Airbus A320 CFD

grabcad

Conducting CFD analysis on an Airbus A320 using OpenFOAM software, with a 3D STL model not created by me. In the analysis, initial velocity (U0) is set at 233 m/s and the time duration (T) is 1000 seconds, with a time step (deltaT) of 1 second. The pressure maximum was measured at 22,472.1 pa at the nose/nase part of the aircraft, while the wing/tragfläche recorded 5,718.69 pa after 7 seconds. The entire analysis took approximately 4.5 hours on 8 CPUs, with a mesh consisting of 4,893,137 points, 13,107,305 faces, 12,497,954 internal faces and 4,142,499 cells with an average of 6.18111 faces per cell.