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Mesh boundary layers for a pipe geometry

$ 33.00

4.8 (187) In stock

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

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

Axial and radial turbulent intensity components at 0.6 cm above the

Saurabh Tendulkar's research works

Axial turbulent intensity components in the impinging jet of Cooper et

Axial turbulent intensity components in the impinging jet of Cooper et

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

PDF) Boundary Layer Adaptivity for Transonic Turbulent Flows

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

Mach number slice and contours for the Delery bump

Iso-surface of Mach 1 for initial and adapted meshes

Mesh boundary layers for a pipe geometry

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