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Aerodynamics and Acoustics of rotor Blade-Vortex Interactions

Yu, Yung H. and Tung, Chee and Gallman, Judy and Schultz, Klaus-J. and van der Wall, Berend G. and Spiegel, Pierre and Michea, B. (1995) Aerodynamics and Acoustics of rotor Blade-Vortex Interactions. Journal of Aircraft, 32 (5), pp. 970-977. ISSN 0021-8669

Full text not available from this repository.

Abstract

Helicopter rotor simulation codes of different organizations are validated against experimental data obtained in the DNW. The comparison addresses rotor blade loading, wake geometry, blade motion and noise radiation. Although specific differences exist the general prediciton of rotor noise is reasonably well.

Item URL in elib:https://elib.dlr.de/20303/
Document Type:Article
Title:Aerodynamics and Acoustics of rotor Blade-Vortex Interactions
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Yu, Yung H.AFDDUNSPECIFIED
Tung, CheeAFDDUNSPECIFIED
Gallman, JudyAFDDUNSPECIFIED
Schultz, Klaus-J.UNSPECIFIEDUNSPECIFIED
van der Wall, Berend G.UNSPECIFIEDUNSPECIFIED
Spiegel, PierreONERAUNSPECIFIED
Michea, B.ONERAUNSPECIFIED
Date:1995
Journal or Publication Title:Journal of Aircraft
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:Yes
Volume:32
Page Range:pp. 970-977
Editors:
EditorsEmail
AIAA, UNSPECIFIED
ISSN:0021-8669
Status:Published
Keywords:Rotor aerodynamics, BVI
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:Rotorcraft (old)
DLR - Research area:Aeronautics
DLR - Program:L RR - Rotorcraft Research
DLR - Research theme (Project):L - The Quiet and Comfortable Rotorcraft (old)
Location: Braunschweig
Institutes and Institutions:Institute of Flight Systems > Rotorcraft
Institute of Aerodynamics and Flow Technology > Technical Acoustics
Deposited By: van der Wall, Prof. Dr. Berend G.
Deposited On:04 Jan 2006
Last Modified:27 Apr 2009 04:45

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