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

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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Bibliographic Details
Main Authors: Alexander Albrecht, Andreas Bender, Philipp Strathoff, Clemens Zumegen, Eike Stumpf, Andreas Strohmayer
Format: Article
Language:English
Published: MDPI AG 2023-04-01
Series:Aerospace
Subjects:
aircraft design
distributed propulsion
hybrid-electric flight
critical loss of thrust
vertical stabilizer
Online Access:https://www.mdpi.com/2226-4310/10/5/395

Internet

https://www.mdpi.com/2226-4310/10/5/395

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