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Model blade for flow simulation has chord length and surface of subsonic model blade scaled to simulate supersonic flow

机译:用于流动模拟的模型叶片的弦长和亚音速模型叶片的表面按比例缩放以模拟超音速流动

摘要

The model blade is to simulate the flow of the transonic flow relation of a gas turbine blade in a compressor by means of subsonic flow over the model blade. The chord length and the surface of the model blade which is to be subjected to the subsonic flow are scaled in such a manner as to simulate the transonic flow relation of the gas turbine blade being simulated.
机译:模型叶片用于通过模型叶片上的亚音速流来模拟压缩机中的燃气涡轮叶片的跨音速流动关系。弦长和要经受亚音速流的模型叶片的表面按比例缩放,以模拟所模拟的燃气涡轮叶片的跨音速流动关系。

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