Comparing the effect of different turbulence models on the CFD predictions of NACA0018 airfoil aerodynamics
The analysis of aerodynamic forces on two-dimensional airfoils and flow phenomena associated with different Reynolds number has been widely investigated for aerospace vehicles and wind turbines. Various numerical methods have been used with different turbulence models, and the discrepancy in flow ph...
| Main Authors: | Khan, Sher Afghan, Bashir, Musavir, Baig, Maugal Ahmed Ali, Mehaboob Ali, Fharukh Ahmed Ghasi |
|---|---|
| Format: | Article |
| Language: | English English |
| Published: |
Penerbit Akademia Baru
2020
|
| Subjects: | |
| Online Access: | http://irep.iium.edu.my/79844/ http://irep.iium.edu.my/79844/7/79844_Comparing%20the%20effect%20of%20different%20turbulence%20models.pdf http://irep.iium.edu.my/79844/13/79844_Comparing%20the%20effect%20of%20different%20turbulence%20models_Scopus.pdf |
Similar Items
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)
Wall Pressure Measurements Beneath the Supersonic Jets in
an Abruptly Augmented Nozzle
by: Bashir, Musavir, et al.
Published: (2020)
by: Bashir, Musavir, et al.
Published: (2020)
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)
by: Khan, Sher Afghan, et al.
Published: (2018)
Active control of base pressure in suddenly expanded flow for area ratio 4.84
by: Ali Baig, Maughal Ahmed, et al.
Published: (2012)
by: Ali Baig, Maughal Ahmed, et al.
Published: (2012)
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)
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)
Influence of expansion level on base pressure and reattachment length
by: Pathan, Khizar Ahmed, et al.
Published: (2019)
by: Pathan, Khizar Ahmed, et al.
Published: (2019)
Effect of nozzle pressure ratio and control jets location to control base pressure in suddenly expanded flows
by: Pathan, Khizer Ahmed, et al.
Published: (2019)
by: Pathan, Khizer Ahmed, et al.
Published: (2019)
Enlarge duct length optimization for suddenly expanded flows
by: Pathan, Khizer Ahmed, et al.
Published: (2020)
by: Pathan, Khizer Ahmed, et al.
Published: (2020)
An investigation of effect of control jets location and blowing pressure ratio to control base pressure in suddenly expanded flows
by: Pathan, Khizar Ahmed, et al.
Published: (2020)
by: Pathan, Khizar Ahmed, et al.
Published: (2020)
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)
Analysis of parameters affecting thrust and base pressure in
suddenly expanded flow from nozzle
by: Pathan, Khizar Ahmed, et al.
Published: (2019)
by: Pathan, Khizar Ahmed, et al.
Published: (2019)
Studies on flow from converging nozzle and the effect of nozzle pressure ratio for area ratio of 6.25
by: Ashfaq, Syed, et al.
Published: (2014)
by: Ashfaq, Syed, et al.
Published: (2014)
Influence of micro jets on wall pressure for area ratio 3.24
by: Ashfaq, Syed, et al.
Published: (2014)
by: Ashfaq, Syed, et al.
Published: (2014)
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)
Experimental study of suddenly expanded flow from correctly expanded nozzles
by: Khan, Sher Afghan, et al.
Published: (2016)
by: Khan, Sher Afghan, et al.
Published: (2016)
A cost-effective data acquisition instrumentation for
measurement of base pressure and wall pressure in suddenly expanded flow through ducts
by: Sethuraman, Vigneshvaran, et al.
Published: (2019)
by: Sethuraman, Vigneshvaran, et al.
Published: (2019)
Numerical investigation of splitter plate effect on the bluff body using finite volume method
by: Afifi, Azmil, et al.
Published: (2020)
by: Afifi, Azmil, et al.
Published: (2020)
Base and wall pressure control using cavities and ribs in suddenly expanded flows -an overview
by: Sethuraman, Vigneshvaran, et al.
Published: (2020)
by: Sethuraman, Vigneshvaran, et al.
Published: (2020)
Influence of control mechanism on the flow field of duct at Mach 1.2 for area ratio 2.56
by: Khan, Sher Afghan, et al.
Published: (2019)
by: Khan, Sher Afghan, et al.
Published: (2019)
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)
Pressure and its derivative with respect to piston Mach number for an oscillating cone
by: Shabana, Ayesha, et al.
Published: (2016)
by: Shabana, Ayesha, 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)
Experimental research on flow development and control effectiveness in the duct at high speed
by: Khan, Sher Afghan, et al.
Published: (2019)
by: Khan, Sher Afghan, et al.
Published: (2019)
Investigation of base flow for an axisymmetric suddenly
expanded nozzle with micro JET
by: Chaudhary, Zakir Ilahi, et al.
Published: (2018)
by: Chaudhary, Zakir Ilahi, et al.
Published: (2018)
Role of active control in increasing base pressure at Sonic Mach Number
by: G. M, Fharukh Ahmed, et al.
Published: (2019)
by: G. M, Fharukh Ahmed, et al.
Published: (2019)
The contribution of Hassan al-Rammah to gunpowder and rocket technology
by: Ahmed Ghazal, Belal, et al.
Published: (2011)
by: Ahmed Ghazal, Belal, et al.
Published: (2011)
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)
Influence of low length-to-diameter ratio and nozzle pressure ratio in an abruptly expanded flow
by: Khan, Sher Afghan
Published: (2015)
by: Khan, Sher Afghan
Published: (2015)
Research onFlows for NACA 2412 airfoil using computational Fluid dynamics method
by: Kharulaman, Liyana, et al.
Published: (2019)
by: Kharulaman, Liyana, et al.
Published: (2019)
Effect of sudden expansion for varied area ratios at subsonic and sonic flow regimes
by: Sethuraman, Vigneshvaran, et al.
Published: (2016)
by: Sethuraman, Vigneshvaran, et al.
Published: (2016)
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)
Creating and simulating turbulence generation on NACA S1046 airfoil with CFD software
by: Erwin, Erwin, et al.
Published: (2024)
by: Erwin, Erwin, et al.
Published: (2024)
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)
ESA 342-3 - PROPULSION SYSTEMS (SISTEM DORONGAN)NOV 2008.
by: PPKA, Pusat Pengajian Kejuruteraan Aeroangkasa
Published: (2008)
by: PPKA, Pusat Pengajian Kejuruteraan Aeroangkasa
Published: (2008)
ESA 485(3) - SISTEM DORONGAN ROKET OKT-NOV 07.
by: PPKA, Pusat Pengajian Kejuruteraan Aeroangkasa
Published: (2007)
by: PPKA, Pusat Pengajian Kejuruteraan Aeroangkasa
Published: (2007)
ESA 485(3) - SISTEM DORONGAN ROKET OKT 04
by: PPKA, Pusat Pengajian Kejuruteraan Aeroangkasa
Published: (2004)
by: PPKA, Pusat Pengajian Kejuruteraan Aeroangkasa
Published: (2004)
Range Optimization Using Trajectory Shaping Analysis Of A Surface-Launched Rocket
by: Saeedipour, Hamid Reza, et al.
Published: (2004)
by: Saeedipour, Hamid Reza, et al.
Published: (2004)
Rocket Drag Prediction Method For Optimizing Design And Flight
Performance.
by: Gunsalam, Henry, et al.
Published: (2004)
by: Gunsalam, Henry, et al.
Published: (2004)
UNIVERSITI SAINS MALAYSIA Second Semester Examination
2012/2013 Academic Session June 2013 ESA 344/2 – Propulsion Systems [Sistem Dorongan] Duration: 2 hours
[Masa: 2 jam]
by: Aeroangkasa, Pusat Pengajian Kejuruteraan
Published: (2013)
by: Aeroangkasa, Pusat Pengajian Kejuruteraan
Published: (2013)
Similar Items
-
Active control of wall pressure flow field at low supersonic Mach numbers
by: Asad Ullah, Mohammed, et al.
Published: (2016) -
Wall Pressure Measurements Beneath the Supersonic Jets in
an Abruptly Augmented Nozzle
by: Bashir, Musavir, et al.
Published: (2020) -
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) -
Active control of base pressure in suddenly expanded flow for area ratio 4.84
by: Ali Baig, Maughal Ahmed, et al.
Published: (2012) -
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)