Vortex Induced Vibration and Structural Integrity of Deep Water Flexible Risers

Lead Research Organisation: Imperial College London
Department Name: Aeronautics

Abstract

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Publications

10 25 50
 
Description The simulations capability we have produced allows us to model very long oil riser pipes that suffer from a fluid structure interaction known as vortex induced vibration (VIV) that can lead to failure of these pipes due to fatigues. The length of these pipes is very long O(1000D) making the simulation of the full problem intractable. Previous approaches have used a series of 2D slices to represent to hydrodynamics which did not fully capture the 3D anisotropic nature of the fluid flow. We have extended this approach to a "thick" strip method which allows us to capture the local anisotropic nature of the fluid flow but also trivially parallelise the approach to be able to model very long pipes in a tractable timescale.
Exploitation Route At a conference in 2015 I discussion with a representative of the US Airforce about using this technique to model the guide strings on parachutes. In a further invitation to the National University of Singapore in January 2017 I discussed the use of the Thick strip method with Professor Rajeev Jaiman who is extending his codes in vortex induced vibration to include this approach. One researcher, Dr Yan Bao, now has an academic position in Shanghai Jaitong University and continues to develop and promote the technology. Finally we are now part of recent EU-Brazil award focusing on wind engineering where the technology is being applied to understand the fluid structure interaction of a turbine blade when it is parked in a stationary position. This grant started in June 2019 and runs until May 2021.
Sectors Aerospace, Defence and Marine,Environment

 
Description Council of Science and Technology Review on Modelling
Geographic Reach National 
Policy Influence Type Membership of a guideline committee
 
Description ExaFlow
Amount £254,824 (GBP)
Funding ID 671571 
Organisation European Commission 
Sector Public
Country European Union (EU)
Start 11/2015 
End 10/2018
 
Description High-Performance Computing for Wind Energy (HPCWE)
Amount € 1,995,651 (EUR)
Funding ID 828799 1 995 651 
Organisation European Commission H2020 
Sector Public
Country Belgium
Start 06/2019 
End 05/2021
 
Description University of São Paulo 
Organisation Federal University of São Paulo
Country Brazil 
Sector Academic/University 
PI Contribution Researchers at the university of Sao Paulo are using Firedrake for a variety of challenges related to seismic inversion. Dr Ham visited in November 2019 and gave a Firedrake tutorial.
Collaborator Contribution Researchers at the university of Sao Paulo are using Firedrake for a variety of challenges related to seismic inversion. Dr Ham visited in November 2019 and gave a Firedrake tutorial.
Impact Researchers at the university of Sao Paulo are using Firedrake for a variety of challenges related to seismic inversion. Dr Ham visited in November 2019 and gave a Firedrake tutorial.
Start Year 2019
 
Title Nektar++ version 4.0.1 
Description Nektar++ is 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 2014 
Open Source License? Yes  
Impact The software is being used by a number of national and international groups and our web site is currently being visited up to 100 times a day according to google analytics 
URL http://www.nektar.info/downloads/file/nektar-source-tar-gz-2/
 
Title SHARPy: Simulation of High-Aspect-Ratio aircraft and wind turbines in Python 
Description Nonlinear and dynamically linearized models of very flexible aircraft dynamics for design, analysis, and control law synthesis. 
Type Of Technology Software 
Year Produced 2014 
Open Source License? Yes  
Impact It has been used in the aerodynamic and structural design of Facebook's Aquila, Airbus's Zephyr and Astigan Ltd's solar-powered aircraft. 
URL http://www.imperial.ac.uk/aeroelastics/sharpy