S1BYL2 is an inviscid-viscous blade-to-blade method for calculating the detailed aerodynamics and overall performance of compressor blades. It may be applied either on its own to predict the flow for individual blade sections, such as the midspan of a linear cascade, or in conjunction with a throughflow calculation to predict the performance of a complete axial compressor. New predictions for the V2 and ARL SL19 cascades and for the high speed compressor cases are presented. It is hoped that this will be one of many sets of calculations for these cases, so that an improved understanding of each case may be obtained, together with an appreciation of the strengths and weaknesses of different computational approaches.
Application of S1BYL2 to the AGARD WG18 Compressor Test Cases
1992
16 pages
Report
No indication
English
AGARD Handbook (Including AGARD By-Laws)
NTIS | 1971
AGARD engine disc cooperative test programme
TIBKAT | 1988
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