Study on the propagation of inlet flow distortion in axial compressor using an integral method

DOI10.1007/S00466-002-0362-7zbMath1018.76521OpenAlexW4239150524MaRDI QIDQ1404585

H. N. Lim, T. L. Tan, Ningyu Liu, Eddie Yin-Kwee Ng

Publication date: 21 August 2003

Published in: Computational Mechanics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s00466-002-0362-7

zbMATH Keywords

Axial flow compressorCritical distortion lineInlet distortionIntegral method

Mathematics Subject Classification ID

Jets and cavities, cavitation, free-streamline theory, water-entry problems, airfoil and hydrofoil theory, sloshing (76B10)

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