Influence of Electric Wing Tip Propulsion on the Sizing of the Vertical Stabilizer and Rudder in Preliminary Aircraft Design

During preliminary aircraft design, the vertical tail sizing is conventionally conducted by the use of volume coefficients. These represent a statistical approach using existing configurations’ correlating parameters, such as wing span and lever arm, to size the empennage. For a more detailed analys...

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Autors principals:	Alexander Albrecht, Andreas Bender, Philipp Strathoff, Clemens Zumegen, Eike Stumpf, Andreas Strohmayer
Format:	Artigo
Idioma:	Inglês
Publicat:	MDPI AG 2023-04-01
Col·lecció:	Aerospace
Matèries:	aircraft design distributed propulsion hybrid-electric flight critical loss of thrust vertical stabilizer
Accés en línia:	https://www.mdpi.com/2226-4310/10/5/395
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