Mesh boundary layers for a pipe geometry

Axial and radial turbulent intensity components at 0.6 cm above the

PDF) Boundary Layer Adaptivity for Transonic Turbulent Flows

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

Types of boundary layer profiles

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

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

Iso-surface of Mach 1 for initial and adapted meshes

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

PDF) Boundary Layer Adaptivity for Transonic Turbulent Flows

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

Saurabh Tendulkar's research works

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