The geometry of the region between the impeller tip and diffuser throat is
accepted as being very influential, little understood and crucial to the pe
rformance of centrifugal compressors. This paper presents an experimental i
nvestigation of the flow in this region where the diffusing section of the
compressor is of the 'pipe diffuser' configuration. The results are present
ed with an emphasis on design-type correlations. The principal features und
er investigation were the size of the diffuser throat and the influence of
the number of diffuser passages.