2015
DOI: 10.1016/j.expthermflusci.2015.07.017
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Impingement pressure characteristics of swirling and non-swirling turbulent jets

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Cited by 46 publications
(30 citation statements)
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“…• Axis: Symmetry axis boundary condition (with zero flux of all quantities across the symmetry boundary). • Inlet: The axial and azimuthal velocity profiles, together with their turbulence characteristics (Ahmed et al, 2015) are imposed onto the simulation as profile files (.prof) in ANSYS-FLUENT. The procedure that has been followed to input the turbulence profiles is described below.…”
Section: Formulation Of the Problemmentioning
confidence: 99%
See 1 more Smart Citation
“…• Axis: Symmetry axis boundary condition (with zero flux of all quantities across the symmetry boundary). • Inlet: The axial and azimuthal velocity profiles, together with their turbulence characteristics (Ahmed et al, 2015) are imposed onto the simulation as profile files (.prof) in ANSYS-FLUENT. The procedure that has been followed to input the turbulence profiles is described below.…”
Section: Formulation Of the Problemmentioning
confidence: 99%
“…According to Ahmed et al (2015), the turbulent characteristics of the imposed jets are not constant at the nozzle exit (inlet of the computational domain). Thus, this property must be modeled as a profile inlet condition, as done for the inlet velocity profiles.…”
Section: Formulation Of the Problemmentioning
confidence: 99%
“…To further analyze the characteristics of the swirling flow field, the swirl number (S) was obtained by the following equation (Ahmed et al, 2015):…”
Section: Velocity Distributionmentioning
confidence: 99%
“…More recently, Ahmed et al (2015) experimentally investigated the effects of swirl on the impingement surface pressure for an incompressible, turbulent, swirling impinging air jet. The effect of swirl number, nozzle-to-plate distance, and Reynolds number on the pressure distribution was examined.…”
Section: Introductionmentioning
confidence: 99%
“…For the swirling impinging jet, Bakirci et al [ 20 ] found that increasing the helical angle can increase the uniformity of radial heat transfer on the plate surface. Ahmed et al [ 21 , 22 , 23 , 24 ] studied the impingement pressure, flow, and heat transfer characteristics of swirling and non-swirling flows. The results showed that the pressure coefficient at the stagnation point is the same as that of non-swirling flow for the low-intensity swirling flow, and has a maximum value.…”
Section: Introductionmentioning
confidence: 99%