Rao, DM (1971) A method of flow stabilisation with high pressure recovery in short, conical diffusers. The Aeronautical Journal, 75. pp. 336-339.
![[img]](https://nal-ir.nal.res.in/style/images/fileicons/application_pdf.png) |
PDF
method_of_flow.pdf Download (754kB) |
![[img]](https://nal-ir.nal.res.in/style/images/fileicons/other.png) |
Indexer Terms (Generate index codes conversion from application/pdf to indexcodes)
indexcodes.txt Download (8kB) |
Abstract
The problem of obtaining proper flow spreading together13; with useful pressure recovery across rapidly expanding13; diffusers is of considerable practical importance, Many13; different approaches to this end have, been reported in13; literature, e.g. vortex generators, screens or bailies, surface roughness, corrugations, etc., apart from the use of direct boundary-layer control. These methods have the common13; aim of preventing separation from the walls of the diffuser. 13; 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.
| Item Type: | Article |
|---|---|
| Additional Information: | Copyright for this article belongs to the Royal Aeronautical Society |
| Uncontrolled Keywords: | Conical flow;Diffusers;Flow stability;Pressure recovery; Conical nozzles;Flow measurement;Gas expansion;Performance tests;Radial flow;Steady flow;Velocity distribution |
| Subjects: | ENGINEERING > Fluid Mechanics and Thermodynamics |
| Depositing User: | Mr. Ravikumar R |
| Date Deposited: | 20 Dec 2006 |
| Last Modified: | 24 May 2010 04:24 |
| URI: | http://nal-ir.nal.res.in/id/eprint/3741 |
Actions (login required)
 |
View Item |
