Atkin, C. J. ORCID: https://orcid.org/0000-0003-2529-1978
(2014)
Convergence of calculated transition loci during computational analysis of transonic aerofoils and infinite swept wings.
In:
29th Congress of the International Council of the Aeronautical Sciences, ICAS 2014.
29th Congress of the International Council of the Aeronautical Sciences, ICAS 2014
.
International Council of the Aeronautical Sciences, SUN.
ISBN 3932182804
Abstract
The effect of intermittent re-calculation of transition position is analysed using a low-order VII platform coupled to an Orr-Sommerfeld-type stability analysis method. Transonic aerofoil and infinite-swept wing flows were studied. Where the transition mechanisms are weakly dependent on the gross flow field characteristics, as few as ten transition updates may be required over a 1000- iteration CFD solution, if correctly timed.
Item Type: | Book Section |
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Uncontrolled Keywords: | cfd,transition modelling,aerospace engineering,control and systems engineering,electrical and electronic engineering,materials science(all) ,/dk/atira/pure/subjectarea/asjc/2200/2202 |
Related URLs: | |
Depositing User: | LivePure Connector |
Date Deposited: | 29 May 2020 23:33 |
Last Modified: | 22 Oct 2022 23:52 |
URI: | https://ueaeprints.uea.ac.uk/id/eprint/75391 |
DOI: |
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