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Active Twist Hover Test - Test Documentation and Representative Results -

Hoffmann, Frauke and Schneider, Oliver and Opitz, Steffen (2011) Active Twist Hover Test - Test Documentation and Representative Results -. DLR-Interner Bericht. DLR-IB 111-2011/7, 104 S.

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Abstract

An active twist model rotor blade has been designed and built by the Institute of Composite Structures and Adaptive Systems. The design is based on a Bo105 model rotor blade and is called AT4. The model rotor has been operated as a one-bladed rotor with a counterweight at the opposite side in order to balance the rotor. The tests have been performed at the DLR Instititue of Flight Systems between January and April 2009. This report presents the model set-up, calibration works in the pre-test phase, model instrumentation, data acquisition, test conduction, and some representative results.

Item URL in elib:https://elib.dlr.de/69011/
Document Type:Monograph (DLR-Interner Bericht)
Title:Active Twist Hover Test - Test Documentation and Representative Results -
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Hoffmann, FraukeDLR-FTUNSPECIFIED
Schneider, OliverDLR-FTUNSPECIFIED
Opitz, SteffenDLR-FAUNSPECIFIED
Date:16 February 2011
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Number of Pages:104
Status:Published
Keywords:active twist, model rotor, test
Institution:DLR
Department:Hubschrauber
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 Active Rotorcraft (old)
Location: Braunschweig
Institutes and Institutions:Institute of Flight Systems > Rotorcraft
Institute of Composite Structures and Adaptive Systems
Deposited By: Hoffmann, Frauke
Deposited On:05 Jul 2011 14:36
Last Modified:05 Jul 2011 14:36

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