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Flight Controls of Otto Lilienthal's Experimental Monoplane from 1895

Raffel, Markus and Wienke, Felix and Schwarz, Clemens and Dillmann, Andreas (2022) Flight Controls of Otto Lilienthal's Experimental Monoplane from 1895. Journal of Aircraft, 59 (6), pp. 1616-1625. American Institute of Aeronautics and Astronautics (AIAA). doi: 10.2514/1.C037047. ISSN 0021-8669.

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Official URL: https://arc.aiaa.org/doi/10.2514/1.C037047

Abstract

In 1889, Otto Lilienthal published his book Birdflight as the Basis of Aviation, containing the first lift-versus-drag data of cambered wings and other important information required for human flight. In 1895, Lilienthal demonstrated his 12th aircraft design, a monoplane with a wing area of over 20 m2. Because of its wingspan of almost 9 m and wing chord length of 3 m, Lilienthal’s largest monoplane can only be used in light winds. Lilienthal applied for a patent on the same day. The patent claim was submitted for the front wing (Vorflügel), a leading-edge flap used in a glider for this purpose for the first time. Because of the size of the apparatus, three profile rails were slid onto each wing instead of the usual two.

Item URL in elib:https://elib.dlr.de/191143/
Document Type:Article
Title:Flight Controls of Otto Lilienthal's Experimental Monoplane from 1895
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Raffel, MarkusUNSPECIFIEDhttps://orcid.org/0000-0002-3340-9115133716131
Wienke, FelixUNSPECIFIEDhttps://orcid.org/0000-0003-0081-1084UNSPECIFIED
Schwarz, ClemensUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Dillmann, AndreasUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Date:17 October 2022
Journal or Publication Title:Journal of Aircraft
Refereed publication:Yes
Open Access:Yes
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:Yes
Volume:59
DOI:10.2514/1.C037047
Page Range:pp. 1616-1625
Editors:
EditorsEmailEditor's ORCID iDORCID Put Code
UNSPECIFIEDARCUNSPECIFIEDUNSPECIFIED
Publisher:American Institute of Aeronautics and Astronautics (AIAA)
ISSN:0021-8669
Status:Published
Keywords:Fliegeberg, controllability, wing design,
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:other
DLR - Research area:Aeronautics
DLR - Program:L - no assignment
DLR - Research theme (Project):L - no assignment
Location: Göttingen
Institutes and Institutions:Institute for Aerodynamics and Flow Technology > Helicopter, GO
Deposited By: Carter, Beatrice
Deposited On:06 Dec 2022 11:44
Last Modified:25 Apr 2023 10:05

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