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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 ...
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The effect of end wall boundary layer on matching and corresponding flow control technique for multistage axial compressor

Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2016
Zheng Xinqian, Li Qiushi, Ji Baohua
exaly  

Influence of different loads on the stresses of multistage axial compressor rotors

Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2017
Xinqian Zheng, Yangjun Zhang
exaly  

Adjoint Optimization of Multistage Axial Compressor Blades with Static Pressure Constraint at Blade Row Interface

International Journal of Turbo and Jet Engines, 2016
Lucheng Ji, Weilin Yi
exaly  

Model predictions for improved recoverability of a multistage axial-flow compressor

25th Joint Propulsion Conference, 1989
KEITH BOYER, WALTER O'BRIEN
openaire   +1 more source

Propagation of Acoustic Resonant Modes in a Multistage Axial Compressor

32nd AIAA/CEAS Aeroacoustics Conference (2026)
Simon Sperlich   +2 more
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