Vicroy, Dan D. und Huber, Kerstin Claudie und Rein, Martin und Irving, Jonathan und Rigby, Glyn und Loeser, Thomas und Birch, Trevor J. (2016) Experimental Investigations of a Generic Swept Unmanned Combat Air Vehicle with Controls. Journal of Aircraft, 55 (2), Seiten 475-501. American Institute of Aeronautics and Astronautics (AIAA). doi: 10.2514/1.C033782. ISSN 0021-8669.
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Offizielle URL: http://dx.doi.org/10.2514/1.C033782
Kurzfassung
Several static and dynamic forced-motion wind-tunnel tests on a generic unmanned combat air vehicle configuration with a 53 deg swept leading edge are reviewed. The static tests include both subsonic and transonic measurements. These tests are part of an international research effort to assess and advance the state-of-the-art of computational-fluid-dynamics methods to predict the static and dynamic stability and control characteristics for this type of configuration. The tests included analysis of trailing-edge control surface effectiveness. This paper describes the data collected from three different models of this unmanned combat air vehicle configuration in four different wind tunnels. A subset of this large experimental dataset was selected as focus test cases for computational-fluid-dynamics comparison. The focus test case data are presented in detail.
elib-URL des Eintrags: | https://elib.dlr.de/105790/ | ||||||||||||||||||||||||||||||||
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Dokumentart: | Zeitschriftenbeitrag | ||||||||||||||||||||||||||||||||
Titel: | Experimental Investigations of a Generic Swept Unmanned Combat Air Vehicle with Controls | ||||||||||||||||||||||||||||||||
Autoren: |
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Datum: | 6 Juni 2016 | ||||||||||||||||||||||||||||||||
Erschienen in: | Journal of Aircraft | ||||||||||||||||||||||||||||||||
Referierte Publikation: | Ja | ||||||||||||||||||||||||||||||||
Open Access: | Nein | ||||||||||||||||||||||||||||||||
Gold Open Access: | Nein | ||||||||||||||||||||||||||||||||
In SCOPUS: | Ja | ||||||||||||||||||||||||||||||||
In ISI Web of Science: | Ja | ||||||||||||||||||||||||||||||||
Band: | 55 | ||||||||||||||||||||||||||||||||
DOI: | 10.2514/1.C033782 | ||||||||||||||||||||||||||||||||
Seitenbereich: | Seiten 475-501 | ||||||||||||||||||||||||||||||||
Herausgeber: |
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Verlag: | American Institute of Aeronautics and Astronautics (AIAA) | ||||||||||||||||||||||||||||||||
ISSN: | 0021-8669 | ||||||||||||||||||||||||||||||||
Status: | veröffentlicht | ||||||||||||||||||||||||||||||||
Stichwörter: | UCAV, wind tunnel testing, NaSA, DLR, BAE Systems, dstl, control surface effectiveness, subsonic and transonic measurements | ||||||||||||||||||||||||||||||||
HGF - Forschungsbereich: | Luftfahrt, Raumfahrt und Verkehr | ||||||||||||||||||||||||||||||||
HGF - Programm: | Luftfahrt | ||||||||||||||||||||||||||||||||
HGF - Programmthema: | Flugzeuge | ||||||||||||||||||||||||||||||||
DLR - Schwerpunkt: | Luftfahrt | ||||||||||||||||||||||||||||||||
DLR - Forschungsgebiet: | L AR - Aircraft Research | ||||||||||||||||||||||||||||||||
DLR - Teilgebiet (Projekt, Vorhaben): | L - Militärische Technologien (alt) | ||||||||||||||||||||||||||||||||
Standort: | Braunschweig , Göttingen | ||||||||||||||||||||||||||||||||
Institute & Einrichtungen: | Institut für Aerodynamik und Strömungstechnik > Transportflugzeuge Institut für Aerodynamik und Strömungstechnik > Hochgeschwindigkeitskonfigurationen | ||||||||||||||||||||||||||||||||
Hinterlegt von: | Schütte, Andreas | ||||||||||||||||||||||||||||||||
Hinterlegt am: | 22 Aug 2016 09:22 | ||||||||||||||||||||||||||||||||
Letzte Änderung: | 05 Nov 2020 21:56 |
Verfügbare Versionen dieses Eintrags
- Experimental Investigations of a Generic Swept Unmanned Combat Air Vehicle with Controls. (deposited 22 Aug 2016 09:22) [Gegenwärtig angezeigt]
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