Mesh boundary layers for a pipe geometry

initial and adapted meshes for the Delery bump

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

Mesh boundary layers for a pipe geometry

Saurabh Tendulkar's research works

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

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

PDF) Boundary Layer Adaptivity for Transonic Turbulent Flows

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

PDF) Boundary Layer Adaptivity for Transonic Turbulent Flows

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

Kedar CHITALE, Principal CFD Engineer, PhD

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