Numerical investigation into the mechanism regarding the inception and evolution of flow unsteadiness induced by the tip leakage flow in a transonic compressor
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DOI: 10.1177/0957650920910597
Abstract: Unsteady flow in the blade tip region of modern axial flow compressors is one of the sources of loss, noise, and blade vibration. In some cases, it is potentially linked to stall inception. In this… read more here.
Keywords: tip leakage; induced tip; flow unsteadiness; leakage vortex ... See more keywords