Numerical investigation of inlet boundary layer skew in axial-flow compressor cascade and the corresponding non-axisymmetric end wall profiling
Proceedings of the Institution of Mechanical Engineers / A ; 228 , 6 ; 638-656
2014
Aufsatz (Zeitschrift)
Englisch
BKL: | 52.50 Energietechnik: Allgemeines / 52.30 Strömungskraftmaschinen, Turbomaschinen / 52.30 / 52.50 | |
Lokalklassifikation TIB: | 275/5345/5365/5500 |
Numerical investigation of the axial compressor performance with inlet distortions
SAGE Publications | 2018
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