| Literature DB >> 25785857 |
Junaid Ahmad Khan1, M Mustafa2, T Hayat3, M Sheikholeslami4, A Alsaedi5.
Abstract
This work deals with the three-dimensional flow of nanofluid over a bi-directional exponentially stretching sheet. The effects of Brownian motion and thermophoretic diffusion of nanoparticles are considered in the mathematical model. The temperature and nanoparticle volume fraction at the sheet are also distributed exponentially. Local similarity solutions are obtained by an implicit finite difference scheme known as Keller-box method. The results are compared with the existing studies in some limiting cases and found in good agreement. The results reveal the existence of interesting Sparrow-Gregg-type hills for temperature distribution corresponding to some range of parametric values.Entities:
Mesh:
Year: 2015 PMID: 25785857 PMCID: PMC4364987 DOI: 10.1371/journal.pone.0116603
Source DB: PubMed Journal: PLoS One ISSN: 1932-6203 Impact factor: 3.240
Fig 1Physical configuration and coordinate system.
List of symbols.
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| ’ 1st order derivative with respect to η |
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| Pr Prandtl number |
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| Re local Reynolds number |
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Comparison of values of wall temperature gradient (0)with previous studies for the case of regular fluid Nb = Nt = 10 when λ = 0.
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| Magyari and Keller [ | Liu et al. [ | Present (Keller-Box) | ||
| 1 | -1.5 | 0.377413 | 0.37741256 | 0.377393 |
| 0 | -0.549643 | -0.54964375 | -0.549641 | |
| 1 | -0.954782 | -0.95478270 | -0.954763 | |
| 3 | -1.560294 | -1.56029540 | -1.560175 | |
| 5 | -1.5 | 1.353240 | 1.35324050 | 1.353250 |
| 0 | -1.521243 | -1.52123900 | -1.521662 | |
| 1 | -2.500135 | -2.50013157 | -2.500653 | |
| 3 | -3.886555 | -3.88655510 | -3.886678 | |
| 10 | -1.5 | 2.200000 | 2.20002816 | 2.200456 |
| 0 | -2.257429 | -2.25742372 | -2.259142 | |
| 1 | -3.660379 | -3.66037218 | -3.662782 | |
| 3 | -5.635369 | -5.62819631 | -5.630445 | |
Numerical values of wall temperature gradient θ’ (0)in the case of regular fluid (Nb = Nt = 10-5). Paranthesis show the corresponding results of Liu et al. [23].
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| 0.0 | 0.7 | 0.6235675 | -0.42582871 | -1.641474 |
| (0.62361839) | (-0.42583804) | (-1.64165922) | ||
| 7 | 5.9319133 | -1.8474565 | -5.8975891 | |
| (5.94094442) | (-1.84660569) | (-5.89780378) | ||
| 0.5 | 0.7 | 0.76367407 | -0.52152683 | -2.0102735 |
| (0.76378454) | (-0.52154103) | (-2.01061361) | ||
| 7 | 7.2596204 | -2.2631841 | -7.2229124 | |
| (7.27614126) | (-2.26162085) | (-7.22330493) | ||
| 1.0 | 0.7 | 0.88177213 | -0.6022019 | -2.3211331 |
| (0.88194314) | (-0.60222359) | (-2.32165661) | ||
| 7 | 8.3764364 | -2.6139021 | -8.3401528 | |
| (8.40176423) | (-2.61149481) | (-8.34075409) | ||
Fig 2Variation in the velocity fields with λ.
Fig 3Variations in wall shear stresses and entrainment velocity with λ.
Fig 4Effect of Nb and Nt on θ.
Fig 5Effect of Pr and Sc on θ.
Fig 6Effect of A and λ on θ.
Fig 7Effect of Nb and Nt on ϕ.
Fig 8Effect of A and λ on ϕ.
Fig 9Effect of Pr and Sc on ϕ.
Fig 10Effect of λ, Nb and Nt on Nur.
Fig 11Effect of λ, Pr and Sc on Nur.
Fig 12Effect of A, Nb and Nt on Nur.
Fig 13Effect of A, Pr and Sc on Nur.
Fig 14Effect of A, Nb and Nt on Shr.
Fig 15Effect of A, Pr and Sc on Shr.