Splettstößer, W.R. und Kube, R. und Wagner, W. und Seelhorst, U. und Boutier, A. und Micheli, F. und Mercker, E. und Pengel, K. (1997) Key Results from a Higher Harmonic Control Aeroacoustic Rotor Test (HART). Journal of the American Helicopter Society, 42 (1), Seiten 58-78.
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Kurzfassung
In a major cooperative research program within existing US-German and US-French Memoranda of Understandings (MoU's) a comprehensive experimental study was conducted with a 40-percent geometrically and dynamically scaled BO-105 main rotor operated in the open-jet-anechoic test section of the German-Dutch Wind Tunnel (DNW). The objectives of the program were to improve the physical understanding and the mathematical modelling of the effects of the higher harmonic blade pitch control technique on blade-vortex interaction (BVI) impulsive noise and vibration reduction. A unique set of acoustic, dynamic, dynamic response, performance, and rotor wake data were acquired with a pressure and strain gauge instrumentedblade and by application of non-intrusive measurement techniques. This paper is focused on the experimental part of this research program, termed Higher-harmonic-control Aeroacoustic Rotor Test (HART) which was jointly performed by researchers from the.
elib-URL des Eintrags: | https://elib.dlr.de/36545/ | ||||||||||||||||||||||||||||||||||||
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Dokumentart: | Zeitschriftenbeitrag | ||||||||||||||||||||||||||||||||||||
Zusätzliche Informationen: | LIDO-Berichtsjahr=1997, | ||||||||||||||||||||||||||||||||||||
Titel: | Key Results from a Higher Harmonic Control Aeroacoustic Rotor Test (HART) | ||||||||||||||||||||||||||||||||||||
Autoren: |
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Datum: | 1997 | ||||||||||||||||||||||||||||||||||||
Erschienen in: | Journal of the American Helicopter Society | ||||||||||||||||||||||||||||||||||||
Referierte Publikation: | Ja | ||||||||||||||||||||||||||||||||||||
Open Access: | Nein | ||||||||||||||||||||||||||||||||||||
Gold Open Access: | Nein | ||||||||||||||||||||||||||||||||||||
In SCOPUS: | Nein | ||||||||||||||||||||||||||||||||||||
In ISI Web of Science: | Ja | ||||||||||||||||||||||||||||||||||||
Band: | 42 | ||||||||||||||||||||||||||||||||||||
Seitenbereich: | Seiten 58-78 | ||||||||||||||||||||||||||||||||||||
Status: | veröffentlicht | ||||||||||||||||||||||||||||||||||||
Stichwörter: | Rotor impulsive noise reduction, blade-vortex interaction (BVI) noise reduction, higher harmonic blade pitch control (HHC) | ||||||||||||||||||||||||||||||||||||
HGF - Forschungsbereich: | Verkehr und Weltraum (alt) | ||||||||||||||||||||||||||||||||||||
HGF - Programm: | Luftfahrt | ||||||||||||||||||||||||||||||||||||
HGF - Programmthema: | keine Zuordnung | ||||||||||||||||||||||||||||||||||||
DLR - Schwerpunkt: | Luftfahrt | ||||||||||||||||||||||||||||||||||||
DLR - Forschungsgebiet: | L DT - Drehflüglertechnologien | ||||||||||||||||||||||||||||||||||||
DLR - Teilgebiet (Projekt, Vorhaben): | L - Der leise und komfortable Drehflügler (alt) | ||||||||||||||||||||||||||||||||||||
Standort: | Köln-Porz , Braunschweig , Göttingen | ||||||||||||||||||||||||||||||||||||
Institute & Einrichtungen: | Institut für Aerodynamik und Strömungstechnik > Institut für Entwurfsaerodynamik Institut für Flugsystemtechnik > Institut für Flugmechanik Institut für Aeroelastik Institut für Aerodynamik und Strömungstechnik > Institut für Strömungsmechanik | ||||||||||||||||||||||||||||||||||||
Hinterlegt von: | DLR-Beauftragter, elib | ||||||||||||||||||||||||||||||||||||
Hinterlegt am: | 03 Apr 2006 | ||||||||||||||||||||||||||||||||||||
Letzte Änderung: | 27 Apr 2009 10:06 |
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