Information transfer between tip leakage vortex and blade aerodynamic force of a compressor cascade
Author:
Funder
National Major Science and Technology Projects of China
National Natural Science Foundation of China
Publisher
Elsevier BV
Reference87 articles.
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2. Daniel Moller, H.P. Schiffer. On the mechanism of spike stall inception and near stall nonsynchronous vibration in an axial compressor, ASME Paper GT2020-14711.
3. Measurements of radial vortices, spill forward, and vortex breakdown in a transonic compressor;Brandstetter;J. Turbomach.,2018
4. Clark S.T., Kielb R.E., Hall K.C. Developing a reduced-order model to understand non-synchronous vibration (NSV)in turbomachinery, ASME Paper GT2012-68145.
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