stagnation point flow of third-grade liquid due to variable thickness: a useful application to non-fourier heat flux approach

Clicks: 102
ID: 243920
2018
Article Quality & Performance Metrics
Overall Quality
Not rated
Combines reader engagement with the AI quality analysis. This article has not been analysed, so there is no overall score — reader engagement is measured and shown alongside.
AI Quality Assessment
Not analyzed
Readership in this journal
Emerging

Ranked #38 of 46 articles by views in international journal of aerospace engineering

Most read Least read

Bar heights use a square-root scale.

Mint this article as an NFT
Not yet minted

Create a permanent, verifiable on-chain record of this article on the Scimatic Network. The NFT is held in your Journament account, and you can withdraw it to your own wallet at any time.

5 SUSD one-off · no wallet required
Abstract
The impact of modified Fourier’s relation in non-linear mixed convective flow of third grade liquid is examined in this article. Stagnation point flow is considered. Variable thermal conductivity and thermal stratification are examined. Non-Fourier heat flux in heat transfer process is retained. Convergent local similar solutions for the nonlinear differential systems are achieved by homotopic procedure. Skin friction is computed and analyzed. Our computations certifies that velocity is higher when nonlinear convection and local buoyancy parameters are augmented. However temperature and thermal layer thickness are reduced for larger thermal relaxation factor. Keywords: Non-Fourier’s approach, Non-linear mixed convection, Third grade liquid, Temperature-dependent conductivity, Stagnation point flow
Reference Key
zubair2018resultsstagnation Use this key to autocite in the manuscript while using SciMatic Manuscript Manager or Thesis Manager
Authors ;M. Zubair;M. Waqas;T. Hayat;A. Alsaedi;M. Ayub
Journal international journal of aerospace engineering
Year 2018
DOI
DOI not found
URL
Keywords

Citations

No citations found. To add a citation, contact the admin at info@scimatic.org

No comments yet. Be the first to comment on this article.