Numerical analysis of convergent-divergent nozzle using finite element method
In this paper, Finite element method (FEM) were used to simulate the different flow configuration. Convergent divergent (CD) nozzle was considered with extended divergent duct. 1 mm of micro jets orifice diameter were arranged at ninety degrees at PCD 13 mm to control base pressure in a suddenly exp...
| Main Authors: | G M, Fharukh Ahmed, Al-Robaian, Abdul Rehman A, Aabid, Abdul, Khan, Sher Afghan |
|---|---|
| Format: | Article |
| Language: | English English |
| Published: |
Transstellar Journal Publications and Research Consultancy Private Limited
2018
|
| Subjects: | |
| Online Access: | http://irep.iium.edu.my/67481/ http://irep.iium.edu.my/67481/7/67481%20NUMERICAL%20ANALYSIS%20OF%20CONVERGENT-DIVERGENT%20NOZZLE.pdf http://irep.iium.edu.my/67481/13/67481_Numerical%20analysis%20of%20convergent-divergent%20nozzle%20using%20finite%20element%20method_scopus.pdf |
Similar Items
Modeling and analysis of convergent divergent nozzle with
sudden expansion duct using finite element method
by: Aabid, Abdul, et al.
Published: (2019)
by: Aabid, Abdul, et al.
Published: (2019)
Experimental investigation of flow through convergent nozzle and the influence of micro jets on the enlarged duct flow field
by: Ashfaq, Syed, et al.
Published: (2014)
by: Ashfaq, Syed, et al.
Published: (2014)
CFD analysis of the supersonic nozzle flow with sudden expansion
by: Ahmed, Khizar Pathan, et al.
Published: (2016)
by: Ahmed, Khizar Pathan, et al.
Published: (2016)
Control of suddenly expanded flow from correctly expanded nozzles
by: Khan, Sher Afghan, et al.
Published: (2004)
by: Khan, Sher Afghan, et al.
Published: (2004)
Active control of suddenly expanded flow from under expanded nozzles
by: Khan, Sher Afghan, et al.
Published: (2004)
by: Khan, Sher Afghan, et al.
Published: (2004)
Base pressure studies from over expanded nozzle for area ratio 2.56
by: Baig, Maughal Ahmed Al, et al.
Published: (2012)
by: Baig, Maughal Ahmed Al, et al.
Published: (2012)
Modelling and analysis of convergent divergent nozzle with
sudden expansion duct using finite element method
by: Aabid, Abdul, et al.
Published: (2019)
by: Aabid, Abdul, et al.
Published: (2019)
Influence of micro jets on the flow development in the enlarged duct at supersonic Mach number
by: Khan, Sher Afghan, et al.
Published: (2019)
by: Khan, Sher Afghan, et al.
Published: (2019)
Experimental studies of the base flow from the nozzles with sudden expansion with micro jets
by: Chaudhary, Zakir Ilahi, et al.
Published: (2016)
by: Chaudhary, Zakir Ilahi, et al.
Published: (2016)
Numerical simulation of suddenly expanded flow at Mach 2.2
by: Aabid, Abdul, et al.
Published: (2019)
by: Aabid, Abdul, et al.
Published: (2019)
A new approach to low-cost open-typed subsonic compressible flow wind tunnel for academic purpose
by: Al-Robaian, Abdul Rehman A, et al.
Published: (2018)
by: Al-Robaian, Abdul Rehman A, et al.
Published: (2018)
Control of nozzle flow in a suddenly expanded duct with micro jets
by: Baig, Maugal Ahmed Ali, et al.
Published: (2012)
by: Baig, Maugal Ahmed Ali, et al.
Published: (2012)
Inspection of supersonic flows in a CD nozzle using experimental method
by: Azami, Muhammad Hanafi, et al.
Published: (2019)
by: Azami, Muhammad Hanafi, et al.
Published: (2019)
Experimental investigation of the base flow from the nozzles with sudden expansion
by: Chaudhary, Zakir Ilahi, et al.
Published: (2015)
by: Chaudhary, Zakir Ilahi, et al.
Published: (2015)
Combined effect of nozzle pressure ratio and screech prone supersonic mach number in a suddenly expanded flow
by: Bashir, Musavir, et al.
Published: (2015)
by: Bashir, Musavir, et al.
Published: (2015)
Experimental and numerical studies on flow from axisymmetric nozzle flow with sudden expansion for Mach 3.0 using CFD
by: Quadros, Jaimon Dennis, et al.
Published: (2016)
by: Quadros, Jaimon Dennis, et al.
Published: (2016)
CFD analysis of convergent-divergent nozzle flow and base pressure control using micro-JETS
by: Khan, Ambareen, et al.
Published: (2018)
by: Khan, Ambareen, et al.
Published: (2018)
Analysis of area ratio in a CD nozzle with suddenly expanded
duct using CFD method
by: Khan, Sher Afghan, et al.
Published: (2019)
by: Khan, Sher Afghan, et al.
Published: (2019)
Base pressure control by supersonic micro jets in a suddenly expanded nozzle
by: Khan, Sher Afghan, et al.
Published: (2018)
by: Khan, Sher Afghan, et al.
Published: (2018)
Experimental studies on low speed converging nozzle flow with sudden expansion
by: Ashfaq, Syed, et al.
Published: (2014)
by: Ashfaq, Syed, et al.
Published: (2014)
Numerical simulations of a CD nozzle and the influence of the duct length
by: Akhtar, Mohammad Nishat, et al.
Published: (2019)
by: Akhtar, Mohammad Nishat, et al.
Published: (2019)
Control of nozzle flow using microjets at supersonic Mach Regime
by: G M, Fharukh, et al.
Published: (2019)
by: G M, Fharukh, et al.
Published: (2019)
Accurate geometric stiffness matrix formulation of beam finite element
by: Sulaeman, Erwin
Published: (2011)
by: Sulaeman, Erwin
Published: (2011)
Control of suddenly expanded flows with micro-jets
by: Khan, Sher Afghan, et al.
Published: (2003)
by: Khan, Sher Afghan, et al.
Published: (2003)
Active control of base pressure in supersonic regime
by: Khan, Sher Afghan, et al.
Published: (2006)
by: Khan, Sher Afghan, et al.
Published: (2006)
Effect of mach number on wall pressure flow field for area ratio 2.56
by: Ashfaq, Syed, et al.
Published: (2014)
by: Ashfaq, Syed, et al.
Published: (2014)
Effect of mach number on stiffness and damping derivatives for oscillating hyersonic non-planar wedge
by: Crasta, Asha, et al.
Published: (2014)
by: Crasta, Asha, et al.
Published: (2014)
Supersonic similitude for oscillating non-planar wedge
by: Crasta, Asha, et al.
Published: (2014)
by: Crasta, Asha, et al.
Published: (2014)
Studies on wall pressure flow control by micro jets for high area ratio
by: Ashfaq, Syed, et al.
Published: (2014)
by: Ashfaq, Syed, et al.
Published: (2014)
Effect of aspect ratio with roll moment derivative of a delta wing in supersonic flow
by: Crasta, Asha, et al.
Published: (2016)
by: Crasta, Asha, et al.
Published: (2016)
Optimization of area ratio and thrust in suddenly expanded flow at supersonic Mach numbers
by: Pathan, Khizer Ahmed, et al.
Published: (2018)
by: Pathan, Khizer Ahmed, et al.
Published: (2018)
Investigation of base pressure variations in internal and
external suddenly expanded flows using CFD analysis
by: Pathan, Khizer Ahmed, et al.
Published: (2019)
by: Pathan, Khizer Ahmed, et al.
Published: (2019)
Prediction of base pressure in a suddenly expanded flow
the processes at supersonic Mach Number Regimes using ANN
and CFD
by: Quadros, Jaimon Dennis, et al.
Published: (2020)
by: Quadros, Jaimon Dennis, et al.
Published: (2020)
Morphing Wing I - finite element modelling of a NiTi SMA wire
by: Wan A Hamid, Wan Luqman Hakim, et al.
Published: (2017)
by: Wan A Hamid, Wan Luqman Hakim, et al.
Published: (2017)
Studies on flow from convergent nozzle with sudden expansion and control effectiveness under the influence of micro jets
by: Ashfaq, Syed, et al.
Published: (2013)
by: Ashfaq, Syed, et al.
Published: (2013)
Effects of micro jets on the flow field of the duct with sudden expansion
by: Akhtar, Mohammad Nishat, et al.
Published: (2019)
by: Akhtar, Mohammad Nishat, et al.
Published: (2019)
Control of base pressure with micro jets for area ratio 2.4
by: Ashfaq, Syed, et al.
Published: (2014)
by: Ashfaq, Syed, et al.
Published: (2014)
Control of base flows with micro jets
by: Ahmed Ali Baig, Maughal, et al.
Published: (2011)
by: Ahmed Ali Baig, Maughal, et al.
Published: (2011)
Structural analysis of vee-cap sheet metal component
by: Afzal, Asif, et al.
Published: (2016)
by: Afzal, Asif, et al.
Published: (2016)
Experimental research of wall pressure distribution and effect of micro jet at Mach 1.5
by: Azami, Muhammad Hanafi, et al.
Published: (2019)
by: Azami, Muhammad Hanafi, et al.
Published: (2019)
Similar Items
-
Modeling and analysis of convergent divergent nozzle with
sudden expansion duct using finite element method
by: Aabid, Abdul, et al.
Published: (2019) -
Experimental investigation of flow through convergent nozzle and the influence of micro jets on the enlarged duct flow field
by: Ashfaq, Syed, et al.
Published: (2014) -
CFD analysis of the supersonic nozzle flow with sudden expansion
by: Ahmed, Khizar Pathan, et al.
Published: (2016) -
Control of suddenly expanded flow from correctly expanded nozzles
by: Khan, Sher Afghan, et al.
Published: (2004) -
Active control of suddenly expanded flow from under expanded nozzles
by: Khan, Sher Afghan, et al.
Published: (2004)