Dear all,
I am also trying to couple spar OC3-Hywind with DTU10MW RWT. During this try I got the following error. Could you please help to interpret it in order to be able to run this simulation.
OpenFAST
Copyright (C) National Renewable Energy Laboratory
Copyright (C) Envision Energy USA LTD
This program is licensed under Apache License Version 2.0 and comes with ABSOLUTELY NO WARRANTY.
See the “LICENSE” file distributed with this software for details.
OpenFAST-v2.3.0
Compile Info:
- Architecture: 32 bit
- Precision: single
- Date: Apr 03 2020
- Time: 14:10:27
Execution Info:
- Date: 08/18/2020
- Time: 11:31:25+0200
OpenFAST input file heading:
------- FAST model for DTU 10MW RWT mounted on spar-buoy from OC3-Hywind project ---------
Running ElastoDyn.
Running AeroDyn14.
Running InflowWind.
Reading a 33x33 grid (200 m wide, 9.99451E-03 m to 229 m above ground) with a characteristic
wind speed of 5 m/s. This full-field file was generated by TurbSim (v1.06.00, 21-Sep-2012) on
18-Aug-2020 at 11:07:00.
Processed 108800 time steps of 20-Hz full-field data (5440 seconds).
Running ServoDyn.
Running ServoDyn Interface for Bladed Controllers.
Running HydroDyn.
Generating incident wave kinematics and current time history.
Reading in WAMIT output with root name “.../Platform/Spar”.
Computing radiation impulse response functions and wave diffraction forces.
Running MoorDyn.
Creating mooring system. 3 fairleads, 3 anchors, 0 connects.
Finalizing ICs using dynamic relaxation.
t=19.001 FairTen 1: 9.10157E+05, 9.10661E+05, 9.10842E+05
Fairlead tensions converged to 0.1% after 19.001 seconds.
Basic DTU Wind Energy Controller (ver. 1.5) loaded…
PIDvar%outres= NaN
PIDvar%outpro= -1.41192486796464
PIDvar%outdif= NaN
dt= 0.000000000000000E+000
PIDvar%error1_old(1)= 0.000000000000000E+000
error(1)= -1.00500000000000
PIDvar%Kdif(1)= 0.000000000000000E+000
Padded_term= 0.000000000000000E+000
PIDvar%outset= 0.000000000000000E+000
FAST_Solution:CalcOutputs_And_SolveForInputs:SolveOption2:AD14_CalcOutput:AeroDyn was designed
for an explicit-loose coupling scheme. Using last calculated values from AeroDyn on all
subsequent calls until time is advanced. Warning will not be displayed again.
SolveOption2:SrvD_CalcOutput:BladedInterface option was designed for an explicit-loose coupling
scheme. Using last calculated values from DLL on all subsequent calls until time is advanced.
Warning will not be displayed again.
WARNING: High VNB velocity encountered during induction factor calculation.
Blade number 1, Element number 21
VNW = 4.553, VNB = -116.28
WARNING: High VNB velocity encountered during induction factor calculation.
Blade number 1, Element number 22
VNW = 4.3429, VNB = -131.54
WARNING: High VNB velocity encountered during induction factor calculation.
Blade number 1, Element number 23
VNW = 4.0304, VNB = -143.13
WARNING: High VNB velocity encountered during induction factor calculation.
Blade number 1, Element number 24
VNW = 3.7313, VNB = -151.71
WARNING: High VNB velocity encountered during induction factor calculation.
Blade number 1, Element number 25
VNW = 3.6599, VNB = -154.58
WARNING: Induced velocity warning written 5 times. The message will not be repeated, though
the condition may persist.
FAST_Solution:FAST_AdvanceStates:ED_ABM4:ED_CalcContStateDeriv:SetCoordSy:Small angle assumption
violated in SUBROUTINE SmllRotTrans() due to a large tower deflection (ElastoDyn SetCoordSy). The
solution may be inaccurate. Simulation continuing, but future warnings from SmllRotTrans() will
be suppressed.
Additional debugging message from SUBROUTINE SmllRotTrans(): 0.375 s
FAST_Solution:CalcOutputs_And_SolveForInputs:SolveOption2:AD14_CalcOutput:ELEMFRC:BeddoesModel:ATT
ACH: Blade #1 element #20 is supersonic! Other elements are likely supersonic as well.
Supersonic mach nos. will be set to 0.7 to attempt continuation.
AD14_CalcOutput:ELEMFRC:BeddoesModel:ATTACH: Supersonic condition has subsided with Blade #1
element #33.
AD14_CalcOutput:ELEMFRC:BeddoesModel:ATTACH: Blade #2 element #23 is supersonic! Other elements
are likely supersonic as well. Supersonic mach nos. will be set to 0.7 to attempt continuation.
AD14_CalcOutput:ELEMFRC:BeddoesModel:ATTACH: Supersonic condition has subsided with Blade #3
element #4.
AD14_CalcOutput:ELEMFRC:BeddoesModel:ATTACH: Blade #3 element #20 is supersonic! Other elements
are likely supersonic as well. Supersonic mach nos. will be set to 0.7 to attempt continuation.
AD14_CalcOutput:ELEMFRC:BeddoesModel:SEPAR: Angle of attack = -6.15209E+10 is outside table.
FAST encountered an error at simulation time 0.375 of 5400 seconds.
Simulation error level: FATAL ERROR
Aborting OpenFAST.
Thank you in advance.
Best regards,
Ioannis.
EDIT: Is there any possibility this issue to be related to wind speed grid?