CFD++ Applications to Full Commercial Airplanes Some of our customers are using CFD++ to compute the flowfield around full commercial airplane geometries: Geometries include Flaps and slats deployed Wings include Winglets (more vortex shedding) • Full Tail Configuration With engine power turned on Prism + Tetrahedral Meshes with 55 million points CFD++ takes 300 iterations to converge (5 orders of residual magnitute) Use over 80 cpu's with less then 7 hours wall clock time for convergence Using K-Epsilon-Rt turbulence model developed by Metacomp Results match wind tunnel data very well CFD++ used with confidence, Launch Once/Compute Once