Lead the design and optimization of the eVTOL aircraft configuration including
propeller layout component sizing and mass estimation.
Utilize ModelBased Systems Engineering (MBSE) concepts in the design of
various aircraft components to ensure a systematic integrated approach.
Select and design airfoils based on MDO concepts to improve aerodynamic
efficiency structural integrity and propeller interaction.
Design aerodynamic surfaces such as interfaces to minimize drag and improve
the lifttodrag ratio for better overall efficiency.
Build low fidelity structural beam model to evaluate aircraft eigen modes to
assess aircraft performance.