Mesh boundary layers for a pipe geometry

Iso-surface of Mach 1 for initial and adapted meshes

Saurabh Tendulkar's research works

Mesh boundary layers for a pipe geometry

Axial and radial turbulent intensity components at 0.6 cm above the

Effect of the first cell height on a turbulent boundary layer profile

Mark SHEPHARD, Rensselaer Polytechnic Institute, NY, RPI, Department of Mechanical, Aerospace and Nuclear Engineering

Mesh boundary layers for a pipe geometry

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

Radial turbulent intensity components in the impinging jet of Cooper et

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