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Helicopter Rotor Blade Aeroacoustics: A Comparison of Model-scale Wind Tunnel and Full-scale Flight Test Results

Heller, H. and Buchholz, H. and Schultz, K.-J. and Ahmed, S.R. and Splettstößer, W. (1996) Helicopter Rotor Blade Aeroacoustics: A Comparison of Model-scale Wind Tunnel and Full-scale Flight Test Results. Nanjing University of Aeronautics and Astronautics (NUAA), Nanjing/China, 1.11.1996.(Einladung).

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Document Type:Conference or Workshop Item (Speech)
Additional Information: LIDO-Berichtsjahr=1996,
Title:Helicopter Rotor Blade Aeroacoustics: A Comparison of Model-scale Wind Tunnel and Full-scale Flight Test Results
Authors:
AuthorsInstitution or Email of Authors
Heller, H.UNSPECIFIED
Buchholz, H.UNSPECIFIED
Schultz, K.-J.UNSPECIFIED
Ahmed, S.R.UNSPECIFIED
Splettstößer, W.UNSPECIFIED
Date:1996
Status:Published
Event Title:Nanjing University of Aeronautics and Astronautics (NUAA), Nanjing/China, 1.11.1996.(Einladung)
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
Location: Köln-Porz , Braunschweig , Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Institut für Entwurfsaerodynamik
Deposited By: elib DLR-Beauftragter
Deposited On:03 Apr 2006
Last Modified:27 Apr 2009 10:06

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