| Literature DB >> 34432830 |
Umar Nazir1, Muhammad Sohail1, Hussam Alrabaiah2,3, Mahmoud M Selim4,5, Phatiphat Thounthong6, Choonkil Park7.
Abstract
This report is prepared to examine the heat transport in stagnation point mixed convective hyperbolic tangent material flow past over a linear heated stretching sheet in the presence of magnetic dipole. Phenomenon of thermal transmission plays a vital role in several industrial manufacturing processes. Heat generation is along with thermal relaxation due to Cattaneo-Christov flux is engaged while modeling the energy equation. In order to improve the thermal performance, inclusion of hybrid nanoparticles is mixed in hyperbolic tangent liquid. The conservation laws are modeled in Cartesian coordinate system and simplified via boundary layer approximation. The modeled partial differential equations (PDEs) system are converted into ordinary differential equations (ODEs) system by engaging the scaling group transformation. The converted system of modeled equations has been tackled via finite element procedure (FEP). The efficiency of used scheme has been presented by establishing the grid independent survey. Moreover, accurateness of results is shown with the help of comparative study. It is worth mentioning that the inclusion of hybrid nanoparticles has significant higher impact on heat conduction as compared with nanoparticle. Moreover, hybrid nanoparticles are more efficient to conduct maximum production of heat energy as compared with the production of heat energy of nanoparticles. Hence, hybrid nanoparticles (MoS2/Ag) are observed more significant to conduct more heat energy rather than nanoparticle (Ag).Entities:
Mesh:
Year: 2021 PMID: 34432830 PMCID: PMC8386857 DOI: 10.1371/journal.pone.0256302
Source DB: PubMed Journal: PLoS One ISSN: 1932-6203 Impact factor: 3.240
Fig 1Manufacturing approach of hybrid nanoparticles and nanoparticles.
Fig 2Geometrical view of flow model.
Properties related to thermal of nanoparticles and hybrid nanoparticles in EG.
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Convergence analysis of velocities and thermal energy considering 300 elements.
| Number of elements |
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|---|---|---|---|
| 30 | 0.4853074 | 0.5326158 | 0.5946054 |
| 60 | 0.4568591 | 0.5163933 | 0.5772373 |
| 90 | 0.4476232 | 0.5110348 | 0.5716849 |
| 120 | 0.4429796 | 0.5082616 | 0.5687690 |
| 150 | 0.4402813 | 0.5066645 | 0.5668638 |
| 180 | 0.4384072 | 0.5055560 | 0.5660132 |
| 210 | 0.4371181 | 0.5047064 | 0.5644715 |
| 240 | 0.4361482 | 0.5041676 | 0.5641853 |
| 270 | 0.4353591 | 0.5036810 | 0.5637239 |
| 300 | 0.4347759 | 0.5033553 | 0.5634322 |
Comparison of simulations in view of Nusselt number when ϕ1 =0, ϕ2 = 0, A = 3.0, β = 1.
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| Iqbal et al. [ | Present results |
|---|---|---|
| 0.07 | 0.33814 | 0.3387103 |
| 0.5 | 0.82748 | 0.8273089 |
| 2.0 | 1.52147 | 1.5239940 |
| 6.8 | 2.59780 | 2.5971029 |
| 10.0 | 3.07902 | 3.0698597 |
Fig 3Distribution of velocity versus we.
Fig 10Distribution of temperature versus Ω.
Fig 4Distribution of velocity versus m.
Fig 5Distribution of velocity versus λ1.
Fig 7Distribution of velocity versus λ1.
Fig 6Distribution of velocity versus H.
Fig 8Distribution of temperature versus λ1.
Fig 9Distribution of temperature versus H.
Comparative simulations of gradient temperature and skin friction coefficient considering nanoparticles and hybrid nanoparticles versus the change in We, λ1, H and Ω.
| Nanoparticles | Hybrid nanoparticles | ||||
|---|---|---|---|---|---|
| −( | −( | −( | −( | ||
| 0.0 | 0.40101802 | 0.31201902 | 1.01219001 | 2.13201732 | |
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| 0.2 | 0.36352971 | 0.44888821 | 1.20065603 | 2.55502285 |
| 0.7 | 0.22859163 | 0.41301203 | 1.335083774 | 2.31001730 | |
| 0.7 | 0.417202388 | 0.34110303 | 1.413212063 | 2.23210163 | |
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| -1.3 | 0.3082075083 | 0.44888821 | 1.510071963 | 3.55502285 |
| 0.3 | 0.2082084230 | 0.53410120 | 1.310072391 | 3.73210132 | |
| 1.2 | 0.1082089891 | 0.61004305 | 1.210072658 | 3.91213031 | |
|
| -1.2 | 0.5082209234 | 0.77329020 | 2.710090674 | 3.27237837 |
| 0.5 | 0.2101789003 | 0.401603593 | 2.231073203 | 3.008146408 | |
| 0.0 | 0.0083779234 | 1.3123635 | 0.010284611 | 3.3180474 | |
| Ω | 0.5 | 0.0083779234 | 1.5012340 | 0.010284611 | 3.4231303 |
| 1.5 | 0.0083779234 | 1.7092120 | 0.010284611 | 3.7121313 | |