IIUM Repository (IREP)

CFD analysis of the supersonic nozzle flow with sudden expansion

Ahmed, Khizar Pathan and Dabeer, P.S. and Khan, Sher Afghan (2016) CFD analysis of the supersonic nozzle flow with sudden expansion. IOSR journal of Mechanical & Civil Engineering ( IOSR-JMCE ), 18 (6). pp. 5-7. ISSN 2320-334x

[img] PDF - Published Version
Restricted to Repository staff only

Download (282kB) | Request a copy

Abstract

This paper presents the Computational Fluid Dynamic (CFD) analysis to study the effect of area ratio and nozzle pressure ratio on the flow field of axi-symmetric sudden expansion from convergent-divergent nozzles to a circular duct of larger cross-sectional area than that of nozzle exit area. The study is focusing on the pressure and velocity distribution along axial length. The analysis is done by varying the area ratios and nozzle pressure ratios. The area ratios for the analysis are 1, 2, 4, 6, 8 and 10. The values of nozzle pressure ratios considered are 2, 4, 6, 8 and 10. The results are plotted with the help to graphs. By observing all the results it can be concluded that the flow field in enlarged duct is much affected by area ratio.

Item Type: Article (Journal)
Additional Information: 7395/54295
Uncontrolled Keywords: Area ratio, CFD, Mach number, nozzle pressure ratio, velocity
Subjects: T Technology > TL Motor vehicles. Aeronautics. Astronautics > TL500 Aeronautics
Kulliyyahs/Centres/Divisions/Institutes: Kulliyyah of Engineering > Department of Mechanical Engineering
Depositing User: Prof. Dr. Sher Afghan Khan
Date Deposited: 25 Jan 2017 10:24
Last Modified: 25 Jan 2017 10:24
URI: http://irep.iium.edu.my/id/eprint/54295

Actions (login required)

View Item View Item

Downloads

Downloads per month over past year