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Pitch test rig



 Pitch test rig with a 2-D aerofoil model in project STELAR
zum Bild Pitch test rig with a 2-D aerofoil model in project STELAR
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 Schematic diagram of the pitch test rig with a UAV model
zum Bild Schematic diagram of the pitch test rig with a UAV model

The Institute operates a pitch test rig (NVS) to demonstrate forced motion. It consists of a symmetrical arrangement of a two-sided hydraulic drive. A 2-D aerofoil model can be clamped between the sections and excited to perform harmonic pitching oscillation. The actuators operate with extreme precision to achieve very exact, harmonic movements with pitch amplitudes of just 0.05 degrees. These low amplitudes are necessary, for instance to determine dynamic derivatives during transonic angle of attack velocities in such a way that they are rendered comparable with the results of linear models in simulation.

Simple 2-D aerofoil models and more complex aerofoil models with trailing edge flaps are analysed in the NVS. Helicopter rotor segments can even be measured in a scale of 1:1, and simulations can be performed with realistic frequencies on cyclic pitch motions through to dynamic stall.

An upgrade of the setup also permits analysis of 3-D half models clamped in on one side – for instance UAV structures and helicopter blade tips. What makes this system special is that a large section of the wind tunnel wall can also be moved similar to a turntable, thus ensuring that, despite external drive and shaft, there is no gap between the wall of the wind tunnel and the model. The modular structure ensures that vital parts of the NVS, such as hydraulics, bearings and piezoelectric sensors, can be used in both configurations.


Contact
Dr. rer. nat Holger Mai
Head of Aeroelastic Experiments

German Aerospace Center

Institute of Aeroelasticity

Göttingen

Tel.: +49 551 709-2481

Fax: +49 551 709-2862

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