Accurate Predictions of Hovering Rotor Flows Using CFD

Jimenez Garcia, A., Colonia, S. and Barakos, G. N. (2017) Accurate Predictions of Hovering Rotor Flows Using CFD. In: 55th AIAA Aerospace Sciences Meeting, AIAA SciTech Forum, (AIAA 2017-1666), Grapevine, TX, USA, 9-13 Jan 2017, ISBN 9781624104473 (doi: 10.2514/6.2017-1666)

133675.pdf - Accepted Version



With work on the S-76 rotor providing encouraging results regarding the prediction of integral loads with CFD in hover, the XV-15 rotor is now analysed. Fully turbulent and transitional results are obtained showing the capability of modern CFD methods. The transition onset and distribution of skin friction are well predicted and were found to have a mild effect on the overall figure of merit. This work also shows the potential of transport-based models for transition prediction in complex 3D flows. Finally, hover simulations for the PSP blade are also shown in terms of surface pressure coefficient and wake visualisation.

Item Type:Conference Proceedings
Additional Information:The use of the cluster Chadwick of the University of Liverpool is gratefully acknowledged. Some results were obtained using the EPSRC funded ARCHIE-WeSt High Performance Computer (www.archie-west., EPSRC grant no. EP/K000586/1. Part of this work is funded under the HiperTilt Project of the UK Technology Strategy Board (TSB) and Leonardo Helicopters under Contract Nr. 101370.
Glasgow Author(s) Enlighten ID:Barakos, Professor George and Jimenez Garcia, Mr Antonio and Colonia, Mr Simone
Authors: Jimenez Garcia, A., Colonia, S., and Barakos, G. N.
College/School:College of Science and Engineering > School of Engineering > Autonomous Systems and Connectivity
Copyright Holders:Copyright © 2017 The Authors
First Published:First published in 55th AIAA Aerospace Sciences Meeting Proceedings 2017
Publisher Policy:Reproduced in accordance with the publisher copyright policy

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