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- [4] Aerodynamic blade row interactions in an axial compressor - part II: Unsteady profile pressure distribution and blade forcesJOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2004, 126 (01): : 45 - 51Mailach, RVogeler, K
- [5] Axial compressor blade-to-blade unsteady aerodynamic variabilityJOURNAL OF PROPULSION AND POWER, 2003, 19 (02) : 242 - 249Boyd, DMFleeter, S
- [6] Unsteady aerodynamic blade excitation at the stability limit and during rotating stall in an axial compressorJOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2007, 129 (03): : 503 - 511Mailach, RonaldVogeler, Konrad
- [7] Unsteady aerodynamic blade excitation at the stability limit and during rotating stall in an axial compressorPROCEEDINGS OF THE ASME TURBO EXPO 2006, VOL 6, PTS A AND B, 2006, : 1701 - 1711Mailach, RonaldVogeler, Konrad
- [8] Aerodynamic blade row interactions in an axial compressor - Part I: Unsteady boundary layer developmentJOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2004, 126 (01): : 35 - 44Mailach, RVogeler, K
- [9] UNSTEADY EFFECTS OF BLADE ROW INTERACTION ON FLOW FIELD AND AERODYNAMIC PERFORMANCE OF A TRANSONIC CENTRIFUGAL COMPRESSOR IMPELLERPROCEEDINGS OF ASME TURBO EXPO 2021: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, VOL 2D, 2021,Yamada, KazutoyoKubo, KosukeIwakiri, KenichiroIshikawa, YoshihiroHigashimori, Hirotaka
- [10] Oscillating airfoil aerodynamics of a rotating compressor blade rowJOURNAL OF PROPULSION AND POWER, 2001, 17 (02) : 232 - 239Frey, KKFleeter, S