Stall prediction of in-flight compressor due to flamming of refueling leakage near inlet

DOI10.1007/S00466-003-0425-4zbMath1038.76541OpenAlexW4231992550MaRDI QIDQ1420031

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

Publication date: 28 January 2004

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

Full work available at URL: https://doi.org/10.1007/s00466-003-0425-4

zbMATH Keywords

Critical distortion lineIntegral methodCompressor performanceDistorted inlet flowmid-air refueling

Mathematics Subject Classification ID

Gas dynamics (general theory) (76N15)

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