Numerical high lift prediction on the JAXA standard model

A growing interest in the prediction of highlift aerodynamics has grown in recent years,motivated by the AIAA High Lift PredictionWorkshop (HiLiftPW) series, which publicly re-lease standard wing-fuselage geometries with ex-perimental results from wind tunnel tests andpromote dissemination of meshing strategies,physics modelling, and statistical analyses on theresults provided by participants. The object ofthis work is the JAXA standard model proposedin the3rdAIAA HiLiftPW. The authors want topropose best practices for numerical meshing andanalysis with the lowest possible number of cells,giving indications on physics modelling and onthe location of grid refinements for mesh tuning.