Hostname: page-component-586b7cd67f-vdxz6 Total loading time: 0 Render date: 2024-11-28T17:09:11.118Z Has data issue: false hasContentIssue false

A Method of Flow Stabilisation with High Pressure Recovery in Short, Conical Diffusers

Published online by Cambridge University Press:  04 July 2016

D. M. Rao*
Affiliation:
National Aeronautical Laboratory, Bangalore

Extract

The problem of obtaining proper flow spreading together with useful pressure recovery across rapidly expanding diffusers is of considerable practical importance. Many different approaches to this end have been reported in literature, e.g. vortex generators, screens or baffles, surface roughness, corrugations, etc., apart from the use of direct boundary-layer control. These methods have the common aim of preventing separation from the walls of the diffuser. With increasing expansion angle and area-ratio, however, the effectiveness of these methods either breaks down or is obtained at a high cost of pressure recovery.

Type
Technical Notes
Copyright
Copyright © Royal Aeronautical Society 1971 

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

1. Rao, D. M. and Raju, K. N. The Use of Splitters for Flow Control in Wide Angle Diffusers. National Aeronautical Laboratory, Bangalore, India. TN-AE-26-64, 1964.Google Scholar
2. Cockrell, D. J. and Markland, E. Effect of Inlet Conditions on Incompressible Flow Through Conical Diffusers. Journal Royal Aeronautical Society, Vol. 66, pp. 5152, January 1962.Google Scholar