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- [1] AN EXPERIMENTAL INVESTIGATION INTO UNSTEADY BLADE FORCES AND BLADE LOSSES IN AXIAL COMPRESSOR BLADE CASCADE JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 1986, 108 (01): : 47 - 52
- [4] BLADE FORCE-DEFECT MODEL IN THE CASING WALL BOUNDARY LAYER OF AN AXIAL FLOW COMPRESSOR. Nippon Kikai Gakkai Ronbunshu, B Hen/Transactions of the Japan Society of Mechanical Engineers, Part B, 1988, 54 (498): : 430 - 434
- [6] Aerodynamic blade row interactions in an axial compressor - part II: Unsteady profile pressure distribution and blade forces JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2004, 126 (01): : 45 - 51
- [7] MEASUREMENT OF BOUNDARY LAYERS ON A COMPRESSOR BLADE IN CASCADE: PART 1 - A UNIQUE EXPERIMENTAL FACILITY. Journal of Turbomachinery, 1987, 109 (04): : 520 - 526
- [8] Periodical unsteady flow within a rotor blade row of an axial compressor - part 1: Flow field at midspan PROCEEDINGS OF THE ASME TURBO EXPO 2007, VOL 6, PTS A AND B, 2007, : 1575 - 1586
- [10] Aerodynamic blade row interactions in an axial compressor - Part I: Unsteady boundary layer development JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2004, 126 (01): : 35 - 44