| Literature DB >> 35718797 |
Umar Nazir1, Muhammad Sohail2, Poom Kumam3,4, Kanokwan Sitthithakerngkiet5, Abd Allah A Mousa6, Muhammad Jahangir Khan7, Ahmed M Galal8,9.
Abstract
The dynamic of fluids and coolants in automobiles are achieved by enhancement in heat energy using ternary hybrid nanostructures. Ternary hybrid nanomaterial is obtained by suspension of three types of nanofluid (aluminum oxide, silicon dioxide and titanium dioxide) in base fluid (EG). Prime investigation is to address comparison study in thermal energy involving various flow models termed as Maxwell fluid and Williamson fluid. This exploration is carried out by partially ionized fluidic particles in the presence of ternary hybrid nanomaterial over cone. Heat transfer is carried out by heat source and thermal radiation. Equations regarding Ordinary differential are achieved from PDEs using variable transformations. The numerical consequences are obtained implementing finite element method. Flow into fluid particles is enhanced versus higher values of Hall and ion slip parameters. Thermal performance as well as flow performance for the case Williamson fluid is better than for case of Maxwell fluid. Production via energy is boosted versus heat source parameter.Entities:
Year: 2022 PMID: 35718797 PMCID: PMC9207031 DOI: 10.1038/s41598-022-14312-9
Source DB: PubMed Journal: Sci Rep ISSN: 2045-2322 Impact factor: 4.996
Figure 1Geometry of developed analysis.
Nanoaprticles properties in term of thermal in EG[13].
| 32.9 | 6310 | ||
| 1.4013 | 2270 | ||
| 8.953 | 4250 | ||
| EG | 0.144 | 884 |
Figure 2FEM related steps.
Simulations of and in term of mesh free study.
| Number of elements | |||
|---|---|---|---|
| 30 | 0.7034699538 | 0.0001271156631 | 0.6643453360 |
| 60 | 0.6654719170 | 0.6476105404 | 0.0001681814168 |
| 90 | 0.6528811600 | 0.6419911471 | 0.0001753839054 |
| 120 | 0.6466025942 | 0.6391737776 | 0.0001776462284 |
| 150 | 0.6428421432 | 0.6374817686 | 0.0001785704232 |
| 180 | 0.6403366926 | 0.6363523416 | 0.0001790046029 |
| 210 | 0.6385486335 | 0.6355451067 | 0.0001792273544 |
| 240 | 0.6372087906 | 0.6349398323 | 0.0001793468912 |
| 270 | 0.6344678686 | 0.6344678686 | 0.0001794104423 |
| 300 | 0.6353326192 | 0.6340911021 | 0.0001794425719 |
Validation of numerical simulations in term of skin friction coefficients and heat transfer rate with published work[19] when and
| Malik et al.[ | Present simulations | |||||
|---|---|---|---|---|---|---|
| 0.0 | 1.0253 | 0.6153 | 0.4295 | 1.0251320192 | 0.61529943250 | 0.4294719073 |
| 1.0 | 2.2007 | 0.8492 | 0.6121 | 2.2007397320 | 0.84977941223 | 0.6126020922 |
| 10 | 8.5041 | 1.3990 | 1.0097 | 8.5046102402 | 1.3995234132 | 1.0097023340 |
Figure 3Influence of versus secondary velocity filed.
Figure 4Influence of versus primary velocity filed.
Figure 5Influence of versus primary velocity filed.
Figure 6Influence of versus secondary velocity filed.
Figure 7Influence of versus primary velocity filed.
Figure 8Influence of versus secondary velocity filed.
Figure 9Influence of versus temperature filed.
Figure 10Influence of versus temperature filed.
Figure 11Comparison heat energy performance for tri-hybrid nanoparticles, nanofluid and fluid and hybrid nanoparticles.
Numerical effects of flow rates and Nusselt number versus and
| Change in parameters | ||||
|---|---|---|---|---|
| 0.0 | 0.5553479204 | 1.748606357 | 0.7829787333 | |
| 0.4 | 0.5753441468 | 1.778320364 | 0.7530277233 | |
| 0.8 | 0.5852129658 | 1.796435697 | 0.7251228524 | |
| 0.0 | 0.5553079541 | 1.680368431 | 0.7799653389 | |
| 0.2 | 0.5350949743 | 1.502998494 | 0.7827366919 | |
| 0.4 | 0.5250832751 | 1.409744755 | 0.7920984199 | |
| 0.0 | 0.5551030346 | 1.727216716 | 0.7784422264 | |
| 0.8 | 0.5351498653 | 1.716458189 | 0.7866359920 | |
| 1.4 | 0.5151749487 | 1.709309779 | 0.7959683439 | |
| -1.3 | 0.5162153062 | 1.652216728 | 0.3736565052 | |
| 0.4 | 0.4313655409 | 1.611410548 | 0.248580176 | |
| 1.5 | 0.4146696632 | 1.592119492 | 0.083446514 |
Comparative numerical performance among Williamson fluid and Maxwell fluid versus impacts of magnetic parameter and Prandtl number.
| Maxwell fluid | Williamson fluid | ||
|---|---|---|---|
| 0.0 | 0.7829754254 | 1.498735588 | |
| 0.4 | 0.7837240327 | 1.619323451 | |
| 0.8 | 0.7861334864 | 1.739324158 | |
| 206 | 0.3562296680 | 1.389662075 | |
| 208 | 0.4278509806 | 1.389671389 | |
| 210 | 0.9917767611 | 1.389693808 |