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Unsteady aerodynamics in an axial flow compressor
2001Current methods for designing compressor blades in axial turbomachines assume that the flow through each blade row is steady. However, interactions associated with the relative motion of neighbouring blade rows are known to produce a disturbance field with both random and periodic components.
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A-to-Z Guide to Thermodynamics, Heat and Mass Transfer, and Fluids Engineering, 2006
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Flow separation control in an axial compressor cascade using various arrangement of plasma actuator
Journal of Electrostatics, 2021Nima Amanifard, Hamed Mohaddes Deylami
exaly

