Northrop Grumman Collaboration Project 25-26
Collaborated on the design and development of a trimotor Vertical Takeoff and Landing aircraft configured with two front tilt rotors and one rear fixed motor. The unmanned aircraft was designed for search and rescue applications, capable of vertical takeoff, hover, and efficient forward flight.
The...
Structural analysis (stress & deflection)Load case development (lift, distributed loads)Load case development for VTOL and forward flightFusion (part and assembly modeling)Wing structure design (spar layout, geometry)Hand calculations (mechanics of materials)Design validation and iteration