Schütte, Andreas und Huber, Kerstin Claudie und Boelens, Okko J. (2014) Static and dynamic numerical simulations of a generic UCAV configuration with and without control devices. In: 32nd AIAA Applied Aerodynamics Conference (2132), Seiten 1-26. 32nd AIAA Applied Aerodynamics Conference, Atlanta, GA, USA, 2014-06-16 - 2014-06-20, USA. doi: 10.2514/6.2014-2132.
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Offizielle URL: http://arc.aiaa.org/doi/pdf/10.2514/6.2014-2132
Kurzfassung
A contribution for the assessment of the static and dynamic aerodynamic behavior of a generic UCAV configuration with control devices using CFD methods is given. For the CFD simulations the unstructured grid based DLR TAU-Code and the structured grid based NLR solver ENSOLV are used. The numerical methods are verified by experimental wind tunnel data. The current investigations should provide a contribution to assess the prediction capability of control device effectiveness using CFD methods. The presented computational results for the assessment will be validated by dedicated experimental data. Furthermore, it should support the understanding of the flow physics around the trailing edge control devices of highly swept configurations with a vortex dominated flow field. Design requirements should be able draw by analyzing the interaction between the vortical flow and the control devices. The present work is part of the NATO STO/AVT Task Group AVT-201 on Stability and Control prediction methods
elib-URL des Eintrags: | https://elib.dlr.de/90254/ | ||||||||||||||||
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Dokumentart: | Konferenzbeitrag (Vortrag) | ||||||||||||||||
Zusätzliche Informationen: | DOI: 10.2514/6.2014-2132 | ||||||||||||||||
Titel: | Static and dynamic numerical simulations of a generic UCAV configuration with and without control devices | ||||||||||||||||
Autoren: |
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Datum: | Juni 2014 | ||||||||||||||||
Erschienen in: | 32nd AIAA Applied Aerodynamics Conference | ||||||||||||||||
Referierte Publikation: | Ja | ||||||||||||||||
Open Access: | Ja | ||||||||||||||||
Gold Open Access: | Nein | ||||||||||||||||
In SCOPUS: | Nein | ||||||||||||||||
In ISI Web of Science: | Nein | ||||||||||||||||
DOI: | 10.2514/6.2014-2132 | ||||||||||||||||
Seitenbereich: | Seiten 1-26 | ||||||||||||||||
Status: | veröffentlicht | ||||||||||||||||
Stichwörter: | UCAV, vortical flow, CFD, DLR-TAU, ENSOLV, Validiation, Stability and Control | ||||||||||||||||
Veranstaltungstitel: | 32nd AIAA Applied Aerodynamics Conference, Atlanta, GA, USA | ||||||||||||||||
Veranstaltungsort: | 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 15:19 | ||||||||||||||||
Letzte Änderung: | 24 Apr 2024 19:56 |
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