UNSflow: A low-order, open-source solver for problems that involve unsteady and nonlinear fluid dynamics
Lead Research Organisation:
University of Glasgow
Department Name: School of Engineering
Abstract
This project aims to derive and develop new theoretical and low-cost numerical methods for analysing general unsteady aerofoil and wing flows that may exhibit nonlinearities such as flow separation and vortex shedding. The solvers implemented through these methods will be made available (open-source) to the public, academia and industry through the UNSflow project.
Unsteady fluid dynamics is ubiquitous in modern aerospace research problems such as aerodynamic optimisation of wind-energy harvesting devices, design of flapping wing fliers, use of flapping foils for propulsion/high-lift, and design of aircraft with flexible wings (such as HALE - High-Altitude Long Endurance, or futuristic aircraft with large aspect ratios). Reducing emissions of pollutants and greenhouse gases, which is the prime motivation behind many of these problems, can only be accomplished by a mix of renewable strategies and incremental improvements. The flow physics in these problems exhibits significant nonlinearities arising from flow separation and vortex shedding which cannot be adequately represented by closed-form theoretical formulations. Though computational fluid dynamics (CFD) and experimental methods have contributed much to the understanding of unsteady flow features, they are unsuitable for use in preliminary design and optimisation because of time and cost considerations. This project aims to develop low-cost, physics-based models for unsteady aerodynamics based on the discrete-vortex method, which will enable fast simulations of medium-fidelity, and provide a simple framework for parametric studies, design optimisation, real-time simulation and interdisciplinary studies (by coupling with other solvers).
UNSflow intends to be a new class of low-cost solvers that sacrifice an acceptable level of accuracy in fluid simulations for a tremendous speedup in simulation time, while being fully physics-based and retaining the fundamental flow quantities. The guiding philosophy in development of the solver is to retain only the physics which are significant in the flow regimes of specific applications. They are hence not an alternative to high-fidelity CFD and experiments, which will still be needed in the final phases of industrial production, but for fewer ideas/concepts. In effect, this will lead to reduced time and cost in the design cycle, and perhaps even a better solution in the long run, because more exploration of the design space will be possible. This research also intends to support the activities of teachers, students and hobbyists who may not have access to CFD software and computing resources. Potential applications for this class of users include design of ornithopters, quadcopters, and home-made wind-energy harvesting devices.
The research to be carried out in this project is fundamental in nature and underpins several applied problems. It is intended to derive new theoretical and numerical tools to study general unsteady flows with intermittent separation and reattachment. It will assist the principal investigator's research group in its research on applied problems such as aerodynamic optimisation, dynamic stall alleviation, flapping-wing design and wind-energy harvesting. The research will also be useful to other research groups working on unsteady flows (for both fundamental and applied research), as a preliminary design/analysis tool for various applications, and student projects.
Unsteady fluid dynamics is ubiquitous in modern aerospace research problems such as aerodynamic optimisation of wind-energy harvesting devices, design of flapping wing fliers, use of flapping foils for propulsion/high-lift, and design of aircraft with flexible wings (such as HALE - High-Altitude Long Endurance, or futuristic aircraft with large aspect ratios). Reducing emissions of pollutants and greenhouse gases, which is the prime motivation behind many of these problems, can only be accomplished by a mix of renewable strategies and incremental improvements. The flow physics in these problems exhibits significant nonlinearities arising from flow separation and vortex shedding which cannot be adequately represented by closed-form theoretical formulations. Though computational fluid dynamics (CFD) and experimental methods have contributed much to the understanding of unsteady flow features, they are unsuitable for use in preliminary design and optimisation because of time and cost considerations. This project aims to develop low-cost, physics-based models for unsteady aerodynamics based on the discrete-vortex method, which will enable fast simulations of medium-fidelity, and provide a simple framework for parametric studies, design optimisation, real-time simulation and interdisciplinary studies (by coupling with other solvers).
UNSflow intends to be a new class of low-cost solvers that sacrifice an acceptable level of accuracy in fluid simulations for a tremendous speedup in simulation time, while being fully physics-based and retaining the fundamental flow quantities. The guiding philosophy in development of the solver is to retain only the physics which are significant in the flow regimes of specific applications. They are hence not an alternative to high-fidelity CFD and experiments, which will still be needed in the final phases of industrial production, but for fewer ideas/concepts. In effect, this will lead to reduced time and cost in the design cycle, and perhaps even a better solution in the long run, because more exploration of the design space will be possible. This research also intends to support the activities of teachers, students and hobbyists who may not have access to CFD software and computing resources. Potential applications for this class of users include design of ornithopters, quadcopters, and home-made wind-energy harvesting devices.
The research to be carried out in this project is fundamental in nature and underpins several applied problems. It is intended to derive new theoretical and numerical tools to study general unsteady flows with intermittent separation and reattachment. It will assist the principal investigator's research group in its research on applied problems such as aerodynamic optimisation, dynamic stall alleviation, flapping-wing design and wind-energy harvesting. The research will also be useful to other research groups working on unsteady flows (for both fundamental and applied research), as a preliminary design/analysis tool for various applications, and student projects.
Planned Impact
The current dependency on fossil fuels and associated climate change is the most urgent threat of our times, and is a global problem with environmental, socio-economic and geo-political ramifications. As the rate of global energy consumption is only expected to increase, novel, interdisciplinary and international collaborations are necessary, involving leaders from diverse fields such as scientists, politicians and investors. Replacement of coal, oil and gas in the generation of electric power is unlikely to be achieved through any one technology, and instead requires a mix of renewable strategies. The research proposed herein, by developing novel low-order models for unsteady fluid problems, aims to tackle this problem on two fronts - by developing methods that enable higher efficiencies in aerial transport, and by enabling the design and optimisation of wind/water energy harvesting devices.
Unsteady flow physics are prevalent in many forms of modern aerial transport. High-Altitude Long Endurance (HALE) aircraft are intended to be systems powered by renewable energy, used for observations, communications, reconnaissance and even for providing internet access in remote areas. These aircraft have long, flexible wings which undergo large deformations, fluid-structure interaction, and require a complete rethink of control laws and systems. Helicopter efficiency is highly influenced by the dynamic stall phenomenon, which involves flow separation and vortex shedding, and is a classical problem in unsteady aerodynamics. Unmanned aircraft which undergo sharp manoeuvres, and novel concept such as micro-air vehicles based on flapping wings, also require unsteady aerodynamics modelling. Even in conventional aircraft wings, the trend is increasing aspect ratio and flexibility with the use of the composites. The transport industry has historically been conservative in adopting innovations and the integration of any novelty undergoes a lengthy and expensive process. Advances in modelling and simulation and the availability of multi-fidelity tools for unsteady aerodynamics could mitigate this cost significantly.
Wind energy harvesters of all configurations, such as horizontal-axis, vertical-axis and piezoelectric flapping-foil generators (which harvest energy using the phenomenon of aerodynamic flutter) involve unsteady aerodynamic phenomena which affect their performance. Optimisation of these harvesters, and using them optimally in various scenarios (urban, farmland, etc.) requires parametric studies spanning a large number of design variables for which the current research provides functionality.
Finally, this research and its outputs will have academic and entrepreneurial/innovation impact. As an open-source tool that facilitates simple coupling with other solvers to tackle multidisciplinary problems, UNSflow will be (and is being) employed by academics for fundamental studies on vortex flow structures and flow separation, and for teaching. It is worth noting that significant inventions and advances in technology have arisen from private innovators and entrepreneurs, hobbyists and small industries. These groups typically lack access to CFD tools, supercomputers and experimental facilities, and will hence benefit from models that could be used to test new concepts and designs. This research aims to develop new theoretical and numerical methods in unsteady fluid dynamics, incorporate these in software, and make them freely available to the public.
Unsteady flow physics are prevalent in many forms of modern aerial transport. High-Altitude Long Endurance (HALE) aircraft are intended to be systems powered by renewable energy, used for observations, communications, reconnaissance and even for providing internet access in remote areas. These aircraft have long, flexible wings which undergo large deformations, fluid-structure interaction, and require a complete rethink of control laws and systems. Helicopter efficiency is highly influenced by the dynamic stall phenomenon, which involves flow separation and vortex shedding, and is a classical problem in unsteady aerodynamics. Unmanned aircraft which undergo sharp manoeuvres, and novel concept such as micro-air vehicles based on flapping wings, also require unsteady aerodynamics modelling. Even in conventional aircraft wings, the trend is increasing aspect ratio and flexibility with the use of the composites. The transport industry has historically been conservative in adopting innovations and the integration of any novelty undergoes a lengthy and expensive process. Advances in modelling and simulation and the availability of multi-fidelity tools for unsteady aerodynamics could mitigate this cost significantly.
Wind energy harvesters of all configurations, such as horizontal-axis, vertical-axis and piezoelectric flapping-foil generators (which harvest energy using the phenomenon of aerodynamic flutter) involve unsteady aerodynamic phenomena which affect their performance. Optimisation of these harvesters, and using them optimally in various scenarios (urban, farmland, etc.) requires parametric studies spanning a large number of design variables for which the current research provides functionality.
Finally, this research and its outputs will have academic and entrepreneurial/innovation impact. As an open-source tool that facilitates simple coupling with other solvers to tackle multidisciplinary problems, UNSflow will be (and is being) employed by academics for fundamental studies on vortex flow structures and flow separation, and for teaching. It is worth noting that significant inventions and advances in technology have arisen from private innovators and entrepreneurs, hobbyists and small industries. These groups typically lack access to CFD tools, supercomputers and experimental facilities, and will hence benefit from models that could be used to test new concepts and designs. This research aims to develop new theoretical and numerical methods in unsteady fluid dynamics, incorporate these in software, and make them freely available to the public.
People |
ORCID iD |
Kiran Kumar Ramesh (Principal Investigator) |
Publications
Bird H
(2021)
Unsteady lifting-line theory and the influence of wake vorticity on aerodynamic loads
in Theoretical and Computational Fluid Dynamics
Bird H
(2022)
Usefulness of Inviscid Linear Unsteady Lifting-Line Theory for Viscous Large-Amplitude Problems
in AIAA Journal
Bird H
(2022)
Applying Frequency-Domain Unsteady Lifting-Line Theory to Time-Domain Problems
in AIAA Journal
Ramesh K
(2020)
On the leading-edge suction and stagnation-point location in unsteady flows past thin aerofoils
in Journal of Fluid Mechanics
Description | 1. In this research project, we have developed a set of theoretical and numerical approaches which provide the groundwork for modelling complex unsteady flows with a much lower cost (in terms of time and resources) than CFD. These are: (i) Unsteady thick-airfoil theory - provides a 2D potential flow solution for thick geometries undergoing arbitrary motion. (ii) Integral boundary-layer solver - calculates the effective airfoil shape due to boundary layer displacement and predicts the occurrence of BL detachment. (iii) Large-angle unsteady lifting line theory - provides a 3D potential for solution for geometries undergoing arbitrary motion 2. A bespoke CFD solver (for Euler and Navier-stokes equations) based on OpenFOAM was developed to study 3D unsteady flows and aid the modelling approaches. New postprocessing techniques to derive the boundary layer displacement and edge velocity distribution were developed. 3. Theoretical developments were made in research questions that popped up during the course of the project. A paper was published on using asymptotic matching to derive the leading edge suction at the leading edge and hence a criterion for LeV formation. 4. Many new research contacts were made while presenting the project objectives and outcomes. Prominent among these is Dr. Karen Mulleners who leads the Unsteady flow disgnostivs lab at EPFL. Collaboration is ongoing and partnership is planned for projects in the future. |
Exploitation Route | Publications on the research outcomes mentioned above will appear in print over the course of this year and the next. These will be of use to academics and researchers working on problems involving unsteady aerodynamics. An open source software package UnsteadyFlowSolvers.jl has been published, which may be used by academics, students, industry and hobbyists for solving simulation, control and design problems. Even in the short duration that the package has been online, it has attracted the interest of prominent researchers working on unsteady fluid dynamics. The Github package currently has 5 contributors and has been forked over 10 times. |
Sectors | Aerospace, Defence and Marine,Energy |
Description | Internal call for EPSRC DTA scholarships |
Amount | £93,000 (GBP) |
Organisation | Engineering and Physical Sciences Research Council (EPSRC) |
Sector | Public |
Country | United Kingdom |
Start | 10/2018 |
End | 06/2022 |
Description | Theoretical, Numerical and Experimental study of unsteady flows |
Organisation | Swiss Federal Institute of Technology in Lausanne (EPFL) |
Country | Switzerland |
Sector | Public |
PI Contribution | In this collaboration, my research team is working on unsteady fluid dynamics from the theoretical and numerical perspectives. |
Collaborator Contribution | My partners are working on unsteady fluid dynamics in this collaboration from numerical and experimental perspectives. |
Impact | In partnership with Dr. Ignazio Viola from UoE, I hosted a vortex hydrodynamics workshop bringing together researchers working on similar technical problems (despite very different applications). This was conducted from 19-20 September 2019 in UoE. Dr. Ignazio Viola from UoE, Dr. Karen Mulleners from EPFL and I have already presented a paper together at the American Physical Society conference in 2019. A journal article is in progress. |
Start Year | 2018 |
Description | Theoretical, Numerical and Experimental study of unsteady flows |
Organisation | University of Edinburgh |
Country | United Kingdom |
Sector | Academic/University |
PI Contribution | In this collaboration, my research team is working on unsteady fluid dynamics from the theoretical and numerical perspectives. |
Collaborator Contribution | My partners are working on unsteady fluid dynamics in this collaboration from numerical and experimental perspectives. |
Impact | In partnership with Dr. Ignazio Viola from UoE, I hosted a vortex hydrodynamics workshop bringing together researchers working on similar technical problems (despite very different applications). This was conducted from 19-20 September 2019 in UoE. Dr. Ignazio Viola from UoE, Dr. Karen Mulleners from EPFL and I have already presented a paper together at the American Physical Society conference in 2019. A journal article is in progress. |
Start Year | 2018 |
Title | UnsteadyFlowSolvers.jl open-source package |
Description | UnsteadyFlowSolvers.jl (abbreviated as UNSflow) is a library of low-order solvers for unsteady aerodynamics and aeroelasticity. The solvers are written in Julia, are based on the discrete-vortex method and cater to various modern aerospace applications. |
Type Of Technology | Software |
Year Produced | 2019 |
Open Source License? | Yes |
Impact | The code has been forked over 10 times by other researchers who are modifying/using it for their own applications. |
Description | Invited Seminar at AIAA SciTech 2019 |
Form Of Engagement Activity | A talk or presentation |
Part Of Official Scheme? | No |
Geographic Reach | International |
Primary Audience | Postgraduate students |
Results and Impact | I was invited to present on the UNSflow project at a special evening session of the "Massively Separated Flows Discussion Group" at the AIAA SciTech conference 2019 in San Diego. |
Year(s) Of Engagement Activity | 2019 |
Description | Presentations in CARDC |
Form Of Engagement Activity | A talk or presentation |
Part Of Official Scheme? | No |
Geographic Reach | International |
Primary Audience | Postgraduate students |
Results and Impact | Presented on the UNSflow project at a join symposium between UofG and CARDC in China, in Sep 2018 and in Sep 2019. |
Year(s) Of Engagement Activity | 2018,2019 |
Description | Visits by Anna Young and Amanda Smyth |
Form Of Engagement Activity | A talk or presentation |
Part Of Official Scheme? | No |
Geographic Reach | Local |
Primary Audience | Postgraduate students |
Results and Impact | Dr. Anna Young (Lecturer at Bath University) and Dr. Amanda Smyth (Researcher at Cambridge University) visited my institution on separate occasions, presented seminars, discussed common research interests and goals, and interacted with my research group. |
Year(s) Of Engagement Activity | 2019 |
Description | Vortex Hydrodynamics Workshop 2019 |
Form Of Engagement Activity | Participation in an activity, workshop or similar |
Part Of Official Scheme? | No |
Geographic Reach | National |
Primary Audience | Professional Practitioners |
Results and Impact | 30 academics and postgraduate researchers working on topics involving vortex hydrodynamics from all over the UK attended this workshop. The goal was to foster knowledge exchange and cross fertilisation of ideas across different fields and applications. |
Year(s) Of Engagement Activity | 2019 |