Lab Migration Solution Proposal

Dr Tushar Chourushi
COMPUTATION (CFD) LABORATORY
Capture the velocity profile and boundary layer for a Steady incompressible flow through 2D & 3D channel
Capture the bow shock profile for a steady supersonic flow over a blunt body
Capture the system of oblique shock waves for steady Supersonic flow over a spiked body
Capture the von-Karmon vortex streak for incompressible viscous flow over a circular cylinder
Analyze the adiabatic flow through the convergent-divergent nozzle.