Abstract
Cockrell and Markland have found that the static-pressure recovery coefficient of a conical diffuser, which is well known to decrease as the (turbulent) boundary layer thickness at entry increases, actually rises again when the inlet boundary layer is so thick as to approximate to fully-developed pipe flow. It may be noted that this is not a consequence of the definition of the pressure coefficient because, for typical pipe flow velocity profiles, the pressure coefficient based on mean velocity, , is very nearly the same as that based on momentum flux .
Publisher
Cambridge University Press (CUP)
Reference2 articles.
1. Reid J. The Effects of a Cylindrical Shroud on the Performance of a Stationary Convergent Nozzle. ARC R & M 3320, 1963.
2. The Effects of Inlet Conditions on Incompressible Fluid Flow Through Conical Diffusers
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