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What issue does this research address? The calcula)on of dynamic load cases for a wind turbine opera)ng in an offshore array, including both the structural and aerodynamic response to unsteady flow condi)ons. Dr Geoff Dutton 1 , David Hankin 1,2 & Professor J. Michael R. Graham 2 1 STFC Rutherford Appleton Laboratory; 2 Imperial College London What method does this research use? The developed model couples an unsteady formula)on of the vortex la>ce panel method, developed at Imperial College London, with a structural dynamic blade model , developed using Abaqus at STFCRAL, to enable soHcoupled fully unsteady aeroelas)c simula)ons. An integrated wake/rotor model David Hankin +44 (0)1235 445 785 [email protected] geoff[email protected] +44 (0)1235 445 823 Dr Geoff Du0on What results were found? The two models have been successfully linked. However there exists an instability in the torque moment. An itera)ve restart posi)on has been implemented to ensure the forces and displacements in both models are converged at the start of the simula)on, but the instability is only delayed rather than removed. Comparison with the original quasisteady 2D aerodynamics shows reasonable agreement prior to the instability. Spectral analysis indicates that the principle difference is in the 2 nd flap and 1 st torsional modes. What is the impact of this research to the wind industry? The combined aeroelas)c model can be used by wind farm developers to inves)gate dynamic load cases during the design of new wind turbines. Professor J. Michael R. Graham +44 (0)207 594 5074 [email protected]

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Page 1: An integrated wake/rotor model - Just another WordPress site · 1STFC Rutherford Appleton Laboratory; 2Imperial College London ... The$ developed$ model$ couples$ an$ unsteady$ formulaon$

What issue does this research

address? The  calcula)on  of  dynamic  load  cases  for  a  wind  turbine  opera)ng   in  an  offshore  array,   including  both  the  structural  and  aerodynamic  response  to  unsteady    flow  condi)ons.  

Dr Geoff Dutton1, David Hankin1,2 & Professor J. Michael R. Graham2 1STFC Rutherford Appleton Laboratory; 2Imperial College London

What method does this research use? The   developed   model   couples   an   unsteady  formula)on   of   the   vortex   la>ce   panel   method,  developed   at   Imperial   College   London,   with   a  structural  dynamic  blade  model  ,  developed  using  Abaqus   at   STFC-­‐RAL,   to   enable   soH-­‐coupled   fully  unsteady  aeroelas)c  simula)ons.  

An integrated wake/rotor model

David  Hankin  +44  (0)1235  445  785  

[email protected]  

[email protected]    +44  (0)1235  445  823  Dr  Geoff  Du0on  

What results were found? The   two   models   have   been   successfully   linked.  However  there  exists  an  instability  in  the  torque  moment.   An   itera)ve   restart   posi)on   has   been  implemented   to   ensure   the   forces   and  displacements   in   both  models   are   converged   at  the   start   of   the   simula)on,  but   the   instability   is  only  delayed  rather  than  removed.                      Comparison   with   the   original   quasi-­‐steady   2D  aerodynamics  shows  reasonable  agreement  prior  to  the  instability.    Spectral  analysis  indicates  that  the  principle  difference   is   in   the  2nd  flap  and  1st  torsional  modes.                        

What is the impact of this research to the wind industry? The  combined  aeroelas)c  model  can  be  used  by  wind   farm   developers   to   inves)gate   dynamic  load   cases   during   the   design   of   new   wind  turbines.  

Professor  J.  Michael  R.  Graham  +44  (0)207  594  5074  [email protected]