Goal-Oriented anisotropic mesh adaptation for unsteady Euler flows
- 2D Blast into a city
- 3D Blast into a city
- Travelling of an acoustic wave in a rectangular domain (2D)
- Difraction of an acoutic wave (2D)
- Travelling of an acoustic wave in a 3D domain with an antinoise barrier
Goal-Oriented anisotropic mesh adaptation for unsteady Navier-Stokes flows
Laminar flow over a Naca airfoil at Mach 0.1, Angle of Attack 30 and Rey=1000