Mesh boundary layers for a pipe geometry

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

PDF) Boundary Layer Adaptivity for Transonic Turbulent Flows

Mesh boundary layers for a pipe geometry

Iso-surface of Mach 1 for initial and adapted meshes

Change in the boundary layer height on upper surface of the wing

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

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

Radial turbulent intensity components in the impinging jet of Cooper et

Radial turbulent intensity components in the impinging jet of Cooper et

Saurabh Tendulkar's research works

Kedar CHITALE, Principal CFD Engineer, PhD

Axial turbulent intensity components in the impinging jet of Cooper et