Discrete-vortex method with novel shedding criterion for unsteady airfoil flows with intermittent leading-edge vortex shedding
- Submitting institution
-
University of Glasgow
- Unit of assessment
- 12 - Engineering
- Output identifier
- 12-04479
- Type
- D - Journal article
- DOI
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10.1017/jfm.2014.297
- Title of journal
- Journal of Fluid Mechanics
- Article number
- -
- First page
- 500
- Volume
- 751
- Issue
- -
- ISSN
- 0022-1120
- Open access status
- Out of scope for open access requirements
- Month of publication
- July
- Year of publication
- 2014
- URL
-
http://eprints.gla.ac.uk/99370/
- Supplementary information
-
-
- 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
-
4
- Research group(s)
-
-
- Proposed double-weighted
- No
- Reserve for an output with double weighting
- No
- Additional information
- The Leading Edge Suction Parameter enables low order prediction and modelling of vortex dominated flows such as those seen in dynamic stall, gust encounters and tiltrotor transition. The work has been highlighted as a breakthrough (https://www.annualreviews.org/doi/abs/10.1146/annurev-fluid-010518-040334 and led to EPSRC funding (EP/R008035/1, https://gow.epsrc.ukri.org/NGBOViewGrant.aspx?GrantRef=EP/R008035/1, £100,770) as well as an invited lecture for Kiran at AIAA Scitech 2019 Meeting of Massively Separated Flows.
- Author contribution statement
- -
- Non-English
- No
- English abstract
- -
