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Two and ThreeDimensional Problems of Unsteady Aerodynamics
Mean Loading Effects on Flutter of Subsonic Rotating Annular Cascade
A Method for Predicting Stall Flutter Under Variable Interblade Phase
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acoustic acoustic impedance actuator disk aeroelastic airfoil amplitude analysis annular axial compressor blade row blade surface blade tip blade vibration boundary conditions boundary layer calculation characteristics chord component compressor computational coordinate corresponding decrease diffuser dimensional distortion dynamic effect equation Euler equations exit experimental field turbines finite flow field flow rate flutter boundary flutter velocity grid harmonic increase influence coefficient inlet flow interaction interblade phase angle Kutta condition leading edge lift coefficient linear Mach number measured method mistuning mode model turbine natural frequency Navier-Stokes equation nozzle obtained oscillating cascade outlet paper parameters periodic prediction pressure distribution problem propeller propfan radial ratio reduced frequency region rotating stall rotor rotor blade shock wave shows simulation solution solved sound speed stage stall flutter static pressure stator steady loading steam steam turbine subsonic supersonic torsional total pressure transonic turbomachinery turbomachines unstalled unsteady aerodynamic forces unsteady flow values wake