Design of Supersonic Nozzle Using CFD

Ibrahim, Omer Musa; Supervisor ,- Eimad Eldin Elhadi

dc.contributor.author	Ibrahim, Omer Musa
dc.contributor.author	Supervisor ,- Eimad Eldin Elhadi
dc.date.accessioned	2013-09-01T08:39:17Z
dc.date.available	2013-09-01T08:39:17Z
dc.date.issued	2012-12-01
dc.identifier.citation	Ibrahim,Omer Musa. Design of Supersonic Nozzle Using CFD/ Omer Musa Ibrahim; Eimad Eldin Elhadi. - Khartoum : Sudan University for Science & Technology, College of Engineering, 2012. - 86p. : ill. ; 28cm.- M.S.c	en_US
dc.identifier.uri	http://repository.sustech.edu/handle/123456789/1394
dc.description	Thesis	en_US
dc.description.abstract	The goal of this research is to design a minimum length supersonic nozzle (MLN) and develops a computer code which uses the Method of Characteristics to design supersonic nozzle contours for isentropic, inviscid, irrotational supersonic flows of any working fluid for any user-defined exit Mach number. The contours were compared to theoretical isentropic exit area ratios and exit area ratios for GA10 nozzle, the percentage of error does not exceed 2% for all exit area ratios, and percentage of error does not exceed 5% for all mass flow rates. Also the contour was compared to Britton’s code, where the difference does not exceed 10% of Britton’s code results.	en_US
dc.language.iso	en	en_US
dc.publisher	Sudan University for Science & Technology	en_US
dc.subject	Supersonic nozzle	en_US
dc.title	Design of Supersonic Nozzle Using CFD	en_US
dc.type	Thesis	en_US