# Examples

# Last publications

### Unsteady Supersonic flow over parabolic 20% bump

Case description 20% bump in a channel inviscid flow unsteady upstream Mach number (sinusoidal oscillation (...)Crée le , Modifé le 1 September 2011

### Supersonic reflexion on 10° wedge

Case description Shock reflexion in a channel which section is reduced by a 10° wedge. The upstream flow is Mach 2. (...)Crée le , Modifé le 1 June 2010

### Shock reflection/diffraction over pyramid

Case description An unsteady shock wave (travelling Mach = 2.85) impacts a pyramid obstacle. A first reflexion (...)Crée le , Modifé le 29 August 2009

### Hypersonic flow around two cylinders

Case description inviscid flow upstream Mach number 10Numerical Parameters first order HLLC (...)Crée le , Modifé le 29 August 2009

### Multi-element inviscid flow (Suddhoo-Hall)

This inviscid flow on a multi-element airfoil is interesting since this geometry has been defined through a (...)Crée le , Modifé le 29 August 2009

### Unsteady shock Wave / boundary Layer interaction

This is an unsteady viscous computation of a shock tube problem in a closed 1x1 box. The initial conditions are set (...)Crée le , Modifé le 19 May 2009