共 50 条
- [31] EFFECTS OF THE INLET BOUNDARY LAYER THICKNESS ON ROTATING STALL IN AN AXIAL COMPRESSOR PROCEEDINGS OF THE ASME TURBO EXPO 2008, VOL 6, PT A, 2008, : 497 - 507
- [33] Experimental study of the mechanism of improving stall margin of low speed axial-flow compressor with micro-injection under rotating inlet distortion Hangkong Dongli Xuebao/Journal of Aerospace Power, 2010, 25 (01): : 67 - 71
- [37] INFLUENCE OF FLOW DISTORTIONS ON AXIAL FLOW FAN + ON ROTATING STALL ZEITSCHRIFT FUR ANGEWANDTE MATHEMATIK UND PHYSIK, 1964, 15 (02): : 116 - &
- [39] A numerical simulation of rotating stall in axial flow fans Nippon Kikai Gakkai Ronbunshu, B Hen/Transactions of the Japan Society of Mechanical Engineers, Part B, 2002, 68 (672): : 2169 - 2177
- [40] Rotating stall control in a high-speed stage with inlet distortion: Part II - Circumferential distortion JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 1999, 121 (03): : 517 - 524