An Investigation of the Promotion of the Aerodynamic Performance of a Supersonic Compressor Cascade Using a Local Negative-Curvature Ramp
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DOI: 10.3390/app15105664
Abstract: Shockwaves induce considerable flow separation loss; it is essential to reduce this using the flow control method. In this manuscript, a method for suppressing flow separation in turbomachinery through a constant adverse-pressure gradient was investigated.… read more here.
Keywords: compressor cascade; baseline cascade; cascade; negative curvature ... See more keywords