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Schütte, Andreas und Cummings, Russ M. und Loeser, Thomas (2012) An integrated computational/experimental approach to X-31 stability & control estimation. Aerospace Science and Technology, 20 (1), Seiten 2-11. Elsevier. doi: 10.1016/j.ast.2011.10.010. ISSN 1270-9638.
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Kurzfassung
A comprehensive research program designed to investigate the ability of computational methods to predict stability and control characteristics of realistic flight vehicles has been undertaken. The approach to simulating static and dynamic stability characteristics for the X-31 configuration was performed by NATO RTO Task Group AVT-161, which resulted in an integrated computational and experimental study. The stability characteristics of the vehicle were evaluated via a highly integrated approach, where CFD and experimental results were used in a parallel and collaborative fashion. The results show that computational methods have made great strides in predicting static and dynamic stability characteristics, but several key issues need to be resolved before efficient, affordable, and reliable predictions are available.
| elib-URL des Eintrags: | https://elib.dlr.de/80502/ | ||||||||||||||||
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| Dokumentart: | Zeitschriftenbeitrag | ||||||||||||||||
| Titel: | An integrated computational/experimental approach to X-31 stability & control estimation | ||||||||||||||||
| Autoren: |
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| Datum: | Juli 2012 | ||||||||||||||||
| Erschienen in: | Aerospace Science and Technology | ||||||||||||||||
| Referierte Publikation: | Ja | ||||||||||||||||
| Open Access: | Nein | ||||||||||||||||
| Gold Open Access: | Nein | ||||||||||||||||
| In SCOPUS: | Ja | ||||||||||||||||
| In ISI Web of Science: | Ja | ||||||||||||||||
| Band: | 20 | ||||||||||||||||
| DOI: | 10.1016/j.ast.2011.10.010 | ||||||||||||||||
| Seitenbereich: | Seiten 2-11 | ||||||||||||||||
| Verlag: | Elsevier | ||||||||||||||||
| ISSN: | 1270-9638 | ||||||||||||||||
| Status: | veröffentlicht | ||||||||||||||||
| Stichwörter: | X-31; Vortical flow; Experiment; Wind tunnel; RTO; AVT; CFD; Stability and control; DLR; USAFA; DNW; NWB | ||||||||||||||||
| HGF - Forschungsbereich: | Luftfahrt, Raumfahrt und Verkehr | ||||||||||||||||
| HGF - Programm: | Luftfahrt | ||||||||||||||||
| HGF - Programmthema: | Starrflügler (alt) | ||||||||||||||||
| DLR - Schwerpunkt: | Luftfahrt | ||||||||||||||||
| DLR - Forschungsgebiet: | L AR - Starrflüglerforschung | ||||||||||||||||
| DLR - Teilgebiet (Projekt, Vorhaben): | L - Militärische Technologien (alt) | ||||||||||||||||
| Standort: | Braunschweig | ||||||||||||||||
| Institute & Einrichtungen: | Institut für Aerodynamik und Strömungstechnik > Transportflugzeuge | ||||||||||||||||
| Hinterlegt von: | Schütte, Andreas | ||||||||||||||||
| Hinterlegt am: | 11 Jan 2013 10:31 | ||||||||||||||||
| Letzte Änderung: | 07 Nov 2023 13:04 |
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