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Experimental Study of Casing Boundary Layers in a Multistage Axial Compressor
Journal of Fluids Engineering, 1991Measurements of the casing boundary layers were obtained in a four-stage, low speed axial flow compressor, to verify the ‘law of the wall’ applicability to these complex flows. Some of the available shear stress models of the two-dimensional flows have been examined towards the quantitative assessment of skin friction.
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An experimental study of rotor-stator wake unsteadiness in a multistage axial compressor
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2021Jun Li, Chenkai Zhang
exaly
Investigating multistage axial flow compressor instabilities
Chinese Journal of Mechanical Engineering (English Edition), 2003openaire +1 more source
A Quasi-1D model for transonic multistage axial compressors
European Conference on Turbomachinery Fluid Dynamics and Thermodynamics, 2011W. Du, O. Léonard
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Effect of tip clearance and rotor–stator axial gap on the efficiency of a multistage compressor
Applied Thermal Engineering, 2016Shafiq R Qureshi +2 more
exaly
The Influence of Stator Endwall Clearances on Multistage Axial Compressor Aerodynamics
Investigating clearance flows and blockage generation in axial compressors represents a longstanding area of research for enhancing aerodynamic performance and operational stability in turbomachinery. With advancements in computational fluid dynamics (CFD), opportunities to explore these phenomena have expanded, allowing a deeper understanding of the ...openaire +1 more source
Model predictions for improved recoverability of a multistage axial-flow compressor
25th Joint Propulsion Conference, 1989KEITH BOYER, WALTER O'BRIEN
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