来自美国NASA-TP-2020报告“STGSTK: A computer code for predicting multistage axial flow compressor performance by a meanline stage stacking method”,采用级叠加法计算压气机一维特性，亲测可用。（此前上传的压缩文件无法正常解压，重新上传）
2021-08-26 16:40:49
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