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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Item URL in elib:

https://elib.dlr.de/36512/

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:

Authors	Institution or Email of Authors	Author's ORCID iD	ORCID Put Code
Heller, H.	UNSPECIFIED	UNSPECIFIED	UNSPECIFIED
Buchholz, H.	UNSPECIFIED	UNSPECIFIED	UNSPECIFIED
Schultz, K.-J.	UNSPECIFIED	UNSPECIFIED	UNSPECIFIED
Ahmed, S.R.	UNSPECIFIED	UNSPECIFIED	UNSPECIFIED
Splettstößer, W.	UNSPECIFIED	UNSPECIFIED	UNSPECIFIED

Date:

1996

Open Access:

Gold Open Access:

In SCOPUS:

In ISI Web of Science:

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 (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 10:06

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