Axisymmetric Blunt Cone Entry Probe:Experimental Campaign and Numerical Rebuilding:
MISTRAL validation paper:
Modeling sensitivity analysis for TC3 on the orbiter aero-thermal properties:
X-38 Experimental and CFD Analysis in Subsonic Flight Regime:
Entry Probe Stability Analysis for the Mars Pathfinder and Mars Premier Orbiter :
Comparative Study of CFD codes MISTRAL and OpenFOAM - Application to Fluid Structure Interaction: