Numerical investigation of mathematical non-dimensional constant representing smoothness in the Nusselt profile
Cooling of devices using air-jet and other fluid impingement has acquired pace in the manufacturing and electronic device industries. The cooling of the surface using liquid jets is studied using the Nusselt distribution profile. The pattern of the Nusselt profile becomes non-uniform when some para...
| Main Authors: | Ansari, Emad, Siddiqui, M. Umair, Khan, Sher Afghan, Akhtar, Mohammad Nishat, Ilmi, Abu Bakar |
|---|---|
| Format: | Article |
| Language: | English English |
| Published: |
Akademia Baru
2020
|
| Subjects: | |
| Online Access: | http://irep.iium.edu.my/81245/ http://irep.iium.edu.my/81245/1/CFDLV12_N6_P16_27.pdf http://irep.iium.edu.my/81245/7/81245_Numerical%20investigation%20of%20mathematical%20non-dimensional%20constant_SCOPUS.pdf |
Similar Items
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)
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)
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)
Effect of level of expansion and inertia level in a suddenly expanded flow
by: Chaudhary, Zakir Ilahi, et al.
Published: (2015)
by: Chaudhary, Zakir Ilahi, 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)
Nozzle expansion level effect on a suddenly expanded flow
by: Khan, Sher Afghan, et al.
Published: (2006)
by: Khan, Sher Afghan, et al.
Published: (2006)
Control of base pressure with micro jets:part-I
by: Rehman, Shafiqur, et al.
Published: (2008)
by: Rehman, Shafiqur, et al.
Published: (2008)
Control of suddenly expanded flow
by: Khan, Sher Afghan, et al.
Published: (2006)
by: Khan, Sher Afghan, et al.
Published: (2006)
Estimation of stability derivatives of an oscillating hypersonic delta wings with curved leading edges
by: Crasta, Asha, et al.
Published: (2012)
by: Crasta, Asha, et al.
Published: (2012)
Stabilty derivatives in the newtonian limit
by: Crasta, Asha, et al.
Published: (2013)
by: Crasta, Asha, et al.
Published: (2013)
Stability derivatives of a delta wing with straight leading edge in the Newtonian limit
by: Crasta, Asha, et al.
Published: (2013)
by: Crasta, Asha, et al.
Published: (2013)
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)
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)
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)
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)
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)
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)
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)
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)
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)
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)
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 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)
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)
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 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)
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)
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)
Comparing the effect of different turbulence models on the CFD predictions of NACA0018 airfoil aerodynamics
by: Khan, Sher Afghan, et al.
Published: (2020)
by: Khan, Sher Afghan, et al.
Published: (2020)
Combined effect of relief and level of expansion in a suddenly expanded flow
by: Syed, Syed Ashfaq, et al.
Published: (2015)
by: Syed, Syed Ashfaq, 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)
The effect of micro jets on wall pressure for sonic under expanded flow
by: Ashfaq, Syed, et al.
Published: (2014)
by: Ashfaq, Syed, et al.
Published: (2014)
Similar Items
-
Influence of low length-to-diameter ratio and nozzle pressure ratio in an abruptly expanded flow
by: Khan, Sher Afghan
Published: (2015) -
Experimental study of suddenly expanded flow from correctly expanded nozzles
by: Khan, Sher Afghan, et al.
Published: (2016) -
Effect of sudden expansion for varied area ratios at subsonic and sonic flow regimes
by: Sethuraman, Vigneshvaran, et al.
Published: (2016) -
Effect of level of expansion and inertia level in a suddenly expanded flow
by: Chaudhary, Zakir Ilahi, 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)