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Vicroy, Dan D. und Huber, Kerstin Claudie und Rohlf, Detlef und Löser, Thomas (2014) Low-speed Dynamic Wind Tunnel Test Analysis of a Generic 53° Swept UCAV Configuration with Controls. In: 32nd AIAA Applied Aerodynamics Conference (2003), Seiten 1-24. 32nd AIAA Applied Aerodynamics Conference, Atlanta, GA, USA, 2014-06-16 - 2014-06-20, Atlanta, GA, USA. doi: 10.2514/6.2014-2003.
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Offizielle URL: http://arc.aiaa.org/doi/pdf/10.2514/6.2014-2003
Kurzfassung
Several static and dynamic forced-motion wind tunnel tests have been conducted on a generic unmanned combat air vehicle (UCAV) configuration with a 53° swept leading edge. These tests are part of an international research effort to assess and advance the state-of-art of computational fluid dynamics (CFD) methods to predict the static and dynamic stability and control characteristics for this type of configuration. This paper describes the dynamic forced motion data collected from two different models of this UCAV configuration as well as analysis of the control surface deflections on the dynamic forces and moments
| elib-URL des Eintrags: | https://elib.dlr.de/90262/ | ||||||||||||||||||||
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| Dokumentart: | Konferenzbeitrag (Vortrag) | ||||||||||||||||||||
| Zusätzliche Informationen: | DOI: 10.2514/6.2014-2003 | ||||||||||||||||||||
| Titel: | Low-speed Dynamic Wind Tunnel Test Analysis of a Generic 53° Swept UCAV Configuration with Controls | ||||||||||||||||||||
| Autoren: |
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| Datum: | Juni 2014 | ||||||||||||||||||||
| Erschienen in: | 32nd AIAA Applied Aerodynamics Conference | ||||||||||||||||||||
| Referierte Publikation: | Ja | ||||||||||||||||||||
| Open Access: | Nein | ||||||||||||||||||||
| Gold Open Access: | Nein | ||||||||||||||||||||
| In SCOPUS: | Nein | ||||||||||||||||||||
| In ISI Web of Science: | Nein | ||||||||||||||||||||
| DOI: | 10.2514/6.2014-2003 | ||||||||||||||||||||
| Seitenbereich: | Seiten 1-24 | ||||||||||||||||||||
| Status: | veröffentlicht | ||||||||||||||||||||
| Stichwörter: | UCAV, vortical flow, control devices, delta wing, Experiment, Stability and Control, dynamic | ||||||||||||||||||||
| Veranstaltungstitel: | 32nd AIAA Applied Aerodynamics Conference, Atlanta, GA, USA | ||||||||||||||||||||
| Veranstaltungsort: | Atlanta, GA, USA | ||||||||||||||||||||
| Veranstaltungsart: | internationale Konferenz | ||||||||||||||||||||
| Veranstaltungsbeginn: | 16 Juni 2014 | ||||||||||||||||||||
| Veranstaltungsende: | 20 Juni 2014 | ||||||||||||||||||||
| Veranstalter : | AIAA | ||||||||||||||||||||
| 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 | ||||||||||||||||||||
| Institute & Einrichtungen: | Institut für Aerodynamik und Strömungstechnik > Transportflugzeuge | ||||||||||||||||||||
| Hinterlegt von: | Schütte, Andreas | ||||||||||||||||||||
| Hinterlegt am: | 03 Sep 2014 15:03 | ||||||||||||||||||||
| Letzte Änderung: | 24 Apr 2024 19:56 |
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