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Wake-induced boundary layer transition in a low-speed axial compressor

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Publication:1417660
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DOI10.1023/A:1027398920038zbMath1113.76381OpenAlexW203374461MaRDI QIDQ1417660

Konrad Vogeler, Ronald Mailach

Publication date: 5 January 2004

Published in: Flow, Turbulence and Combustion (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1023/a:1027398920038


zbMATH Keywords

boundary layerunsteady flowaxial compressorturbomachinewake-induced transition


Mathematics Subject Classification ID

Turbulence (76F99)


Related Items (1)

Recent German research on periodical unsteady flow in turbomachinery







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