共 50 条
- [1] AEROELASTICITY OF COMPRESSOR BLADES - SUBSONIC STALL FLUTTER. [J]. Recherche Aerospatiale (English Edition), 1981, (06): : 47 - 59
- [3] An experimental investigation of the subsonic stall flutter [J]. Proceedings of ISMA2006: International Conference on Noise and Vibration Engineering, Vols 1-8, 2006, : 1603 - 1614
- [5] SUBSONIC UNSTEADY AERODYNAMIC PRESSURES ON COMPRESSOR BLADES [J]. COMPTES RENDUS HEBDOMADAIRES DES SEANCES DE L ACADEMIE DES SCIENCES SERIE A, 1972, 274 (10): : 863 - &
- [6] Method for Predicting Unsteady Vibration of Gas Turbine Compressor Blades Under Subsonic Near-Stall Conditions [J]. JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 2014, 136 (12):
- [7] Mechanisms and Key Parameters for Compressor Blade Stall Flutter [J]. JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2013, 135 (02):
- [8] CALCULATION OF UNSTEADY SUBSONIC AERODYNAMIC PRESSURES ON COMPRESSOR BLADES [J]. RECHERCHE AEROSPATIALE, 1973, (01): : 41 - 49
- [10] Rotating stall and stall-controlled performance of a single stage subsonic axial compressor [J]. Journal of Thermal Science, 2006, 15 : 1 - 13