In this paper the application of 3D inverse design code TURBOdesign1 to the design of the vane geometry of a centrifugal compressor vaned diffuser is presented. For this study the new diffuser is designed to match the flow leaving the conventional impeller, which is highly non-uniform.
CFD predictions confirmed the considerable reduction in loss in the new inverse vaned diffuser both at design (30% lower) and lower than design (50% lower) flow conditions. Also the diffuser exit flow non-uniformity was found to be significantly lower in the inverse designed diffuser at all flow conditions considered.