Static structural Analysis
Fixed support boundary condition was applied to ribs in the fuselage where the single heaviest component, the battery, is mounted. Thrust loads are applied to the motor mounts on the front as well as on the rear. Lift load is distributed over the airfoil ribs of the wing. Landing loads are applied to the wheel mounting holes on the landing gear.
This video illustrates the transition load simulation of the airframe during mode change from vertical takeoff to forward flight. The analysis captures the variation in structural loads and stress distribution caused by combined aerodynamic forces, thrust realignment, and inertial effects during the transition phase. The simulation helps identify critical load conditions and ensures structural integrity and stability of the airframe under transitional flight regimes.