Investigation of the effects of nozzle exit mach number and nozzle pressure ratio on axisymmetric flow through suddenly expanded nozzles
Computational Fluid Dynamics simulations were carried out using ANSYS FLUENT for suddenly expanded flow through the convergent-divergent nozzle and a suddenly expanded duct. The Length-to-Diameter ratio of 10 for the duct was used in the analysis. Also, an Area Ratio between CD Nozzle exit area and...
Main Authors: | Khan, Sher Afghan, Mohiuddin, M, Saleel, Ahmad C, G M, Fharukh |
---|---|
Format: | Article |
Language: | English English |
Published: |
Blue Eyes Intelligence Engineering & Sciences Publication
2019
|
Subjects: | |
Online Access: | http://irep.iium.edu.my/71059/ http://irep.iium.edu.my/71059/ http://irep.iium.edu.my/71059/7/71059%20Investigation%20of%20the%20effects%20of%20nozzle%20exit%20mach%20number.pdf http://irep.iium.edu.my/71059/8/71059%20Investigation%20of%20the%20effects%20of%20nozzle%20exit%20mach%20number%20SCOPUS.pdf |
Similar Items
-
Investigation on the prominence of abrupt expansion on the base pressure of an axi-symmetric body
by: Bashir, Musavir, et al.
Published: (2017) -
CFD analysis of effect of Mach number, area ratio and nozzle pressure ratio on velocity for suddenly expanded flows
by: Pathan, Khizer Ahmed, et al.
Published: (2017) -
Investigation of base flow for an axisymmetric suddenly
expanded nozzle with micro JET
by: Chaudhary, Zakir Ilahi, et al.
Published: (2018) -
Combined effect of nozzle pressure ratio and screech prone supersonic mach number in a suddenly expanded flow
by: Bashir, Musavir, et al.
Published: (2015) -
CFD analysis of CD nozzle and effect of nozzle pressure ratio on pressure and velocity for suddenly expanded flows
by: Khan, Sher Afghan, et al.
Published: (2018)