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Titel:

Investigation of Centrifugal Pumping Rotor Blades in Hover Using CFD

Dokumenttyp:
Konferenzbeitrag
Autor(en):
Platzer, S., Rauleder, J., Hajek, M.
Seitenangaben Beitrag:
16
Abstract:
Rotorcraft in hover, descent, and low-speed forward flight operate close to the vortices trailed from their rotors. Consequently, blade vortex interactions occur, which can result in large transient loads on the blades, high noise levels, and vibrations. Furthermore, the trailed vortices can persist far downstream in the rotor wake, where they may produce dust or snow clouds when the rotorcraft operates close to the ground. Therefore, in the present research work one possible passive solution t...     »
Stichworte:
applied aerodynamics, rotorcraft aerodynamics, CFD, flow control, vortex flows
Dewey-Dezimalklassifikation:
620 Ingenieurwissenschaften
Kongress- / Buchtitel:
AIAA Aviation 2016
Kongress / Zusatzinformationen:
34th Applied Aerodynamics Conference
Ausrichter der Konferenz:
The American Institute of Aeronautics and Astronautics
Datum der Konferenz:
June 13-17, 2016
Jahr:
2016
Nachgewiesen in:
Scopus
Sprache:
en
Volltext / DOI:
doi:http://dx.doi.org/10.2514/6.2016-3420
WWW:
http://arc.aiaa.org/doi/abs/10.2514/6.2016-3420
TUM Einrichtung:
Lehrstuhl für Hubschraubertechnologie
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