Free Vortex Wake within AeroDyn15 #447
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Remove Interpolation.f90
Used MOVE_ALLOC to move from InitInp to u% The WingsMesh now exactly follows the u_AD%BladeMotion mesh
This will reduce merge conflicts with PR OpenFAST#373
NOT WORKING YET!!!!
Still need to update baselines (after PR 373 gets merged in)
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Merged the Items to address after merging:
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CpMin Pressure coefficient SgCav Cavitation number SigCr Critical cavitation number Gam Gamma -- circulation on blade Cl_Static Static portion of lift force coefficient at each node, without unsteady effects Cd_Static Static portion of drag force coefficient at each node, without unsteady effects Cm_Static Static portion of pitching moment coefficient at each node, without unsteady effects Uin Axial induction in hub coordinates (polar rotating) rotor plane polar hub rotating coordinates Uit Tangential induction in hub coordinates (polar rotating) rotor plane polar hub rotating coordinates Uir Radial induction in hub coordinates (polar rotating) rotor plane polar hub rotating coordinates
This was referenced Jul 20, 2020
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Feature or improvement description
This pull request adds a free vortex wake module to OpenFAST in AD15. Features included:
Other updates unrelated to vortex wake
Impacted areas of the software
Existing AD15 simulations are unrelated
Additional supporting information
Wake visualization examples, showing the near wake consisting of multiple vortex lattice elements and the far wake consisting of a root and tip vortex only :
Comparison of normal and tangential forces (
F_n,F_t), and blade root bending moments (M_y), using the free vortex wake (FVW), or Blade Element Momentum (BEM), against measurements for the DanAero turbine under 38 degree yaw:Test results, if applicable
A unit test was also included.