Marcus Stalberg

Design Responsible Engineer responsible for the structural substantiation of various internal and external modifications to metallic and composite airplane frames. Approval of repair solutions and performing stress analysis of repairs in primary composite fuselage structure, including report writing.

Structural analysis and testing of primary wing composite structure. Approval and analysis of repairs in primary wing composite structure.

Material and design concept studies. Establishing of weight target and calculation of weight of airplane substructure. Structural analysis of manufacturing jig.

Aerodynamic CFD trade studies and drag calculations of different wing geometries and airplane configurations. Calculating and testing flight performance such as takeoff, landing, climb, en-route performance. Supporting international crash investigations. Department lead of the mass properties department responsible for weight targets, impact of structural modifications and budget.

Aerodynamics, Mechanics of Materials