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发表于 2011-11-7 09:01:15
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回复 1# tubaofeng 的帖子
Reid, L. and Moore, R.D., “Design and Overall Performance of Four Highly-Loaded, High SpeedInlet Stages for an Advanced, High Pressure Ratio Core Compressor,” NASA TP–1337, 1978.
在这篇文献里有rotor 37的几何数据,很是详细的。 |
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