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Mathematics of Turbomachinery: Centrifugal Impeller

机译:涡轮机械数学:离心叶轮

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摘要

The mathematics required to design and analyze turbomachinery were gathered from many sources and presented in its entirety as a single source, step-by-step procedure. An impeller was then designed and analyzed. A one-dimensional (1D) model explains the mathematics for performance in detail. The 1D model lacked the ability to predict flow-related phenomena such as flow surge but highlighted the direct connection between blade angle and rotation direction with pressure rise and efficiency. For the present study, positive blade angles pointing in the direction of rotation (clockwise in the present study) provided higher pressure rise and higher losses. Negative blade angles pointing in the opposite direction of rotation (counterclockwise in the present study) resulted in lower pressure rise and lower losses. Flow surge was studied with a three-dimensional (3D) model. The 3D model confirmed counterclockwise rotation as the most efficient rotation direction and identified areas of flow surge. Both models found pressure rise across the turbomachine under study was higher for the clockwise rotation.
机译:从许多来源收集设计和分析涡轮机所需的数学,并作为单一来源,作为单一来源,逐步呈现。然后设计和分析叶轮。一维(1D)模型详细解释了数学进行了性能。 1D模型缺乏预测流动相关现象的能力,例如流量浪涌,而是突出显示叶片角度和旋转方向之间的直接连接,具有压力升高和效率。对于本研究,正叶片角度指向旋转方向(在本研究中顺时针方向)提供了更高的压力升高和更高的损失。在相反的旋转方向上指向的负叶片角度(在本研究中逆时针)导致较低的压力升高和较低的损耗。使用三维(3D)模型研究了流动浪涌。 3D模型确认逆时针旋转作为最有效的旋转方向,并确定流量浪涌区域。在顺时针旋转时,两种模型都发现涡轮机跨越涡轮机的压力升高。

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