The software OPTIMENGA_AERO_WB is intended for optimizing the shape of aerodynamic wings in presence of fuselage. The optimization is for minimum drag in specified design conditions subject to prescribed constraints. The code can be also used for analyzing the flow about wing-fuselage combinations.

The system operates in fully automated regime without need for user intervention.

The optimization target is the total wing drag at fixed aerodynamic design conditions (lift coefficient, free stream Mach and Reynolds numbers).

OPTIMENGA_AERO_WB also performs multipoint optimization which minimizes a weighted combination of drag values at specified design points (e.g. at cruise and take-off conditions).