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The effects of blade reshaping on shock system, tip clearance flow and flow separation at hub are examined.
Both the plate and the adjacent blade vibration induce an acoustic feedback that propagates within the jet and blade tip clearance flow, respectively.
A study of velocity and pressure fluctuations in the tip clearance flow of an axial fan is presented in this paper.
In an effort to reduce the blade tip clearance leakage in turbine designs, this article aims to numerically investigate the effects of active jet-flow injected from the blade tip platform upon the blade tip clearance flow.
So the blocking effect of pressure side/tip junction separation bubble on clearance flow prevents more flow on the tip pressure side from leaking to the suction side, which results in weaker leakage vortex and less associated losses.
In this way, the article elucidates the mechanism of active injection control, analyzes the topological tip clearance flow structure, and, finally, calculates the turbine efficiency considering the effects of the jet-flow.
Similar(47)
Study of rotor tip-clearance flow using large-eddy simulation.
Large-eddy simulation of a rotor tip-clearance flow.
Study of Tip-Clearance Flow and Stator-Rotor Interaction Using Large-Eddy Simulation.
Vortex dynamics and low-pressure fluctuations in the tip-clearance flow.
Vortex dynamics and mechanisms for viscous losses in the tip-clearance flow.
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CEO of Professional Science Editing for Scientists @ prosciediting.com