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Experimental Turbine Research at DLR Goettingen

机译:DLR哥廷根的涡轮机研究

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摘要

At DLR Goettingen (Germany) two windtunnels especially adapted to turbine research in the transonic flow regime are available. These are the "Windtunnel for Straight Cascades" and the "Windtunnel for Rotating Cascades". The Straight Cascade windtunnel is of blow-down type, operating in the Mach number range of 0.2 to 1.6. The Rotating Cascade Tunnel is a facility with closed flow path enabling the independent variation of Mach and Reynolds number. In the Rotating Cascade Tunnel the investigated objects range from isolated vanes to 1.5 stages. In the following the features of the windtunnels will be described and some experimental results shown.
机译:在DLR哥廷根(德国),有两个特别适用于跨音速流动状态下的涡轮研究的风洞。它们是“直叶栅风道”和“旋转叶栅风道”。直联级联风洞是放气式的,在0.2至1.6的马赫数范围内运行。级联旋转隧道是一种具有封闭流道的设施,可独立改变马赫数和雷诺数。在旋转叶栅隧道中,研究对象的范围从孤立的叶片到1.5级。在下文中,将描述风洞的特征并显示一些实验结果。

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