FSI applications

Reverse thrust

Aeroelasticity (3D wing)

Mesh adaptation applications

Sonic bang reduction

Falcon subsonic calculation

Optimal design calculation

2D case

Multiobjectives optimisation : reduce drag while presering lift Final Cd=0.005 Vs initial Cd=0.009

Available tools
  • Gradient based algorithms
  • Genetic algorithms
  • AD method

3D case

Overpressure considerably reduced by shape optimisation