Please use this identifier to cite or link to this item: https://doi.org/10.48441/4427.245
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Publisher DOI: 10.13111/2066-8201.2021.13.3.13
Title: Empennage sizing with the tail volume complemented with a method for dorsal fin layout
Language: English
Authors: Scholz, Dieter  
Keywords: aircraft; airplane; tail; tailplane; stabilizer; fin; THS; lever; moment; fuselage; wing
Issue Date: Sep-2021
Publisher: National Institute for Aerospace Research Elie Carafoli
Journal or Series Name: INCAS Bulletin 
Volume: 13
Issue: 3
Startpage: 149
Endpage: 164
Project: Spitzencluster Luftfahrt - Metropolregion Hamburg; Teilprojekt 3: Effizienter Flughafen 2030 
Abstract: 
Purpose: Provide good values for the tail volume coefficient and the lever arm as a percentage of the fuselage length. Provide a statistical method for dorsal fin layout. ––– Methodology: Based on an understanding of flight physics, the statistical correlation of real aircraft parameters is investigated. This is based on the firm conviction that high fidelity parameters for future aircraft need a ...
URI: http://hdl.handle.net/20.500.12738/11442
DOI: 10.48441/4427.245
ISSN: 2247-4528
Review status: This version was peer reviewed (peer review)
Institute: Department Fahrzeugtechnik und Flugzeugbau 
Fakultät Technik und Informatik 
Forschungs- und Transferzentrum Future Air Mobility 
Forschungsgruppe Flugzeugentwurf und -systeme (AERO) 
Type: Article
Funded by: Bundesministerium für Forschung, Technologie und Raumfahrt 
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