共 50 条
- [31] A NOTE ON THE WEIGHT OF THE BLADES IN AN AXIAL-FLOW COMPRESSOR JOURNAL OF THE AERONAUTICAL SCIENCES, 1953, 20 (06): : 427 - 428
- [33] Secondary flow in cascades with leaned and swept blades - a literature study FORSCHUNG IM INGENIEURWESEN-ENGINEERING RESEARCH, 2000, 65 (08): : 236 - 246
- [34] COMPARATIVE STUDY ON TIP CLEARANCE FLOW FIELDS IN TWO TYPES OF TRANSONIC CENTRIFUGAL COMPRESSOR IMPELLER WITH SPLITTER BLADES PROCEEDINGS OF THE ASME TURBO EXPO 2010: TURBOMACHINERY: AXIAL FLOW FAN AND COMPRESSOR AERODYNAMICS DESIGN METHODS, AND CFD MODELING FOR TURBOMACHINERY, VOL 7, PTS A-C, 2010, : 2053 - 2063
- [36] SECONDARY FLOW EFFECTS ON GAS EXIT ANGLES IN RECTILINEAR CASCADES JOURNAL OF ENGINEERING FOR POWER-TRANSACTIONS OF THE ASME, 1975, 97 (01): : 93 - 100
- [37] Experimental investigation on exit flow fields of a transonic compressor with high-turning bowed-twisted stator Kung Cheng Je Wu Li Hsueh Pao/Journal of Engineering Thermophysics, 2010, 31 (10): : 1659 - 1662
- [38] Effects of blade curved on compressor cascades with different camber angles under different incidences Hangkong Dongli Xuebao, 2007, 3 (406-411):