Mesh boundary layers for a pipe geometry

Mesh boundary layers for a pipe geometry

PDF) Boundary Layer Adaptivity for Transonic Turbulent Flows

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

Kedar CHITALE, Principal CFD Engineer, PhD

Axial and radial turbulent intensity components at 0.6 cm above the

Iso-surface of Mach 1 for initial and adapted meshes

Axial and radial turbulent intensity components on the axis for Case B

Saurabh Tendulkar's research works

Mesh boundary layers for a pipe geometry