Mesh boundary layers for a pipe geometry
![](https://www.researchgate.net/publication/269047838/figure/fig1/AS:447379984916480@1483675108191/Mesh-boundary-layers-for-a-pipe-geometry.png)
![](https://www.researchgate.net/profile/Kedar-Chitale-2/publication/269047838/figure/fig2/AS:447379984916481@1483675108230/Types-of-boundary-layer-profiles_Q320.jpg)
Mesh boundary layers for a pipe geometry
![](https://www.researchgate.net/publication/269047838/figure/fig11/AS:447379989110797@1483675109523/Iso-surface-of-Mach-1-for-initial-and-adapted-meshes.png)
Iso-surface of Mach 1 for initial and adapted meshes
![](https://i1.rgstatic.net/ii/profile.image/796865025019905-1566998835791_Q64/Elie-Hachem-2.jpg)
PDF) Boundary Layer Adaptivity for Transonic Turbulent Flows
![](https://www.researchgate.net/profile/Manmatha-Roul/publication/277015474/figure/fig1/AS:669481462407173@1536628227302/Pc-versus-V-2-2-data-for-water-in-oil-emulsions-flowing-through-a-sudden-contraction_Q320.jpg)
Top) Subgrid arrangement within the near-wall main-grid control
![](https://i1.rgstatic.net/ii/profile.image/276581894377473-1442953670218_Q512/Kenneth-Jansen.jpg)
Kenneth JANSEN, Professor (Full), Doctor of Engineering, University of Colorado Boulder, CO, CUB, Department of Aerospace Engineering Sciences (AES)
![](https://www.researchgate.net/profile/Kedar-Chitale-2/publication/269047838/figure/fig4/AS:447379984916483@1483675108482/a-shows-zooms-of-the-initial-and-the-adapted-meshes-over-the-bump-The-boundary-layer_Q320.jpg)
a) shows zooms of the initial and the adapted meshes over the bump. The
![](https://www.researchgate.net/profile/Michel-Rasquin/publication/260428194/figure/fig3/AS:297148596932609@1447857154194/figure-fig3_Q320.jpg)
Kedar CHITALE, Principal CFD Engineer, PhD
show results for the countercurrent jets in Mounaim-Rousselle et al.
![](https://www.researchgate.net/profile/Kwang-Yong-Kim/publication/245356298/figure/fig8/AS:668849858957312@1536477641078/Comparison-of-the-terms-for-uu-at-rODAe0-in-the-impinging-jet-of-Cooper-et-al-12-a_Q320.jpg)
Nusselt number predictions for the impinging jet ðH=D ¼ 4; Re ¼ 70;