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Heister, C. C. und Klein, A. und Krämer, E. (2010) RANS-Based Laminar-Turbulent Transition Prediction for Airfoil and Rotary Wing Applications Using Semi/Empirical Criteria. STAB-Symposium 2010, 09.-10.11.2010, Berlin.
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Kurzfassung
The transition prediction capability of two different semi/empirical methods originating from fixed wing applications is studied for steady, rotary wing application. This includes the AHD method, used with approximated boundary layer data, as well as the Drela eN envelope method, based on integral boundary layer parameters. The methods have been implemented in the DLR's structured flow solver FLOWer. A two-dimensional test case (Somers airfoil) and three-dimensional rotor test case at hover (DLR Bo 105 flight test ) serve to validate the computed transition locations.
| elib-URL des Eintrags: | https://elib.dlr.de/79461/ | ||||||||||||||||
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| Dokumentart: | Konferenzbeitrag (Vortrag) | ||||||||||||||||
| Titel: | RANS-Based Laminar-Turbulent Transition Prediction for Airfoil and Rotary Wing Applications Using Semi/Empirical Criteria | ||||||||||||||||
| Autoren: |
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| Datum: | November 2010 | ||||||||||||||||
| Referierte Publikation: | Nein | ||||||||||||||||
| Open Access: | Nein | ||||||||||||||||
| Gold Open Access: | Nein | ||||||||||||||||
| In SCOPUS: | Nein | ||||||||||||||||
| In ISI Web of Science: | Nein | ||||||||||||||||
| Status: | veröffentlicht | ||||||||||||||||
| Stichwörter: | helicopter, rotor, hover, transition, laminar, boundary layer, empirical, AHD, Drela, eN, Blasius, Thwaites | ||||||||||||||||
| Veranstaltungstitel: | STAB-Symposium 2010 | ||||||||||||||||
| Veranstaltungsort: | Berlin | ||||||||||||||||
| Veranstaltungsart: | nationale Konferenz | ||||||||||||||||
| Veranstaltungsdatum: | 09.-10.11.2010 | ||||||||||||||||
| Veranstalter : | STAB | ||||||||||||||||
| HGF - Forschungsbereich: | Luftfahrt, Raumfahrt und Verkehr | ||||||||||||||||
| HGF - Programm: | Luftfahrt | ||||||||||||||||
| HGF - Programmthema: | Drehflügler (alt) | ||||||||||||||||
| DLR - Schwerpunkt: | Luftfahrt | ||||||||||||||||
| DLR - Forschungsgebiet: | L RR - Drehflüglerforschung | ||||||||||||||||
| DLR - Teilgebiet (Projekt, Vorhaben): | L - Der virtuelle Drehflügler (alt) | ||||||||||||||||
| Standort: | Braunschweig | ||||||||||||||||
| Institute & Einrichtungen: | Institut für Aerodynamik und Strömungstechnik > C²A²S²E - Center for Computer Applications in AeroSpace Science and Engineering | ||||||||||||||||
| Hinterlegt von: | Heister, Christoph | ||||||||||||||||
| Hinterlegt am: | 06 Dez 2012 15:55 | ||||||||||||||||
| Letzte Änderung: | 30 Jun 2016 10:21 |
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