To investigate the coupled effects of secondary flow stability (or ins
tability) due to Coriolis force, and adverse pressure gradient on the
flow in a rotating diffuser of low aspect ratio, quantitative experime
nts were performed. The diffuser had parallel end walls and straight s
ide walls, which could vary its included angle up to 18 deg. Pressure,
mean velocity, and turbulence intensity were measured with a pressure
transducer, hot-wire anemometers, and a transmission system of electr
ical signals from a rotating apparatus to the stationary system. Exper
imental results indicate the formation of a stable large separated flo
w region on the suction side and a through-flow region on the pressure
side. The flow pattern was steady, and once the separation occurred,
the change of the angular velocity had little or no effect on the mean
velocity and turbulence intensity profiles at the midheight of the ro
tating diffuser.