University of North Texas Digital Library (University of North Texas) · 1949 · 11 citations · 0 references
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EngineeringAerospace EngineeringAerodynamicsComputational Fluid DynamicsFluid DynamicsExperimental AerodynamicsGas Turbine EnginesGas Turbine PropulsionLow-speed AerodynamicsVortex DynamicsVortex VisualizationBlade AerodynamicsBlade DesignCombustor AerodynamicsTurbine AerodynamicsTurbine Blade AerodynamicsTurbine DesignTurbinesVortex Flow
Report presenting a comparison between the calculated design performance of a gas-turbine stator blade and its performance in a sector of an annular cascade tunnel. The gas velocities on the blade surface were computed by the stress filament method and compared with experimental values, with which they agreed satisfactorily. Results regarding discharge angle, vane-surface-velocity distribution, tangential- and axial-velocity distribution, and radial-equilibrium consideration are provided.