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Advanced Rotary Wing Aeromechanics

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High Performance Computing in Science and Engineering’ 05

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Abstract

This paper presents recent developments and results in the aerodynamic and aeroelastic simulation of helicopter main rotors. Our current work focusses on two aspects which are of high relevance for the further improvement of helicopter rotors: The aeroelastic simulation of active rotor concepts and the correct reproduction and prediction of Blade Vortex Interaction.

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References

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Author information

Authors and Affiliations

  1. Institut für Aerodynamik und Gasdynamik (IAG), Universität Stuttgart, Pfaffenwaldring 21, 70550, Stuttgart, Germany

    M. Dietz, M. Kessler & E. Krämer

Authors
  1. M. Dietz
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  2. M. Kessler
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  3. E. Krämer
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Editor information

Editors and Affiliations

  1. Zentrum für Informationsdienste und Hochleistungsrechnen (ZIH), Technische Universität Dresden, Zellescher Weg 12-14, 01169, Dresden, Germany

    Wolfgang E. Nagel

  2. Höchstleistungsrechenzentrum Stuttgart (HLRS), Universität Stuttgart, Nobelstraße 19, 70569, Stuttgart, Germany

    Michael Resch

  3. Interdisziplinäres Zentrum für Wissenschaftliches Rechnen (IWR), Universität Heidelberg, Im Neuenheimer Feld 368, 69120, Heidelberg, Germany

    Willi Jäger

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© 2006 Springer-Verlag Berlin Heidelberg

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Dietz, M., Kessler, M., Krämer, E. (2006). Advanced Rotary Wing Aeromechanics. In: Nagel, W.E., Resch, M., Jäger, W. (eds) High Performance Computing in Science and Engineering’ 05. Springer, Berlin, Heidelberg. https://doi.org/10.1007/3-540-29064-8_15

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