| KEYWORD |
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
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