ONERA 468 CRM: CFD wall wall fields about the Common Reserch Model (WBPN) for 468 flow conditions

The database contains the wall distributions of 468 Reynolds-Averaged Navier–Stokes simulations using the Spalart–Allmaras turbulence model, performed on the NASA/Boeing Common Research Model wing-body-pylon-nacelle configuration. The database spans a wide range of flow conditions, varying Mach number (including transonic regimes), angle of attack (capturing flow separation), and Reynolds number (based on three stagnation pressures, with one setting matching wind tunnel experiments). The numerical quality of the database is assessed, through checking the convergence level of each computation.