Performance, Stability and Control of Electric Short Takeoff and Landing Aircraft

Performance, Stability and Control of Electric Short Takeoff and Landing Aircraft

The maturation of distributed electric propulsion (DEP) technologies for aircraft presents an opportunity to develop new aircraft configurations which take advantage of favorable aero-propulsive couplings. One such arrangement is the electrically blown wing, where the slipstream of distributed, elec...

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Bibliographic Details
Main Author:	Courtin, Christopher B.
Other Authors:	Greitzer, Edward M.
Format:	Thesis
Published:	Massachusetts Institute of Technology 2024
Online Access:	https://hdl.handle.net/1721.1/155476

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