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Area Engineering

Aerodynamic and stability analysis of an aicraft with distributed propulsion

Reference persons GIOACCHINO CAFIERO, ANGELO LERRO

External reference persons Paolo J. Comunian

Description Following a thorough state-of-the art survey, the student will identify the main effects of a distributed propulsion configuration for a conventional general aviation or regional transport aircraft. Then, aided by numerical tools, the stability characteristics of such architecture are to be determined. Subsequently, an optimized configuration is to be found and studied under maneuver and normal aircraft operations. Finally, a systematic method to estimate the influence of distributed propulsion is to be proposed and used as preliminary sizing tool.

See also  thesis_flight_dynamics_distributed_propulsion.pdf 


Deadline 29/12/2024      PROPONI LA TUA CANDIDATURA