A quasi-three-dimensional method for calculating blade surface velocities for an axial flow turbine blade
Quasi-three-dimensional compressible flow analysis for calculating blade surface velocities for axial flow turbine blade
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Quasi-three-dimensional compressible flow analysis for calculating blade surface velocities for axial flow turbine blade
Radial pressure distribution on enclosed rotating disk with or without blades and with radial outward or inward throughflow
Radial pressure distribution on enclosed rotating disk with or without blades and with radial outward or inward throughflow
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Steam filament solution determines velocity distribution due to potential flow in the blade-to-blade plane of the radial impeller. This is used to determine the mass-averaged relative fluid angle, which is in turn used in an axisymmetric program to obtain steam surfaces of the assumed axisymmetric flow.