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Computational and experimental investigations of performance curve of an axial flow fan using downstream flow resistance method

机译:下游流阻法计算轴流风机性能曲线的实验研究

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摘要

A newly developed computational approach different from the conventional methods which are popularly adopted by the fan designers is employed to study the flow field and performance characteristics of an axial flow fan by using the commercial code(STAR-CD)of computational fluid dynamics. The new approach, which is termed the "downstream flow resistance"(DFR)method, engages the flow resistance of the fan test bench in the downstream area of the computational domain. Both the static and moving grids are employed in the computation. The results show at least three emphases. Firstly, the deviations of the calculated fan performance curves from the experimental results can attain levels less than 3% and 1.5% by using the DFR method with static-grid and moving-grid schemes, respectively. These results present dramatic improvement over the maximum deviation of about 26% obtained by using the conventional method with the static-grid scheme. Secondly, usage of the static or moving grids for the purpose of fan performance prediction is no longer an important issue when the DFR method is employed because both the static and moving grids show almost identical results. Thirdly, the stall occurs when the aerodynamic contour of the fan blade is inappropriately designed for the mid and high back-pressure operations. Under this situation, recirculation bubble would appear around the trailing edge of the suction surface of the fan blade, and therefore obstructs the development of the flow. At deep-stall, large recirculation flow structures may even appear around the pressure surface and block the passage between the neighboring fan blades to cause the reduction of flow rate.
机译:通过使用商业上的计算流体动力学代码(STAR-CD),采用一种不同于风扇设计者普遍采用的常规方法的新开发的计算方法来研究轴流风扇的流场和性能特性。被称为“下游流动阻力”(DFR)方法的新方法将风扇测试台的流动阻力引入计算域的下游区域。在计算中既使用静态网格又使用移动网格。结果显示至少三个重点。首先,通过将DFR方法与静态网格和移动网格方案分别使用,计算出的风扇性能曲线与实验结果的偏差可以分别达到3%和1.5%以下的水平。这些结果相对于使用常规方法和静态网格方案获得的最大偏差(约26%)提出了显着改善。其次,当采用DFR方法时,出于风扇性能预测的目的而使用静态或移动网格不再是重要的问题,因为静态和移动网格都显示几乎相同的结果。第三,当风扇叶片的空气动力学轮廓设计得不适合中高背压操作时,就会发生失速。在这种情况下,再循环气泡将出现在风扇叶片吸入表面的后缘周围,从而阻碍了气流的发展。在深度失速时,大的再循环流动结构甚至可能出现在压力表面周围,并阻塞相邻风扇叶片之间的通道,从而导致流速降低。

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