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Study of Unsteady Flow Simulation of Backward Impeller with non-uniform Casing

机译:壳体不均匀的后叶轮非定常流动模拟研究

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摘要

The flow characteristics in the centrifugal fan with difference blade ontlet angles are basically discussed on steady and unsteady simulations for the rectangular casing fan.The blade outlet angles of the impellers are 35° and 25° respectively.The unsteady flow behavior in the passage of the impeller 35° is quite a difference in the steady flow behavior.The large flow separation occurs in the steady flow field and unsteady flow field of the impeller 35° that the flow distribution of the circumferential direction is varied much and the flow separation on the blade is occurred only at the back region of the fan.But the steady flow behavior in the impeller 25°is almost agreed with the unsteady flow behavior that the flow distribution of the circumferential direction is not varied so much and the flow separation on the blade is hardly occurred.When the circumferential variation of the flow in the impeller is large, the steady flow simulation is not coincident to the unsteady flow simulation.
机译:在矩形壳体风扇的稳态和非稳态模拟中,基本讨论了具有不同叶片入口角的离心风扇的流动特性。叶轮的叶片出口角分别为35°和25°。叶轮35°在稳态流动特性上有很大的差异。叶轮35°的稳态流场和非稳态流场中发生大的流分离,从而沿周向的流分布变化很大,叶片上的流分离叶轮25°内的稳态流动特性几乎与非稳态流动特性一致,即周向方向的气流分布变化不大且叶片上的流分离为当叶轮内水流的周向变化较大时,稳态流模拟与非稳态流模拟不一致。 。

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