Measurements of the unsteady flow field near and within a turbine rotor were made by means of a Laser-2-Focus velocimeter. The testing was performed in a single-stage cold-air turbine at part-load and near-design conditions. Random unsteadiness and flow angle results indicate that the secondary vortices of the stator break down after being cut and deformed by the rotor blades. A quantitative comparison shows that some of the energy contained in these secondary vortices is thereby converted into turbulence energy in the front part of the rotor. An attempt is made to explain this turbulence energy production as caused by the vortex breakdown.
Issue Section:
Research Papers
Topics:
Cutting,
Rotors,
Turbines,
Turbulence,
Vortices,
Blades,
Design,
Energy generation,
Flow (Dynamics),
Lasers,
Stators,
Stress,
Testing,
Unsteady flow,
Velocimeters
This content is only available via PDF.
Copyright © 1985
by ASME
You do not currently have access to this content.