Potential Flow Over an Airfoil
Potential Flow Over an Airfoil
This example models and simulates the flow field around the cross section of a NACA airfoil using the inviscid potential equation. The potential field is here modeled with the classic Laplace PDE equation with a correction for the discontinuity at the trailing edge (the Kutta condition). On the boundaries, there is …
Supersonic Flow Over an Obstacle
Supersonic Flow Over an Obstacle
Steady inviscid flow over a cylindrical bump using the compressible Euler equations. The flow at the inlet is supersonic with Ma = 1.4 resulting in a series of reflected shock waves as the flow hits the obstacle [1]. This model is available as an automated tutorial by selecting Model Examples and Tutorials… > …