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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| Format: | Thesis |
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Massachusetts Institute of Technology
2024
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| Online Access: | https://hdl.handle.net/1721.1/155476 |