Mesh boundary layers for a pipe geometry

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

Normalized bottom wall pressure for the Delery bump

Radial turbulent intensity components in the impinging jet of Cooper et

PDF) Boundary Layer Adaptivity for Transonic Turbulent Flows

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

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

Saurabh Tendulkar's research works

Axial and radial turbulent intensity components at 0.6 cm above the

Kedar CHITALE, Principal CFD Engineer, PhD

initial and adapted meshes for the Delery bump

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

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