A new concept to determine the mass distribution of an active twist rotor blade

Author:

Schulz Martin,Opitz Steffen,Riemenschneider Johannes

Publisher

Springer Science and Business Media LLC

Subject

Aerospace Engineering,Transportation

Reference12 articles.

1. Opitz, S., Riemenschneider, J., Monner, H.P.: Modal investigation of an active twist helicopter rotor blade. In: ICAST—International Conference on adaptive Structures and Technologies. Hong Kong, China (2009)

2. Riemenschneider, J., Opitz, S., Wierach, P., des Rochettes, H.M., Buchaniek, L., Joly, D.: Structural design and testing of active twist blades—a comparison. In: ERF—European Rotorcraft Forum. Hamburg, Germany (2009)

3. Hoffmann, F., Opitz, S., Riemenschneider, J.: Validation of active twist modeling based on whirl tower tests. In: AHS—American Helicopter Society. Texas, USA (2009)

4. Monner, H.P., Opitz, S., Riemenschneider, J., Wierach, P.: Evolution of active twist rotor designs at dlr. In: AIAA/ASME/AHS Adaptive Structures Conference. Schaumburg, IL, USA (2008)

5. Wierach, P., Riemenschneider, J., Opitz, S., Hoffmann, F.: Experimental investigation of an active twist rotor under centrifugal loads. In: ERF—European Rotorcraft Forum. Kazan, Russia (2007)

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