COMPRESSIBLE THREE-DIMENSIONAL INVERSE DESIGN METHOD BASED ON THE STREAMLINE CURVATURE APPROACH AND CLEBSCH FORMULATION FOR RADIAL AND MIXED FLOW TURBOMACHINES
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A COMPRESSIBLE THREE-DIMENSIONAL INVERSE DESIGN METHOD BASED ON THE STREAMLINE CURVATURE APPROACH AND CLEBSCH FORMULATION FOR RADIAL AND MIXED FLOW TURBOMACHINES

机译:一种基于流线曲率曲曲线法和尖端混合流动涡轮机的压缩三维反向设计方法

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The through-flow inverse design method based on the streamline curvature approach is nowadays a widely used quasi-3-dimensional blades design method for radial and mixed flow turbomachines. The main limitation of this method is using the flow field on the mean stream surface S_(2,m) to approximate the actual 3-dimensional flow field. Without an effective description of the periodic flow, it is impossible for this method to realize exactly the prescribed circumferentially averaged swirl rV_θ. Is there any way to develop this classical through-flow inverse method to a 3-dimensional one conveniently? The answer is yes. A new compressible 3-dimensional inverse design method for radial and mixed flow turbomachines is presented in this paper. This new 3-dimensional inverse method provides a convenient and effective way to obtain the periodic flow field for the streamline curvature through-flow inverse method. Meanwhile, compared with another type of similar 3-dimensional inverse method firstly described by Tan etc. based on Stokes stream functions and Monge potential functions from the Clebsch formulation to calculate the circumferentially averaged flow and the periodic flow respectively, this new method has its own advantages. In order to assess the usefulness of the new method, four centrifugal impellers are designed under the same design specifications by four different inverse methods respectively. They are two quasi-3-dimensional streamline curvature through-flow inverse methods without and with a slip factor model, a 3-dimensional approximated inverse approach based on stream functions and Monge potential functions and the 3-dimensional inverse method presented here. The performances of the four impellers yielding from a RANS commercial solver are compared. The capabilities of the four methods to realize the target circumferentially averaged swirl are also studied.
机译:通流逆设计方法基于所述流线曲率的方法是现今用于径向和混合流涡轮机广泛使用的准3维叶片设计方法。该方法的主要限制是使用上的平均流表面S_(2,M)的流场近似实际的三维流场。没有周期性流的有效的描述中,这是不可能的这个方法来实现准确规定的圆周平均涡流rV_θ。有什么办法来开发这个经典的穿流反推法方便三维一个?答案是肯定的。一种新的可压缩的3维逆设计用于径向和混合流涡轮机方法被提出本文。这种新的3维逆方法提供了一种方便和有效的方式,以获得所述周期性流场为通流逆方法的流线曲率。同时,与另一种类型由谈等基于从Clebsch制剂来计算圆周平均流量和分别周期性流动斯托克斯流功能和Monge的势函数首先描述相似3维逆方法相比,这种新方法具有其自身的好处。为了评估新的方法的有用性,四次离心叶轮在相同的设计规格由四个不同的反演方法分别设计的。它们是两个准3维流线曲率逆方法通流不具有和具有滑移系数模型的基础上,流功能和Monge的潜在功能的3维近似逆算法和3维逆方法呈现在这里。四个叶轮从RANS商业求解器产生的性能进行了比较。这四种方法的能力以实现目标圆周平均涡流进行了研究。

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