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Distributed Electric Propulsion

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Poster Undergraduate Research Program For Honor Students (922.0Kb)
Date
2019-08-19
Author
Morales, Ángel
Torres Rivera, Aníbal
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Abstract
This investigation focused on predicting aerodynamic improvements obtained when air is blown over a wing by six propellers distributed equally along the wing’s span The purpose was to validate a method to implement Distributed Electric Propulsion and quantify its impact during conceptual aircraft design
URI
http://hdl.handle.net/20.500.12475/112
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  • Undergraduate Research Program For Honor Students (URP-HS)

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