Pressure Coefficient on ONERA-M6 Wing
The airflow around ONERA-M6 is computed with OpenFoam using central upwind schemes. The LU-SGS implicit time marching yields similar results with a 30x speedup compared with rhoCentralFoam.
Wake Vortex of ONERA-M6 Wing
The wake vortex structure behind the ONERA-M6 wing.
N2A Blended Wing Body
The blended-wing body is an aircraft configuration that has the potential to be more efficient than conventional large transport aircraft configurations with the same capability.
Pressure Distribution On Surface and Section
Aerodynamical analysis has been performed for the N2A transonic BWB model using OpenFOAM.
Comparison with experimental data for ONERA-M6 wing
