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https://doi.org/10.48441/4427.245
License: | ![]() |
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 |
Appears in Collections: | Publications with full text |
Files in This Item:
File | Description | Size | Format | |
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AERO_PUB_INCAS_TailVolume_Vol13No3_2021.pdf | 1.11 MB | Adobe PDF | View/Open |
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