Embedded large eddy simulation of transitional flow over NACA0012 aerofoil
- Submitting institution
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Kingston University
- Unit of assessment
- 12 - Engineering
- Output identifier
- 12-063-1618
- Type
- D - Journal article
- DOI
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10.1177/0954410020939797
- Title of journal
- Proceedings of the Institution of Mechanical Engineers, Part G, Journal of Aerospace Engineering
- Article number
- -
- First page
- 0
- Volume
- 0
- Issue
- -
- ISSN
- 0954-4100
- Open access status
- Compliant
- Month of publication
- -
- Year of publication
- 2020
- URL
-
-
- Supplementary information
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- Request cross-referral to
- -
- Output has been delayed by COVID-19
- No
- COVID-19 affected output statement
- -
- Forensic science
- No
- Criminology
- No
- Interdisciplinary
- No
- Number of additional authors
-
-
- Research group(s)
-
-
- Proposed double-weighted
- No
- Reserve for an output with double weighting
- No
- Additional information
- An accurate computation of near-field unsteady turbulent flow around aerofoil is of outstanding importance for aerofoil trailing edge noise source capture, thus for the airframe near-field and far-field noise prediction in modern commercial aircraft. This work is significant because a high-fidelity embedded larger eddy simulation method is successfully implemented for a transitional boundary layer flow in the first time, in order to provide a computationally efficient approach for aeroacoustic simulation with sufficient accuracy, which has been proved to be a promising approach for industrial flow involving wall boundary layer in aerospace engineering application.
- Author contribution statement
- -
- Non-English
- No
- English abstract
- -
