Performance of Truncated Conical Diffusers with Compressible Flow
- 1 December 1972
- journal article
- Published by SAGE Publications in Journal of Mechanical Engineering Science
- Vol. 14 (6) , 382-388
- https://doi.org/10.1243/jmes_jour_1972_014_047_02
Abstract
The performance has been assessed for a variety of geometrical configurations and for inlet Mach numbers ranging from 0·2 to choking. Particular attention has been focused on the developing flow in the tailpipe.Keywords
This publication has 4 references indexed in Scilit:
- The Performance of Truncated Conical DiffusersJournal of Mechanical Engineering Science, 1971
- The Performance of Conical Diffusers Discharging through TailpipesAircraft Engineering and Aerospace Technology, 1970
- Some Preliminary Results for Conical Diffusers with high Subsonic entry mach NumbersJournal of Mechanical Engineering Science, 1966
- AN EXPERIMENTAL INVESTIGATION ON THE EFFECT OF SUBSONIC INLET MACH NUMBER ON THE PERFORMANCE OF CONICAL DIFFUSERSPublished by Defense Technical Information Center (DTIC) ,1966