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O EXPERIMENTAL PROGRAMME
O AEROFOIL AND ROTOR RESPONSE
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actuator disc aerofoil airfoil amplitude anemometer ASME assumption axial clearances axial compressor axial flow compressor axial velocity blade height blade rows blade to blade calculation cascade characteristic circumferential comparison component compressor stage computation constant downstream effect enthalpy equations experimental flow angle flow coefficient flow field flow vector frequency harmonics hot wire inlet guide vanes investigation leading edge lift coefficient low speed mass flow measured method midspan NACA number of cells observed performance perturbation plane position potential flow prediction pressure distortion pressure distribution pressure ratio pressure surface probe propagation velocity pulse radial region rotating stall rotor blade rotor wake RWTH Aachen shown in figure solution stagnation pressure stagnation temperature stall cell static pressure stator stator blade steady streamline suction side suction surface tangential temperature distortion throttle total pressure trailing edge transducers unsteady flow upstream values variation vortex sheet vorticity