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- [5] EXPERIMENTAL INVESTIGATION OF ROTATING STALL AND SURGE IN MULTISTAGE, HIGH-LOADED AXIAL-FLOW COMPRESSORS FORSCHUNG IM INGENIEURWESEN-ENGINEERING RESEARCH, 1985, 51 (04): : 116 - 116
- [6] ON THE EVALUATION OF REYNOLDS-NUMBER AND RELATIVE SURFACE-ROUGHNESS EFFECTS ON CENTRIFUGAL-COMPRESSOR PERFORMANCE BASED ON SYSTEMATIC EXPERIMENTAL INVESTIGATIONS JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 1984, 106 (02): : 489 - 501
- [8] Effects of Reynolds number in a small multistage axial flow compressor Hangkong Dongli Xuebao/Journal of Aerospace Power, 2004, 19 (01): : 81 - 88
- [9] SURFACE-ROUGHNESS STUDIES FOR WIND-TUNNEL MODELS USED IN HIGH REYNOLDS-NUMBER TESTING JOURNAL OF AIRCRAFT, 1986, 23 (01): : 56 - 61
- [10] A Correction Method for the Effects of Reynolds Number, Roughness, and Tip Clearance on Geometric Scaling of Axial Compressors JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 2023, 145 (10):