Centrifugal compressors, sometimes termed radial
compressors, are a sub-class of dynamic axisymmetric work-absorbing
turbomachinery.
The idealized compressive dynamic turbo-machine
achieves a pressure rise by adding kinetic energy/velocity to a continuous flow
of fluid through the rotor or impeller. This kinetic energy is then converted
to an increase in potential energy/static pressure by slowing the flow through
a diffuser. The pressure rise in impeller is in most cases almost equal to the rise
in the diffuser section. In the case of where flow simply passesthrough a straight pipe to enter a centrifugal compressor; the flow is
straight, uniform and has no vorticity. As illustrated below α1 = 0°. As the
flow continues to pass into and through the centrifugal impeller, the impeller
forces the flow to spin faster and faster. According to a form of Euler's fluid
dynamics equation, known as pump and turbine equation, the energy input to the
fluid is proportional to the flow's local spinning velocity multiplied by the
local impeller tangential velocity.
In many cases the flow leaving centrifugal impeller
is near the speed of sound (340 metres/second). The flow then typically flowsthrough a stationary compressor causing it to decelerate. These stationary
compressors are actually static guide vanes where energy transformation takes
place. As described in Bernoulli's principle, this reduction in velocity causes
the pressure to rise leading to a compressed fluid.




