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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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A control volume model of rotating stall in multistage axial compressors [PDF]
23rd Joint Propulsion Conference, 1987 Steven Gordon Koff +2 more
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Aerospace Science and Technology, 2019
Sangjo Kim, Kui-soon Kim, C. Son
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Sangjo Kim, Kui-soon Kim, C. Son
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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
Investigating multistage axial flow compressor instabilities
Chinese Journal of Mechanical Engineering (English Edition), 2003openaire +2 more sources
Model predictions for improved recoverability of a multistage axial-flow compressor [PDF]
25th Joint Propulsion Conference, 1989 Walter F. O'Brien, Keith M. Boyer
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Influence of different loads on the stresses of multistage axial compressor rotors
, 2017Xinqian Zheng, C. Ding, Yangjun Zhang
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Numerical investigation of surge and rotating stall in multistage axial compressors
28th Joint Propulsion Conference and Exhibit, 1992Y. Kashiwabara, H. Ishii
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