CFD simulation with analytical and theoretical validation of different flow parameters for the wedge at supersonic Mach number
In this paper, analytical and numerical methods are used to evaluate flow over a wedge at supersonic Mach numbers. Closed form solutions are obtained for the various semi-vertex angle of the wedge and the Mach numbers. Supersonic similarity parameter has been used to obtain the pressure distribution...
| Main Authors: | Khan, Sher Afghan, Aabid, Abdul, Saleel, Ahamad C. |
|---|---|
| Format: | Article |
| Language: | English English |
| Published: |
International Journals of Engineering & Sciences
2019
|
| Subjects: | |
| Online Access: | http://irep.iium.edu.my/71239/ http://irep.iium.edu.my/71239/1/71239_CFD%20Simulation%20with%20Analytical%20and%20Theoretical.pdf http://irep.iium.edu.my/71239/7/71239_CFD%20simulation%20with%20analytical%20and%20theoretical_SCOPUS.pdf |
Similar Items
Optimization of two-dimensional wedge flow field at
supersonic Mach number
by: Khan, Sher Afghan, et al.
Published: (2019)
by: Khan, Sher Afghan, 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)
Determination of wall pressure flows at supersonic Mach numbers
by: Aabid, Abdul, et al.
Published: (2020)
by: Aabid, Abdul, et al.
Published: (2020)
Estimation of stability derivatives of a wedges at supersonic Mach numbers
by: Shanbhag, Pavithra, et al.
Published: (2017)
by: Shanbhag, Pavithra, et al.
Published: (2017)
Control of suddenly expanded flow at low supersonic Mach
numbers
by: Chaudhury, Zakir Ilahi, et al.
Published: (2015)
by: Chaudhury, Zakir Ilahi, et al.
Published: (2015)
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)
Prediction of base pressure in a suddenly expanded flow process 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)
Study of effect of flow parameters on base pressure in a
suddenly expanded duct at supersonic mach number regimes using CFD and design of experiments
by: Quadros, Jaimon Dennis, et al.
Published: (2018)
by: Quadros, Jaimon Dennis, et al.
Published: (2018)
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)
Active control of wall pressure flow field at low supersonic Mach numbers
by: Asad Ullah, Mohammed, et al.
Published: (2016)
by: Asad Ullah, Mohammed, et al.
Published: (2016)
Analysis of variation of stiffness derivative with Mach number and angle of attack for a supersonic flow
by: Crasta, Asha, et al.
Published: (2016)
by: Crasta, Asha, et al.
Published: (2016)
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)
Experimental and numerical investigation of suddenly expanded flow field for supersonic Mach numbers with and without annular cavities
by: Quadros, Jaimon Dennis, et al.
Published: (2020)
by: Quadros, Jaimon Dennis, et al.
Published: (2020)
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)
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)
High incidence supersonic similitude for planar wedge
by: Crasta, Asha, et al.
Published: (2012)
by: Crasta, Asha, et al.
Published: (2012)
Supersonic similitude for oscillating non-planar wedge
by: Crasta, Asha, et al.
Published: (2014)
by: Crasta, Asha, et al.
Published: (2014)
Predictive modeling of suddenly expanded flow process in the Supersonic Mach number regime using response surface methodology
by: Quadros, Jaimon Dennis, et al.
Published: (2017)
by: Quadros, Jaimon Dennis, et al.
Published: (2017)
Experimental investigations on wall pressure in suddenly enlarged ducts at supersonic Mach number regimes
by: Baig, Maugal Ahmed Ali, et al.
Published: (2012)
by: Baig, Maugal Ahmed Ali, et al.
Published: (2012)
Estimation of stability derivatives in pitch for an oscillating 2-D wedge in supersonic Flow
by: Pavithra, Shanbhag,, et al.
Published: (2016)
by: Pavithra, Shanbhag,, et al.
Published: (2016)
Experimental investigation on the effectiveness of active control mechanism on base pressure at low supersonic mach numbers
by: Chaudhary, Zakir Ilahi, et al.
Published: (2017)
by: Chaudhary, Zakir Ilahi, et al.
Published: (2017)
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)
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)
by: Pathan, Khizer Ahmed, et al.
Published: (2017)
Control of suddenly expanded flows from correctly expanded and under expanded nozzles at supersonic mach number for area ratio 2.56
by: Bashir, Musavir, et al.
Published: (2016)
by: Bashir, Musavir, et al.
Published: (2016)
Study of base pressure behavior in a suddenly expanded duct at supersonic mach number regimes using statistical analysis
by: Quadros, Jaimon Dennis, et al.
Published: (2018)
by: Quadros, Jaimon Dennis, et al.
Published: (2018)
Base pressure behaviour in a suddenly expanded duct at supersonic mach number regimes using Taguchi design of experiments
by: Quadros, Jaimon Dennis, et al.
Published: (2018)
by: Quadros, Jaimon Dennis, et al.
Published: (2018)
Active control of flow through the nozzles at sonic Mach number
by: Ashfaq, Syed, et al.
Published: (2013)
by: Ashfaq, Syed, et al.
Published: (2013)
Investigation of the effects of nozzle exit mach number and nozzle pressure ratio on axisymmetric flow through suddenly expanded nozzles
by: Khan, Sher Afghan, et al.
Published: (2019)
by: Khan, Sher Afghan, et al.
Published: (2019)
Modelling of suddenly expanded flow process in supersonic Mach regime using design of experiments and response surface methodology
by: Quadros, Jaimon Dennis, et al.
Published: (2018)
by: Quadros, Jaimon Dennis, et al.
Published: (2018)
Analytical estimation of stability derivatives of wing with curved leading edges at hypersonic mach number
by: Renita, sharon Monis, et al.
Published: (2020)
by: Renita, sharon Monis, et al.
Published: (2020)
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 in a suddenly expanded flow for area ratio 4.84
by: Baig, Maugal Ahmed Ali, et al.
Published: (2012)
by: Baig, Maugal Ahmed Ali, et al.
Published: (2012)
Effect of micro jet control on the flow filed of the duct at Mach 1.5
by: Khan, Sher Afghan, et al.
Published: (2019)
by: Khan, Sher Afghan, et al.
Published: (2019)
Experiment on of nozzle flow with sudden expansion at Mach 1.1
by: Faheem, Mohammad, et al.
Published: (2019)
by: Faheem, Mohammad, et al.
Published: (2019)
Investigation of effect of process parameters on suddenly expanded flows through an axi-symmetric nozzle for different Mach numbers using design of experiments
by: Quadros, Jaimon Dennis, et al.
Published: (2017)
by: Quadros, Jaimon Dennis, et al.
Published: (2017)
Cfd Simulation To Study The Effects Of Ribs In A Converging Nozzle Flow At Sonic Mach Number
by: Khan, Ambareen
Published: (2020)
by: Khan, Ambareen
Published: (2020)
Control of CD nozzle flow using microjets at Mach 2.1
by: Akhtar, Mohammad Nishat, et al.
Published: (2019)
by: Akhtar, Mohammad Nishat, et al.
Published: (2019)
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)
Experimental research on wall pressure distribution in C-D nozzle at Mach number 1.1 for area ratio 3.24
by: Khan, Sher Afghan, et al.
Published: (2019)
by: Khan, Sher Afghan, et al.
Published: (2019)
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)
Similar Items
-
Optimization of two-dimensional wedge flow field at
supersonic Mach number
by: Khan, Sher Afghan, 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) -
Determination of wall pressure flows at supersonic Mach numbers
by: Aabid, Abdul, et al.
Published: (2020) -
Estimation of stability derivatives of a wedges at supersonic Mach numbers
by: Shanbhag, Pavithra, et al.
Published: (2017) -
Control of suddenly expanded flow at low supersonic Mach
numbers
by: Chaudhury, Zakir Ilahi, et al.
Published: (2015)