May I ask why my power generation is 0

Dear everyone,
I ran my fast model and found that the power generation was 0. I checked servo and elastdyn and did not find any problems. I hope to get everyone’s help. Thank you very much!

------- OpenFAST INPUT FILE ------------------------------------------- 
IEA 15 MW offshore reference model on UMaine VolturnUS-S semi-submersible floating platform
---------------------- SIMULATION CONTROL -------------------------------------- 
False                  Echo        - Echo input data to <RootName>.ech (flag) 
"FATAL"                AbortLevel  - Error level when simulation should abort (string) {"WARNING", "SEVERE", "FATAL"} 
3600                   TMax        - Total run time (s) 
0.01                  DT          - Integration time step (s)  
2                      InterpOrder - Interpolation order for input/output time history (-) {1=linear, 2=quadratic} 
0                      NumCrctn    - Number of correction iterations (-) {0=explicit calculation, i.e., no corrections} 
99999.0                DT_UJac     - Time between calls to get Jacobians (s) 
1000000.0              UJacSclFact - Scaling factor used in Jacobians (-) 
---------------------- FEATURE SWITCHES AND FLAGS ------------------------------ 
      1   CompElast       - Compute structural dynamics (switch) {1=ElastoDyn; 2=ElastoDyn + BeamDyn for blades}  
      0   CompInflow      - Compute inflow wind velocities (switch) {0=still air; 1=InflowWind; 2=external from OpenFOAM} 
      2   CompAero        - Compute aerodynamic loads (switch) {0=None; 1=AeroDyn v14; 2=AeroDyn v15} 
      1   CompServo       - Compute control and electrical-drive dynamics (switch) {0=None; 1=ServoDyn} 
      1   CompHydro       - Compute hydrodynamic loads (switch) {0=None; 1=HydroDyn} 
      0   CompSub         - Compute sub-structural dynamics (switch) {0=None; 1=SubDyn; 2=External Platform MCKF}
      3   CompMooring     - Compute mooring system (switch) {0=None; 1=MAP++; 2=FEAMooring; 3=MoorDyn; 4=OrcaFlex} 
      0   CompIce         - Compute ice loads (switch) {0=None; 1=IceFloe; 2=IceDyn} 
      0   MHK             - MHK turbine type (switch) {0=Not an MHK turbine; 1=Fixed MHK turbine; 2=Floating MHK turbine}
---------------------- ENVIRONMENTAL CONDITIONS --------------------------------
Omitted here, thank you
---------------------- INPUT FILES --------------------------------------------- 
"IEA-15-240-RWT-UMaineSemi_ElastoDyn.dat"    EDFile          - Name of file containing ElastoDyn input parameters (quoted string) 
"../IEA-15-240-RWT/IEA-15-240-RWT_InflowFile.dat"    InflowFile      - Name of file containing inflow wind input parameters (quoted string) 
"IEA-15-240-RWT-UMaineSemi_AeroDyn15.dat"  AeroFile     - Name of file containing aerodynamic input parameters (quoted string) 
"IEA-15-240-RWT-UMaineSemi_ServoDyn.dat"    ServoFile       - Name of file containing control and electrical-drive input parameters (quoted string) 
"IEA-15-240-RWT-UMaineSemi_HydroDyn.dat"      HydroFile       - Name of file containing hydrodynamic input parameters (quoted string) 
"none"                 SubFile         - Name of file containing sub-structural input parameters (quoted string) 
"IEA-15-240-RWT-UMaineSemi_MoorDyn_v2_30mPolyester.dat"      MooringFile     - Name of file containing mooring system input parameters (quoted string) 
"none"                 IceFile         - Name of file containing ice input parameters (quoted string) 

------- SERVODYN v1.05.* INPUT FILE --------------------------------------------
IEA 15 MW offshore reference model on UMaine VolturnUS-S semi-submersible floating platform
---------------------- SIMULATION CONTROL --------------------------------------
False                  Echo        - Echo input data to <RootName>.ech (flag)
"default"              DT          - Communication interval for controllers (s) (or "default")
---------------------- PITCH CONTROL -------------------------------------------
5                      PCMode      - Pitch control mode {0: none, 3: user-defined from routine PitchCntrl, 4: user-defined from Simulink/Labview, 5: user-defined from Bladed-style DLL} (switch)
0.0                    TPCOn       - Time to enable active pitch control (s) [unused when PCMode=0]
9999.9                 TPitManS(1) - Time to start override pitch maneuver for blade 1 and end standard pitch control (s)
9999.9                 TPitManS(2) - Time to start override pitch maneuver for blade 2 and end standard pitch control (s)
9999.9                 TPitManS(3) - Time to start override pitch maneuver for blade 3 and end standard pitch control (s) [unused for 2 blades]
2.0                    PitManRat(1) - Pitch rate at which override pitch maneuver heads toward final pitch angle for blade 1 (deg/s)
2.0                    PitManRat(2) - Pitch rate at which override pitch maneuver heads toward final pitch angle for blade 2 (deg/s)
2.0                    PitManRat(3) - Pitch rate at which override pitch maneuver heads toward final pitch angle for blade 3 (deg/s) [unused for 2 blades]
0.0                    BlPitchF(1) - Blade 1 final pitch for pitch maneuvers (degrees)
0.0                    BlPitchF(2) - Blade 2 final pitch for pitch maneuvers (degrees)
0.0                    BlPitchF(3) - Blade 3 final pitch for pitch maneuvers (degrees) [unused for 2 blades]
---------------------- GENERATOR AND TORQUE CONTROL ----------------------------
5                      VSContrl    - Variable-speed control mode {0: none, 1: simple VS, 3: user-defined from routine UserVSCont, 4: user-defined from Simulink/Labview, 5: user-defined from Bladed-style DLL} (switch)
1                      GenModel    - Generator model {1: simple, 2: Thevenin, 3: user-defined from routine UserGen} (switch) [used only when VSContrl=0]
95.756                 GenEff      - Generator efficiency [ignored by the Thevenin and user-defined generator models] (%)
True                   GenTiStr    - Method to start the generator {T: timed using TimGenOn, F: generator speed using SpdGenOn} (flag)
True                   GenTiStp    - Method to stop the generator {T: timed using TimGenOf, F: when generator power = 0} (flag)
9999.9                 SpdGenOn    - Generator speed to turn on the generator for a startup (HSS speed) (rpm) [used only when GenTiStr=False]
0.0                    TimGenOn    - Time to turn on the generator for a startup (s) [used only when GenTiStr=True]
9999.9                 TimGenOf    - Time to turn off the generator (s) [used only when GenTiStp=True]
---------------------- SIMPLE VARIABLE-SPEED TORQUE CONTROL --------------------
7.559987120819503      VS_RtGnSp   - Rated generator speed for simple variable-speed generator control (HSS side) (rpm) [used only when VSContrl=1]
19624046.66639         VS_RtTq     - Rated generator torque/constant generator torque in Region 3 for simple variable-speed generator control (HSS side) (N-m) [used only when VSContrl=1]
343357.4355671095      VS_Rgn2K    - Generator torque constant in Region 2 for simple variable-speed generator control (HSS side) (N-m/rpm^2) [used only when VSContrl=1]
2.                     VS_SlPc     - Rated generator slip percentage in Region 2 1/2 for simple variable-speed generator control (%) [used only when VSContrl=1]
---------------------- SIMPLE INDUCTION GENERATOR ------------------------------
9999.9                 SIG_SlPc    - Rated generator slip percentage (%) [used only when VSContrl=0 and GenModel=1]
9999.9                 SIG_SySp    - Synchronous (zero-torque) generator speed (rpm) [used only when VSContrl=0 and GenModel=1]
9999.9                 SIG_RtTq    - Rated torque (N-m) [used only when VSContrl=0 and GenModel=1]
9999.9                 SIG_PORt    - Pull-out ratio (Tpullout/Trated) (-) [used only when VSContrl=0 and GenModel=1]
---------------------- THEVENIN-EQUIVALENT INDUCTION GENERATOR -----------------
9999.9                 TEC_Freq    - Line frequency [50 or 60] (Hz) [used only when VSContrl=0 and GenModel=2]
100                    TEC_NPol    - Number of poles [even integer > 0] (-) [used only when VSContrl=0 and GenModel=2]
9999.9                 TEC_SRes    - Stator resistance (ohms) [used only when VSContrl=0 and GenModel=2]
9999.9                 TEC_RRes    - Rotor resistance (ohms) [used only when VSContrl=0 and GenModel=2]
9999.9                 TEC_VLL     - Line-to-line RMS voltage (volts) [used only when VSContrl=0 and GenModel=2]
9999.9                 TEC_SLR     - Stator leakage reactance (ohms) [used only when VSContrl=0 and GenModel=2]
9999.9                 TEC_RLR     - Rotor leakage reactance (ohms) [used only when VSContrl=0 and GenModel=2]
9999.9                 TEC_MR      - Magnetizing reactance (ohms) [used only when VSContrl=0 and GenModel=2]
---------------------- HIGH-SPEED SHAFT BRAKE ----------------------------------
0                      HSSBrMode   - HSS brake model {0: none, 1: simple, 3: user-defined from routine UserHSSBr, 4: user-defined from Simulink/Labview, 5: user-defined from Bladed-style DLL} (switch)
9999.9                 THSSBrDp    - Time to initiate deployment of the HSS brake (s)
9999.9                 HSSBrDT     - Time for HSS-brake to reach full deployment once initiated (sec) [used only when HSSBrMode=1]
9999.9                 HSSBrTqF    - Fully deployed HSS-brake torque (N-m)
---------------------- NACELLE-YAW CONTROL -------------------------------------
0                      YCMode      - Yaw control mode {0: none, 3: user-defined from routine UserYawCont, 4: user-defined from Simulink/Labview, 5: user-defined from Bladed-style DLL} (switch)
9999.9                 TYCOn       - Time to enable active yaw control (s) [unused when YCMode=0]
0.0                    YawNeut     - Neutral yaw position--yaw spring force is zero at this yaw (degrees)
8458453511.0           YawSpr      - Nacelle-yaw spring constant (N-m/rad)
28561762.0              YawDamp     - Nacelle-yaw damping constant (N-m/(rad/s))
9999.9                 TYawManS    - Time to start override yaw maneuver and end standard yaw control (s)
0.25                   YawManRat   - Yaw maneuver rate (in absolute value) (deg/s)
0.0                    NacYawF     - Final yaw angle for override yaw maneuvers (degrees)
---------------------- Aerodynamic Flow Control -------------------------------------
0                      AfCmode     - Airfoil control mode {0- none, 1- cosine wave cycle, 4- user-defined from Simulink/Labview, 5- user-defined from Bladed-style DLL}
0.0                    AfC_Mean    - Mean level for sinusoidal cycling or steady value (-) [used only with AfCmode==1]
0.0                    AfC_Amp     - Amplitude for for cosine cycling of flap signal (AfC = AfC_Amp*cos(Azimuth+phase)+AfC_mean) (-) [used only with AfCmode==1]
0.0                    AfC_phase   - Phase relative to the blade azimuth (0 is vertical) for for cosine cycling of flap signal (deg) [used only with AfCmode==1]
---------------------- STRUCTURAL CONTROL ---------------------------------------
0                      NumBStC     - Number of blade structural controllers (integer)
"unused"               BStCfiles   - Name of the file for blade tuned mass damper (quoted string) [unused when CompNTMD is false]
0                      NumNStC     - Number of nacelle structural controllers (integer)
"unused"               NStCfiles   - Name of the file for nacelle tuned mass damper (quoted string) [unused when CompNTMD is false]
0                      NumTStC     - Number of tower structural controllers (integer)
"unused"               TStCfiles   - Name of the file for tower tuned mass damper (quoted string) [unused when CompNTMD is false]
0                      NumSStC     - Number of sbustructure structural controllers (integer)
"unused"               SStCfiles   - Name of the file for sbustructure tuned mass damper (quoted string) [unused when CompNTMD is false]
---------------------- CABLE CONTROL ---------------------------------------- 
0                      CCmode      - Cable control mode {0- none, 4- user-defined from Simulink/Labview, 5- user-defineAfC_phased from Bladed-style DLL}
---------------------- BLADED INTERFACE ---------------------------------------- [used only with Bladed Interface]
"../IEA-15-240-RWT/ServoData/libdiscon.dll"  DLL_FileName - Name/location of the dynamic library {.dll [Windows] or .so [Linux]} in the Bladed-DLL format (-) [used only with Bladed Interface]
"IEA-15-240-RWT-UMaineSemi_DISCON.IN"   DLL_InFile  - Name of input file sent to the DLL (-) [used only with Bladed Interface]
"DISCON"               DLL_ProcName - Name of procedure in DLL to be called (-) [case sensitive; used only with DLL Interface]
"default"              DLL_DT      - Communication interval for dynamic library (s) (or "default") [used only with Bladed Interface]
False                  DLL_Ramp    - Whether a linear ramp should be used between DLL_DT time steps [introduces time shift when true] (flag) [used only with Bladed Interface]
9999.9                 BPCutoff    - Cuttoff frequency for low-pass filter on blade pitch from DLL (Hz) [used only with Bladed Interface]
0.0                    NacYaw_North - Reference yaw angle of the nacelle when the upwind end points due North (deg) [used only with Bladed Interface]
0                      Ptch_Cntrl  - Record 28: Use individual pitch control {0: collective pitch; 1: individual pitch control} (switch) [used only with Bladed Interface]
0.0                    Ptch_SetPnt - Record  5: Below-rated pitch angle set-point (deg) [used only with Bladed Interface]
0.0                    Ptch_Min    - Record  6: Minimum pitch angle (deg) [used only with Bladed Interface]
0.0                    Ptch_Max    - Record  7: Maximum pitch angle (deg) [used only with Bladed Interface]
0.0                    PtchRate_Min - Record  8: Minimum pitch rate (most negative value allowed) (deg/s) [used only with Bladed Interface]
0.0                    PtchRate_Max - Record  9: Maximum pitch rate  (deg/s) [used only with Bladed Interface]
0.0                    Gain_OM     - Record 16: Optimal mode gain (Nm/(rad/s)^2) [used only with Bladed Interface]
0.0                    GenSpd_MinOM - Record 17: Minimum generator speed (rpm) [used only with Bladed Interface]
0.0                    GenSpd_MaxOM - Record 18: Optimal mode maximum speed (rpm) [used only with Bladed Interface]
0.0                    GenSpd_Dem  - Record 19: Demanded generator speed above rated (rpm) [used only with Bladed Interface]
0.0                    GenTrq_Dem  - Record 22: Demanded generator torque above rated (Nm) [used only with Bladed Interface]
0.0                    GenPwr_Dem  - Record 13: Demanded power (W) [used only with Bladed Interface]
---------------------- BLADED INTERFACE TORQUE-SPEED LOOK-UP TABLE -------------
0                      DLL_NumTrq  - Record 26: No. of points in torque-speed look-up table {0 = none and use the optimal mode parameters; nonzero = ignore the optimal mode PARAMETERs by setting Record 16 to 0.0} (-) [used only with Bladed Interface]
GenSpd_TLU            	GenTrq_TLU            
(rpm)                 	(Nm)                  
---------------------- OUTPUT --------------------------------------------------
True                   SumPrint    - Print summary data to <RootName>.sum (flag) (currently unused)
1                      OutFile     - Switch to determine where output will be placed: {1: in module output file only; 2: in glue code output file only; 3: both} (currently unused)
True                   TabDelim    - Use tab delimiters in text tabular output file? (flag) (currently unused)
"ES10.3E2"             OutFmt      - Format used for text tabular output (except time).  Resulting field should be 10 characters. (quoted string) (currently unused)
30.0                   TStart      - Time to begin tabular output (s) (currently unused)
OutList      - The next line(s) contains a list of output parameters.  
"GenPwr"
"GenTq"
END of input file (the word "END" must appear in the first 3 columns of this last Out_List line)
---------------------------------------------------------------------------------------
------- ELASTODYN v1.03.* INPUT FILE -------------------------------------------
IEA 15 MW offshore reference model on UMaine VolturnUS-S semi-submersible floating platform
---------------------- SIMULATION CONTROL --------------------------------------
False         Echo        - Echo input data to "<RootName>.ech" (flag)
          3   Method      - Integration method: {1: RK4, 2: AB4, or 3: ABM4} (-)
"default"     DT          Integration time step (s)
---------------------- DEGREES OF FREEDOM --------------------------------------
True          FlapDOF1    - First flapwise blade mode DOF (flag)
True          FlapDOF2    - Second flapwise blade mode DOF (flag)
True          EdgeDOF     - First edgewise blade mode DOF (flag)
False         TeetDOF     - Rotor-teeter DOF (flag) [unused for 3 blades]
False         DrTrDOF     - Drivetrain rotational-flexibility DOF (flag)
True          GenDOF      - Generator DOF (flag)
False         YawDOF      - Yaw DOF (flag)
True          TwFADOF1    - First fore-aft tower bending-mode DOF (flag)
True          TwFADOF2    - Second fore-aft tower bending-mode DOF (flag)
True          TwSSDOF1    - First side-to-side tower bending-mode DOF (flag)
True          TwSSDOF2    - Second side-to-side tower bending-mode DOF (flag)
True          PtfmSgDOF   - Platform horizontal surge translation DOF (flag)
True          PtfmSwDOF   - Platform horizontal sway translation DOF (flag)
True          PtfmHvDOF   - Platform vertical heave translation DOF (flag)
True          PtfmRDOF    - Platform roll tilt rotation DOF (flag)
True          PtfmPDOF    - Platform pitch tilt rotation DOF (flag)
True          PtfmYDOF    - Platform yaw rotation DOF (flag)
---------------------- INITIAL CONDITIONS --------------------------------------
          0   OoPDefl     - Initial out-of-plane blade-tip displacement (meters)
          0   IPDefl      - Initial in-plane blade-tip deflection (meters)
          0  BlPitch(1)  - Blade 1 initial pitch (degrees)
          0  BlPitch(2)  - Blade 2 initial pitch (degrees)
          0  BlPitch(3)  - Blade 3 initial pitch (degrees) [unused for 2 blades]
          0   TeetDefl    - Initial or fixed teeter angle (degrees) [unused for 3 blades]
          0   Azimuth     - Initial azimuth angle for blade 1 (degrees)
          0   RotSpeed    - Initial or fixed rotor speed (rpm)
          0   NacYaw      - Initial or fixed nacelle-yaw angle (degrees)
          0   TTDspFA     - Initial fore-aft tower-top displacement (meters)
          0   TTDspSS     - Initial side-to-side tower-top displacement (meters)
          0   PtfmSurge   
          0   PtfmSway    
          0   PtfmHeave   
          0   PtfmRoll    
          0   PtfmPitch   
          0   PtfmYaw    
---------------------- TURBINE CONFIGURATION -----------------------------------
          3   NumBl       - Number of blades (-)
     120.97   TipRad      - The distance from the rotor apex to the blade tip (meters)
       3.97   HubRad      - The distance from the rotor apex to the blade root (meters)
         -4   PreCone(1)  - Blade 1 cone angle (degrees)
         -4   PreCone(2)  - Blade 2 cone angle (degrees)
         -4   PreCone(3)  - Blade 3 cone angle (degrees) [unused for 2 blades]
          0   HubCM       - Distance from rotor apex to hub mass [positive downwind] (meters)
          0   UndSling    - Undersling length [distance from teeter pin to the rotor apex] (meters) [unused for 3 blades]
          0   Delta3      - Delta-3 angle for teetering rotors (degrees) [unused for 3 blades]
          0   AzimB1Up    - Azimuth value to use for I/O when blade 1 points up (degrees)
    -12.098   OverHang    - Distance from yaw axis to rotor apex [3 blades] or teeter pin [2 blades] (meters)
        0.0   ShftGagL    - Distance from rotor apex [3 blades] or teeter pin [2 blades] to shaft strain gages [positive for upwind rotors] (meters)
       -6.0   ShftTilt    - Rotor shaft tilt angle (degrees)
    -4.7201   NacCMxn     - Downwind distance from the tower-top to the nacelle CM (meters)
        0.0   NacCMyn     - Lateral  distance from the tower-top to the nacelle CM (meters)
     4.2751   NacCMzn     - Vertical distance from the tower-top to the nacelle CM (meters)
        0.0   NcIMUxn     - Downwind distance from the tower-top to the nacelle IMU (meters)
        0.0   NcIMUyn     - Lateral  distance from the tower-top to the nacelle IMU (meters)
        0.0   NcIMUzn     - Vertical distance from the tower-top to the nacelle IMU (meters)
     4.3495   Twr2Shft    - Vertical distance from the tower-top to the rotor shaft (meters)
    144.386   TowerHt     - Height of tower above ground level [onshore] or MSL [offshore] (meters)
         15   TowerBsHt   - Height of tower base above ground level [onshore] or MSL [offshore] (meters)
          0   PtfmCMxt    - Downwind distance from the ground level [onshore] or MSL [offshore] to the platform CM (meters)
          0   PtfmCMyt    - Lateral distance from the ground level [onshore] or MSL [offshore] to the platform CM (meters)
    -14.400   PtfmCMzt    - Vertical distance from the ground level [onshore] or MSL [offshore] to the platform CM (meters)
          0   PtfmRefzt   - Vertical distance from the ground level [onshore] or MSL [offshore] to the platform reference point (meters)
---------------------- MASS AND INERTIA ----------------------------------------
          0   TipMass(1)  - Tip-brake mass, blade 1 (kg)
          0   TipMass(2)  - Tip-brake mass, blade 2 (kg)
          0   TipMass(3)  - Tip-brake mass, blade 3 (kg) [unused for 2 blades]
      69360   HubMass     - Hub mass (kg)
     973520   HubIner     - Hub inertia about rotor axis [3 blades] or teeter axis [2 blades] (kg m^2)
    1836784   GenIner     - Generator inertia about HSS (kg m^2)
     646895   NacMass     - Nacelle mass (kg)
   24240914   NacYIner    - Nacelle inertia about yaw axis (kg m^2)
      28280   YawBrMass   - Yaw bearing mass (kg)
1.7838E+07    PtfmMass    - Platform mass (kg)
1.2507E+10    PtfmRIner   - Platform inertia for roll tilt rotation about the platform CM (kg m^2)
1.2507E+10    PtfmPIner   - Platform inertia for pitch tilt rotation about the platform CM (kg m^2)
2.3667E+10    PtfmYIner   - Platform inertia for yaw rotation about the platform CM (kg m^2)
---------------------- BLADE ---------------------------------------------------
         50   BldNodes    - Number of blade nodes (per blade) used for analysis (-)
"../IEA-15-240-RWT/IEA-15-240-RWT_ElastoDyn_blade.dat"    BldFile1    - Name of file containing properties for blade 1 (quoted string)
"../IEA-15-240-RWT/IEA-15-240-RWT_ElastoDyn_blade.dat"    BldFile2    - Name of file containing properties for blade 2 (quoted string)
"../IEA-15-240-RWT/IEA-15-240-RWT_ElastoDyn_blade.dat"    BldFile3    - Name of file containing properties for blade 3 (quoted string) [unused for 2 blades]
---------------------- ROTOR-TEETER --------------------------------------------
          0   TeetMod     - Rotor-teeter spring/damper model {0: none, 1: standard, 2: user-defined from routine UserTeet} (switch) [unused for 3 blades]
          0   TeetDmpP    - Rotor-teeter damper position (degrees) [used only for 2 blades and when TeetMod=1]
          0   TeetDmp     - Rotor-teeter damping constant (N-m/(rad/s)) [used only for 2 blades and when TeetMod=1]
          0   TeetCDmp    - Rotor-teeter rate-independent Coulomb-damping moment (N-m) [used only for 2 blades and when TeetMod=1]
          0   TeetSStP    - Rotor-teeter soft-stop position (degrees) [used only for 2 blades and when TeetMod=1]
          0   TeetHStP    - Rotor-teeter hard-stop position (degrees) [used only for 2 blades and when TeetMod=1]
          0   TeetSSSp    - Rotor-teeter soft-stop linear-spring constant (N-m/rad) [used only for 2 blades and when TeetMod=1]
          0   TeetHSSp    - Rotor-teeter hard-stop linear-spring constant (N-m/rad) [used only for 2 blades and when TeetMod=1]
---------------------- DRIVETRAIN ----------------------------------------------
        100   GBoxEff     - Gearbox efficiency (%)
          1   GBRatio     - Gearbox ratio (-)
51140939610   DTTorSpr    - Drivetrain torsional spring (N-m/rad)
   42676833   DTTorDmp    - Drivetrain torsional damper (N-m/(rad/s))
---------------------- FURLING -------------------------------------------------
False         Furling     - Read in additional model properties for furling turbine (flag) [must currently be FALSE)
"unused"      FurlFile    - Name of file containing furling properties (quoted string) [unused when Furling=False]
---------------------- TOWER ---------------------------------------------------
         20   TwrNodes    - Number of tower nodes used for analysis (-)
"IEA-15-240-RWT-UMaineSemi_ElastoDyn_tower.dat"    TwrFile     - Name of file containing tower properties (quoted string)




Best regards,

I would like to supplement the remaining documents here

------- AERODYN v15.03.* INPUT FILE ------------------------------------------------
IEA 15 MW Offshore Reference Turbine
======  General Options  ============================================================================
False                  Echo        - Echo the input to "<rootname>.AD.ech"?  (flag)
default                DTAero      - Time interval for aerodynamic calculations {or "default"} (s)
1                      WakeMod     - Type of wake/induction model (switch) {0=none, 1=BEMT, 2=DBEMT, 3=OLAF} [WakeMod cannot be 2 or 3 when linearizing]
2                      AFAeroMod   - Type of blade airfoil aerodynamics model (switch) {1=steady model, 2=Beddoes-Leishman unsteady model} [AFAeroMod must be 1 when linearizing]
1                      TwrPotent   - Type tower influence on wind based on potential flow around the tower (switch) {0=none, 1=baseline potential flow, 2=potential flow with Bak correction}
1                      TwrShadow   - Calculate tower influence on wind based on downstream tower shadow (switch) {0=none, 1=Powles model, 2=Eames model}
True                   TwrAero     - Calculate tower aerodynamic loads? (flag)
False                  FrozenWake  - Assume frozen wake during linearization? (flag) [used only when WakeMod=1 and when linearizing]
False                  CavitCheck  - Perform cavitation check? (flag) [AFAeroMod must be 1 when CavitCheck=true]
False                  Buoyancy    - Include buoyancy effects? (flag)
False                  CompAA      - Flag to compute AeroAcoustics calculation [only used when WakeMod=1 or 2]
AeroAcousticsInput.dat AA_InputFile - AeroAcoustics input file [used only when CompAA=true]
======  Environmental Conditions  ===================================================================
"default"              AirDens     - Air density (kg/m^3)
"default"              KinVisc     - Kinematic air viscosity (m^2/s)
"default"              SpdSound    - Speed of sound (m/s)
"default"              Patm        - Atmospheric pressure (Pa) [used only when CavitCheck=True]
"default"              Pvap        - Vapour pressure of fluid (Pa) [used only when CavitCheck=True]
======  Blade-Element/Momentum Theory Options  ====================================================== [used only when WakeMod=1]
1                      SkewMod     - Type of skewed-wake correction model (switch) {1=uncoupled, 2=Pitt/Peters, 3=coupled} [unused when WakeMod=0 or 3]
default                SkewModFactor - Constant used in Pitt/Peters skewed wake model {or "default" is 15/32*pi} (-) [used only when SkewMod=2; unused when WakeMod=0 or 3]
True                   TipLoss     - Use the Prandtl tip-loss model? (flag) [unused when WakeMod=0 or 3]
True                   HubLoss     - Use the Prandtl hub-loss model? (flag) [unused when WakeMod=0 or 3]
True                   TanInd      - Include tangential induction in BEMT calculations? (flag) [unused when WakeMod=0 or 3]
True                   AIDrag      - Include the drag term in the axial-induction calculation? (flag) [unused when WakeMod=0 or 3]
True                   TIDrag      - Include the drag term in the tangential-induction calculation? (flag) [unused when WakeMod=0,3 or TanInd=FALSE]
default                IndToler    - Convergence tolerance for BEMT nonlinear solve residual equation {or "default"} (-) [unused when WakeMod=0 or 3]
500                    MaxIter     - Maximum number of iteration steps (-) [unused when WakeMod=0]
======  Dynamic Blade-Element/Momentum Theory Options  ====================================================== [used only when WakeMod=1]
2                      DBEMT_Mod   - Type of dynamic BEMT (DBEMT) model {1=constant tau1, 2=time-dependent tau1} (-) [used only when WakeMod=2]
29.03                  tau1_const  - Time constant for DBEMT (s) [used only when WakeMod=2 and DBEMT_Mod=1]
======  OLAF -- cOnvecting LAgrangian Filaments (Free Vortex Wake) Theory Options  ================== [used only when WakeMod=3]
../IEA-15-240-RWT-OLAF/IEA-15-240-RWT_OLAF.dat OLAFInputFileName - Input file for OLAF [used only when WakeMod=3]
======  Beddoes-Leishman Unsteady Airfoil Aerodynamics Options  ===================================== [used only when AFAeroMod=2]
3                      UAMod       - Unsteady Aero Model Switch (switch) {1=Baseline model (Original), 2=Gonzalez's variant (changes in Cn,Cc,Cm), 3=Minnema/Pierce variant (changes in Cc and Cm)} [used only when AFAeroMod=2]
True                   FLookup     - Flag to indicate whether a lookup for f' will be calculated (TRUE) or whether best-fit exponential equations will be used (FALSE); if FALSE S1-S4 must be provided in airfoil input files (flag) [used only when AFAeroMod=2]
0.1                    UAStartRad  - Starting radius for dynamic stall (fraction of rotor radius) [used only when AFAeroMod=2]
1.0                    UAEndRad    - Ending radius for dynamic stall (fraction of rotor radius) [used only when AFAeroMod=2]
======  Airfoil Information =========================================================================
1                      AFTabMod    - Interpolation method for multiple airfoil tables {1=1D interpolation on AoA (first table only); 2=2D interpolation on AoA and Re; 3=2D interpolation on AoA and UserProp} (-)
1                      InCol_Alfa  - The column in the airfoil tables that contains the angle of attack (-)
2                      InCol_Cl    - The column in the airfoil tables that contains the lift coefficient (-)
3                      InCol_Cd    - The column in the airfoil tables that contains the drag coefficient (-)
4                      InCol_Cm    - The column in the airfoil tables that contains the pitching-moment coefficient; use zero if there is no Cm column (-)
0                      InCol_Cpmin - The column in the airfoil tables that contains the Cpmin coefficient; use zero if there is no Cpmin column (-)
50                     NumAFfiles  - Number of airfoil files used (-)
"../IEA-15-240-RWT/Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_00.dat"    AFNames            - Airfoil file names (NumAFfiles lines) (quoted strings)
"../IEA-15-240-RWT/Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_01.dat"
"../IEA-15-240-RWT/Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_02.dat"
"../IEA-15-240-RWT/Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_03.dat"
"../IEA-15-240-RWT/Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_04.dat"
"../IEA-15-240-RWT/Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_05.dat"
"../IEA-15-240-RWT/Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_06.dat"
"../IEA-15-240-RWT/Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_07.dat"
"../IEA-15-240-RWT/Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_08.dat"
"../IEA-15-240-RWT/Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_09.dat"
"../IEA-15-240-RWT/Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_10.dat"
"../IEA-15-240-RWT/Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_11.dat"
"../IEA-15-240-RWT/Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_12.dat"
"../IEA-15-240-RWT/Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_13.dat"
"../IEA-15-240-RWT/Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_14.dat"
"../IEA-15-240-RWT/Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_15.dat"
"../IEA-15-240-RWT/Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_16.dat"
"../IEA-15-240-RWT/Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_17.dat"
"../IEA-15-240-RWT/Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_18.dat"
"../IEA-15-240-RWT/Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_19.dat"
"../IEA-15-240-RWT/Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_20.dat"
"../IEA-15-240-RWT/Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_21.dat"
"../IEA-15-240-RWT/Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_22.dat"
"../IEA-15-240-RWT/Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_23.dat"
"../IEA-15-240-RWT/Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_24.dat"
"../IEA-15-240-RWT/Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_25.dat"
"../IEA-15-240-RWT/Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_26.dat"
"../IEA-15-240-RWT/Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_27.dat"
"../IEA-15-240-RWT/Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_28.dat"
"../IEA-15-240-RWT/Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_29.dat"
"../IEA-15-240-RWT/Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_30.dat"
"../IEA-15-240-RWT/Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_31.dat"
"../IEA-15-240-RWT/Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_32.dat"
"../IEA-15-240-RWT/Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_33.dat"
"../IEA-15-240-RWT/Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_34.dat"
"../IEA-15-240-RWT/Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_35.dat"
"../IEA-15-240-RWT/Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_36.dat"
"../IEA-15-240-RWT/Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_37.dat"
"../IEA-15-240-RWT/Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_38.dat"
"../IEA-15-240-RWT/Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_39.dat"
"../IEA-15-240-RWT/Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_40.dat"
"../IEA-15-240-RWT/Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_41.dat"
"../IEA-15-240-RWT/Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_42.dat"
"../IEA-15-240-RWT/Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_43.dat"
"../IEA-15-240-RWT/Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_44.dat"
"../IEA-15-240-RWT/Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_45.dat"
"../IEA-15-240-RWT/Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_46.dat"
"../IEA-15-240-RWT/Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_47.dat"
"../IEA-15-240-RWT/Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_48.dat"
"../IEA-15-240-RWT/Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_49.dat"
======  Rotor/Blade Properties  =====================================================================
True                   UseBlCm     - Include aerodynamic pitching moment in calculations?  (flag)
"../IEA-15-240-RWT/IEA-15-240-RWT_AeroDyn15_blade.dat" ADBlFile(1) - Name of file containing distributed aerodynamic properties for Blade #1 (-)
"../IEA-15-240-RWT/IEA-15-240-RWT_AeroDyn15_blade.dat" ADBlFile(2) - Name of file containing distributed aerodynamic properties for Blade #2 (-) [unused if NumBl < 2]
"../IEA-15-240-RWT/IEA-15-240-RWT_AeroDyn15_blade.dat" ADBlFile(3) - Name of file containing distributed aerodynamic properties for Blade #3 (-) [unused if NumBl < 3]
======  Hub Properties ============================================================================== [used only when Buoyancy=True]
0.0   VolHub             - Hub volume (m^3)
0.0   HubCenBx           - Hub center of buoyancy x direction offset (m)
======  Nacelle Properties ========================================================================== [used only when Buoyancy=True]
0.0   VolNac             - Nacelle volume (m^3)
0,0,0 NacCenB            - Position of nacelle center of buoyancy from yaw bearing in nacelle coordinates (m)
======  Tail fin Aerodynamics ======================================================================== 
False         TFinAero           - Calculate tail fin aerodynamics model (flag)
"unused"      TFinFile           - Input file for tail fin aerodynamics [used only when TFinAero=True]
======  Tower Influence and Aerodynamics ============================================================= [used only when TwrPotent/=0, TwrShadow/=0, or TwrAero=True]
11                     NumTwrNds   - Number of tower nodes used in the analysis  (-) [used only when TwrPotent/=0, TwrShadow/=0, or TwrAero=True]
TwrElev        TwrDiam        TwrCd         TwrTI      TwrCb !TwrTI used only with TwrShadow=2, TwrCb used only with Buoyancy=True
(m)              (m)           (-)           (-)        (-)
  15.           10.            0.5           0.1        0.0
  28.           10.            0.5           0.1        0.0
  41.           10.            0.5           0.1        0.0
  54.           10.            0.5           0.1        0.0
  67.           10.            0.5           0.1        0.0
  80.           10.            0.5           0.1        0.0
  93.           10.            0.5           0.1        0.0
 106.           10.            0.5           0.1        0.0
 119.           10.            0.5           0.1        0.0
 132.           10.            0.5           0.1        0.0
 144.386         6.5           0.5           0.1        0.0
======  Outputs  ====================================================================================
False                  SumPrint    - Generate a summary file listing input options and interpolated properties to "<rootname>.AD.sum"?  (flag)
9                      NBlOuts     - Number of blade node outputs [0 - 9] (-)
6, 11, 16, 21, 25, 30, 35, 40, 45 BlOutNd     - Blade nodes whose values will be output  (-)
0                      NTwOuts     - Number of tower node outputs [0 - 9]  (-)
0                      TwOutNd     - Tower nodes whose values will be output  (-)
                   OutList             - The next line(s) contains a list of output parameters.  See OutListParameters.xlsx for a listing of available output channels, (-)
"RtFldFxh"
"RtFldFyh"
"RtFldFzh"
"RtFldMxh"
"RtFldMyh"
"RtFldMzh"
"RtVAvgxh"
"RtFldCp"
"RtFldCt"
"RtArea"
"RtSpeed"
"RtTSR"
END of input file (the word "END" must appear in the first 3 columns of this last OutList line)

Dear @Yushun.Fu,

You have not enabled InflowWind (CompInflow = 0), so, still air is assumed and I would not expect power generation.

Best regards,

1 Like

Dear,
Thank you very much for your help. The simplest part is the easiest to overlook
Best regards,