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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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.
|Document Type:||Monograph (DLR-Interner Bericht)|
|Title:||Active Twist Hover Test - Test Documentation and Representative Results -|
|Date:||16 February 2011|
|Number of Pages:||104|
|Keywords:||active twist, model rotor, test|
|HGF - Research field:||Aeronautics, Space and Transport|
|HGF - Program:||Aeronautics|
|HGF - Program Themes:||L RR - Rotorcraft Research|
|DLR - Research area:||Aeronautics|
|DLR - Program:||L RR - Rotorcraft Research|
|DLR - Research theme (Project):||L - The Active Rotorcraft (old)|
|Institutes and Institutions:||Institute of Flight Systems > Rotorcraft|
Institute of Composite Structures and Adaptive Systems
|Deposited By:||Frauke Hoffmann|
|Deposited On:||05 Jul 2011 14:36|
|Last Modified:||05 Jul 2011 14:36|
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