Mesh boundary layers for a pipe geometry

Mesh boundary layers for a pipe geometry

Iso-surface of Mach 1 for initial and adapted meshes

PDF) Boundary Layer Adaptivity for Transonic Turbulent Flows

Top) Subgrid arrangement within the near-wall main-grid control

Kenneth JANSEN, Professor (Full), Doctor of Engineering, University of Colorado Boulder, CO, CUB, Department of Aerospace Engineering Sciences (AES)

a) shows zooms of the initial and the adapted meshes over the bump. The

Kedar CHITALE, Principal CFD Engineer, PhD

show results for the countercurrent jets in Mounaim-Rousselle et al.

Nusselt number predictions for the impinging jet ðH=D ¼ 4; Re ¼ 70;