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Study of Unsteady Transonic Flows with a New Mixed Van Leer Flux Splitting Method
and 3Dimensional Calculations in Cascades
A Panel Code for the Analysis of Blade Flutter and Blade Interference Effects
37 other sections not shown
acoustic actuator surface aeroacoustic Aeroelasticity Aeroelasticity of Turbomachines AIAA airfoil amplitude analysis angle of attack ASME axial blade oscillation blade row blade surface blade vibration boundary conditions boundary layer calculations cascade cavitation chord component compressor computed deep stall diffuser downstream effect equations Euler Euler equations experimental Figure flow angle flow field fluid flutter flux grid harmonic inlet interaction interblade phase angle inviscid leading edge Mach number Mach wave mean flow measured mesh method mode Navier-Stokes Navier-Stokes equations oscillation passage pitch plane position predicted pressure distribution pressure fluctuation pressure surface propagation ratio reduced frequency region Reynolds number rotating stall rotor rotor-stator scheme separation bubble SFLOW shock wave shown in Fig shows simulation solution stall cell static pressure stator steady subsonic suction surface supersonic torsional trailing edge transonic transonic flow turbine Turbomachinery unsteady aerodynamic force unsteady flow unsteady pressure upstream values vector velocity vortex vortices wake