Mechanical improvement in solar aircraft by using tangent hyperbolic single-phase nanofluid

Basit Öğe Kaydı
dc.authoridKaratas Akgul, Esra/0000-0003-3205-2393
dc.authoridHussain, Professor (Dr) Syed Modassir/0000-0003-1847-4776
dc.contributor.authorHussain, Syed M.
dc.contributor.authorJamshed, Wasim
dc.contributor.authorAkgul, Esra Karatas
dc.contributor.authorNasir, Nor Ain Azeany Mohd
dc.date.accessioned2024-12-24T19:29:51Z
dc.date.available2024-12-24T19:29:51Z
dc.date.issued2021
dc.departmentSiirt Üniversitesi
dc.description.abstractSolar power is the primary thermal energy source from the sunlight. This research has carried out the study of solar aircraft with solar radiation in enhancing efficiency. The thermal transfer inside the solar aircraft wings using a nanofluid past a parabolic surface trough collector (PTSC) is investigated thoroughly. The source of heat is regarded as solar radiation. For several impacts, such as porous medium, thermal radiation, and varying heat conductivity, the heat transmission performance of the wings is examined. By using the tangent hyperbolic nanofluid (THNF), the entropy analysis has been performed. The modeled momentum and energy equations are managed using the well-established numerical methodology known as the finite difference method. Two distinct kinds of nano solid-particles have been examined, such as Copper (Cu) and Zirconium dioxide (ZrO2), while Engine Oil (EO) being regarded as a based fluid. Different diagram parameters will be reviewed and revealed as figures and tables on speed, shear stress, temperature, and the surface drag coefficient and Nuselt number. It is observed that in terms of heat transfer for amplification of thermal radiation and changeable thermal conductance parameters, the performance of the aircraft wings raises. In contrast to traditional fluid, nanofluid is the best source of heat transmission. Cu-EO's thermal efficiency over ZrO2-EG falls to the minimum level of 12.6% and has reached a peak of 15.3%.
dc.description.sponsorshipDeanship of Scientific Research, Islamic University of Madinah, Ministry of Education, KSA [2/490]
dc.description.sponsorshipThe author(s) disclosed receipt of the following financial support for the research, authorship, and/or publication of this article: The author is grateful to the Deanship of Scientific Research, Islamic University of Madinah, Ministry of Education, KSA, for supporting this research work through a research project grant under Tamayuzz Program/2/490.
dc.identifier.doi10.1177/09544089211059377
dc.identifier.issn0954-4089
dc.identifier.issn2041-3009
dc.identifier.scopus2-s2.0-85122101499
dc.identifier.scopusqualityQ2
dc.identifier.urihttps://doi.org/10.1177/09544089211059377
dc.identifier.urihttps://hdl.handle.net/20.500.12604/7283
dc.identifier.wosWOS:000738064400001
dc.identifier.wosqualityQ3
dc.indekslendigikaynakWeb of Science
dc.indekslendigikaynakScopus
dc.language.isoen
dc.publisherSage Publications Ltd
dc.relation.ispartofProceedings of The Institution of Mechanical Engineers Part E-Journal of Process Mechanical Engineering
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanı
dc.rightsinfo:eu-repo/semantics/closedAccess
dc.snmzKA_20241222
dc.subjectsolar aircraft
dc.subjectparabolic trough solar collector
dc.subjectsteady tangent hyperbolic nanofluid
dc.subjectradiative heat flux
dc.subjectfinite difference method
dc.titleMechanical improvement in solar aircraft by using tangent hyperbolic single-phase nanofluid
dc.typeArticle

Dosyalar

Koleksiyon

WOS İndeksli Yayınlar Koleksiyonu
Scopus İndeksli Yayınlar Koleksiyonu