Three dimensionality and Instabilities of Leading-Edge Vortices

Lead Research Organisation: Imperial College London
Department Name: Aeronautics

Abstract

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Publications

10 25 50
 
Description We have investigated the fundamental flow dynamics of how the leading edge vortex on a plunging wing is formed and evolves for different oscillatory frequencies of the plunging wing. We have in particular established how the vortex is formed near the tip of the wing which helps us understand the how this region can generate lift under plunigng conditions. This type of dynmaics information is useful in understanding animal flow dynaimcs with potential application to unanned aircarft and wind turbines.
Exploitation Route We have published this work in the academic literature and reported it at international conferences and seminars
Sectors Aerospace, Defence and Marine,Energy

 
Description We have discussed the results with our industrial collaborators at McLaren Racing who are interested in adopting the software.
First Year Of Impact 2001
Sector Transport
 
Description McLaren Racing 
Organisation McLaren Racing
Country United Kingdom 
Sector Private 
PI Contribution We have transferred fundamental ideas behind vortex stability and identification to their design practice. More recently we are been applying computational modelling tools developed in an academic setting to example flow problems of direct interest to McLaren.
Collaborator Contribution Data and motivation on how to focus our research direction
Impact .
Start Year 2007
 
Title Nektar++ v5.0.1 
Description A tensor product based finite element package designed to allow one to construct efficient classical low polynomial order h-type solvers (where h is the size of the finite element) as well as higher p-order piecewise polynomial order solvers. 
Type Of Technology Software 
Year Produced 2021 
Open Source License? Yes  
Impact The latest version of Nektar++, v5.0.1, was released on the 21st January 2021. It can be downloaded from the downloads page. 
 
Description "Numerical simulation and experiment of the three-dimensional leading-edge vortex generated by a plunging wing" at The 13th International ERCOFTAC symposium on Engineering, Turbulence, Modelling and Measurements (ETMM13). 
Form Of Engagement Activity A talk or presentation
Part Of Official Scheme? No
Geographic Reach International
Primary Audience Postgraduate students
Results and Impact Gao, A. K., Cantwell, C. D., Sherwin, S. J., Son, O., Wang, Z., & Gursul, I. (2021, September). Numerical simulation and experiment of the three-dimensional leading-edge vortex generated by a plunging wing. In The 13th International ERCOFTAC symposium on Engineering, Turbulence, Modelling and Measurements (ETMM13).
Year(s) Of Engagement Activity 2021
URL https://etmm.ercoftac.org/etmm/past-etmm-conference/etmm-13-in-rhodes-20/
 
Description Three-dimensional instabilities of vortices shed from a plunging wing: Computations. In APS Division of Fluid Dynamics Meeting (2020) 
Form Of Engagement Activity A talk or presentation
Part Of Official Scheme? No
Geographic Reach International
Primary Audience Postgraduate students
Results and Impact Gao, A. K., Sherwin, S. J., & Cantwell, C. D. (2020). Three-dimensional instabilities of vortices shed from a plunging wing: Computations. In APS Division of Fluid Dynamics Meeting Abstracts (pp. P19-005).
Year(s) Of Engagement Activity 2020