Comparison of RANS, DES and DDES Results for ONERA M-6 Wing at Transonic Flow Speed Using an In-House Parallel Code

Durrani, N. and Qin, N. (2011) Comparison of RANS, DES and DDES Results for ONERA M-6 Wing at Transonic Flow Speed Using an In-House Parallel Code. In: 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, 4-7 January 2011, Orlando, Florida (2011). AIAA 2011-190 . American Institute of Aeronautics and Astronautics . ISBN 978-1-60086-950-1

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Authors/Creators:
  • Durrani, N.
  • Qin, N.
Copyright, Publisher and Additional Information: © 2011 American Institute of Aeronautics and Astronautics. Reproduced in accordance with the publisher's self-archiving policy.
Dates:
  • Published: January 2011
Institution: The University of Sheffield
Academic Units: The University of Sheffield > Faculty of Engineering (Sheffield) > Department of Mechanical Engineering (Sheffield)
Depositing User: Symplectic Sheffield
Date Deposited: 09 Oct 2015 13:51
Last Modified: 09 Oct 2015 13:51
Published Version: http://arc.aiaa.org/doi/abs/10.2514/6.2011-190
Status: Published
Publisher: American Institute of Aeronautics and Astronautics
Series Name: AIAA 2011-190
Identification Number: https://doi.org/10.2514/6.2011-190

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