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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.
For the blade-tip trailing-edge flow regions, at two blade tip gaps the overtip heat transfer decreases normally as the incidence increases.
Most interesting is the determination of the blade tip twist angle.
Improved internal convective cooling is therefore required to increase the blade tip lifetime.
Tip vortex shed from the blade tip was also visualized clearly.
The generation of acoustical signals also changes with the blade tip thickness.
Increased internal convective cooling is therefore required to increase the blade tip lifetime.
Appropriate changes to the blade tip structure can effectively improve fan performance.
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However, blade tip-timing signals are typically under-sampled.
This investigation focuses on the effects of contoured axisymmetric-casing on the blade tip-leakage flow.
First, a sparse representation (SR) mathematical model for sparse blade tip-timing signals is built.
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CEO of Professional Science Editing for Scientists @ prosciediting.com