Raffel, Markus und Wienke, Felix und Schwarz, Clemens und Dillmann, Andreas (2022) Flight Controls of Otto Lilienthal's Experimental Monoplane from 1895. Journal of Aircraft, 59 (6), Seiten 1616-1625. American Institute of Aeronautics and Astronautics (AIAA). doi: 10.2514/1.C037047. ISSN 0021-8669.
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Offizielle URL: https://arc.aiaa.org/doi/10.2514/1.C037047
Kurzfassung
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.
| elib-URL des Eintrags: | https://elib.dlr.de/191143/ | ||||||||||||||||||||
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| Dokumentart: | Zeitschriftenbeitrag | ||||||||||||||||||||
| Titel: | Flight Controls of Otto Lilienthal's Experimental Monoplane from 1895 | ||||||||||||||||||||
| Autoren: |
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| Datum: | 17 Oktober 2022 | ||||||||||||||||||||
| Erschienen in: | Journal of Aircraft | ||||||||||||||||||||
| Referierte Publikation: | Ja | ||||||||||||||||||||
| Open Access: | Ja | ||||||||||||||||||||
| Gold Open Access: | Nein | ||||||||||||||||||||
| In SCOPUS: | Ja | ||||||||||||||||||||
| In ISI Web of Science: | Ja | ||||||||||||||||||||
| Band: | 59 | ||||||||||||||||||||
| DOI: | 10.2514/1.C037047 | ||||||||||||||||||||
| Seitenbereich: | Seiten 1616-1625 | ||||||||||||||||||||
| Herausgeber: |
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| Verlag: | American Institute of Aeronautics and Astronautics (AIAA) | ||||||||||||||||||||
| ISSN: | 0021-8669 | ||||||||||||||||||||
| Status: | veröffentlicht | ||||||||||||||||||||
| Stichwörter: | Fliegeberg, controllability, wing design, | ||||||||||||||||||||
| HGF - Forschungsbereich: | Luftfahrt, Raumfahrt und Verkehr | ||||||||||||||||||||
| HGF - Programm: | Luftfahrt | ||||||||||||||||||||
| HGF - Programmthema: | keine Zuordnung | ||||||||||||||||||||
| DLR - Schwerpunkt: | Luftfahrt | ||||||||||||||||||||
| DLR - Forschungsgebiet: | L - keine Zuordnung | ||||||||||||||||||||
| DLR - Teilgebiet (Projekt, Vorhaben): | L - keine Zuordnung | ||||||||||||||||||||
| Standort: | Göttingen | ||||||||||||||||||||
| Institute & Einrichtungen: | Institut für Aerodynamik und Strömungstechnik > Hubschrauber, GO | ||||||||||||||||||||
| Hinterlegt von: | Carter, Beatrice | ||||||||||||||||||||
| Hinterlegt am: | 06 Dez 2022 11:44 | ||||||||||||||||||||
| Letzte Änderung: | 25 Apr 2023 10:05 |
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