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Prediction of Rotor Aeroacoustics in Forward Flight by a Lifting Surface Method

Lieser, J.A. and Lohmann, D. and Schultz, K.J. (1994) Prediction of Rotor Aeroacoustics in Forward Flight by a Lifting Surface Method. In: American Helicopter Society, 50th Annual Forum, Washington DC, May 11-13, 1994., pp. 45-60.

Full text not available from this repository.

Abstract

Mit einem Panelverfahren werden Hubschrauberrotoren im Schwebeflug und im Vorwaertsflug berechnet. Der Rueckwirkung der Blattspitzenwirbel auf den Rotor wird mit einem Nachlaufmodell von Beddoes beschrieben. Zur Berechnung der Laermabstrahlung wird die Ffowks Williams/Hawkings Gleichung unter Beruecksichtigung der Monopol und Dipolterme verwendet.

Item URL in elib:https://elib.dlr.de/36312/
Document Type:Conference or Workshop Item (Paper)
Additional Information: institution=American Helicopter Society, LIDO-Berichtsjahr=1994,
Title:Prediction of Rotor Aeroacoustics in Forward Flight by a Lifting Surface Method
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Lieser, J.A.UNSPECIFIEDUNSPECIFIED
Lohmann, D.UNSPECIFIEDUNSPECIFIED
Schultz, K.J.UNSPECIFIEDUNSPECIFIED
Date:1994
Journal or Publication Title:American Helicopter Society, 50th Annual Forum, Washington DC, May 11-13, 1994.
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Page Range:pp. 45-60
Status:Published
Keywords:Rotor, Akustik, Blatt Wirbel Interferenz
HGF - Research field:UNSPECIFIED
HGF - Program:Aeronautics
HGF - Program Themes:other
DLR - Research area:UNSPECIFIED
DLR - Program:L DT - Drehflüglertechnologien
DLR - Research theme (Project):L - The Quiet and Comfortable Rotorcraft (old)
Location: Köln-Porz , Braunschweig , Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Institut für Entwurfsaerodynamik
Deposited By: DLR-Beauftragter, elib
Deposited On:03 Apr 2006
Last Modified:27 Apr 2009 10:05

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