Khier, W. und Le Chuiton, F. und Schwarz, T. (2002) Navier-Stokes Analysis of the Helicopter Rotor-Fuselage Interference in Forward Flight. CEAS Aerospace Aerodynamics Research Conference, 2002-06-10 - 2002-06-12, Cambridge, UK.
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Kurzfassung
This paper demonstrates the capabilities of the DLR's CFD code (FLOWer) to predict air flow past helicopters via the solution of the compressible Navier-Stokes equations in three dimensions. Both the stationary actuator disc and a time accurate moving Chimera method were applied to simulate low Mach numbers, forward flight flow cases. The flight conditions correspond to wind tunnel measurements of a scale model of an Eurocopter BO-105 helicopter for a range of Reynolds and Mach numbers of 11 to 12 Million and 0.125 to 0.135 respectively. The numerical approach is based on finite volume discretization and a two-equation eddy viscosity k-omega model. Comparison of the results with experimental measurements revealed that both the model support and spoiler play a dominant role in determining the overall flow pattern around the aircraft.
elib-URL des Eintrags: | https://elib.dlr.de/18865/ | ||||||||||||||||
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Dokumentart: | Konferenzbeitrag (Paper) | ||||||||||||||||
Zusätzliche Informationen: | LIDO-Berichtsjahr=2005, | ||||||||||||||||
Titel: | Navier-Stokes Analysis of the Helicopter Rotor-Fuselage Interference in Forward Flight | ||||||||||||||||
Autoren: |
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Datum: | 2002 | ||||||||||||||||
Open Access: | Nein | ||||||||||||||||
Gold Open Access: | Nein | ||||||||||||||||
In SCOPUS: | Nein | ||||||||||||||||
In ISI Web of Science: | Nein | ||||||||||||||||
Status: | veröffentlicht | ||||||||||||||||
Stichwörter: | CFD, Helicopter Aerodynamics, Rotor-Fuselage interaction, Time accurate simulations | ||||||||||||||||
Veranstaltungstitel: | CEAS Aerospace Aerodynamics Research Conference | ||||||||||||||||
Veranstaltungsort: | Cambridge, UK | ||||||||||||||||
Veranstaltungsart: | internationale Konferenz | ||||||||||||||||
Veranstaltungsbeginn: | 10 Juni 2002 | ||||||||||||||||
Veranstaltungsende: | 12 Juni 2002 | ||||||||||||||||
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 aktive Drehflügler (alt) | ||||||||||||||||
Standort: | Köln-Porz , Braunschweig , Göttingen | ||||||||||||||||
Institute & Einrichtungen: | Institut für Aerodynamik und Strömungstechnik | ||||||||||||||||
Hinterlegt von: | Grant, Claudia | ||||||||||||||||
Hinterlegt am: | 11 Jan 2006 | ||||||||||||||||
Letzte Änderung: | 24 Apr 2024 19:00 |
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