Hi,
I want to run the 5MW Baseline file from r-test: 5MW_Land_DLL_WTurb.
When I run it I get the following errors:
[code]OpenFAST-v1.0.0
Compile Info:
- Architecture: 64 bit
- Precision: single
Execution Info: - Date: 03/06/2019
- Time: 14:12:10+0100
OpenFAST input file heading:
FAST Certification Test #18: NREL 5.0 MW Baseline Wind Turbine (Onshore)
Running ElastoDyn.
Running AeroDyn.
FAST_InitializeAll:AD_Init:ReadInputFiles:ReadPrimaryFile:Invalid logical input for file
“.\NRELOffshrBsline5MW_Onshore_AeroDyn15.dat” occurred while trying to read TipLoss.
ReadPrimaryFile:Invalid numerical input for file “.\NRELOffshrBsline5MW_Onshore_AeroDyn15.dat”
occurred while trying to read IndToler.
ReadPrimaryFile:Invalid numerical input for file “.\NRELOffshrBsline5MW_Onshore_AeroDyn15.dat”
occurred while trying to read MaxIter.
FAST encountered an error during module initialization.
Simulation error level: FATAL ERROR
Aborting OpenFAST.[/code]
I am using only the default settings from r-test:
[code]------- AERODYN v15 for OpenFAST INPUT FILE -----------------------------------------------
NREL 5.0 MW offshore baseline aerodynamic input properties.
====== General Options ============================================================================
False Echo - Echo the input to “.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} [WakeMod cannot be 2 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}
False TwrShadow - Calculate tower influence on wind based on downstream tower shadow? (flag)
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]
====== Environmental Conditions ===================================================================
1.225 AirDens - Air density (kg/m^3)
1.464E-05 KinVisc - Kinematic air viscosity (m^2/s)
335 SpdSound - Speed of sound (m/s)
103500 Patm - Atmospheric pressure ¶ [used only when CavitCheck=True]
1700 Pvap - Vapour pressure of fluid ¶ [used only when CavitCheck=True]
0.5 FluidDepth - Water depth above mid-hub height (m) [used only when CavitCheck=True]
====== Blade-Element/Momentum Theory Options ====================================================== [unused when WakeMod=0]
2 SkewMod - Type of skewed-wake correction model (switch) {1=uncoupled, 2=Pitt/Peters, 3=coupled} [unused when WakeMod=0]
“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]
True TipLoss - Use the Prandtl tip-loss model? (flag) [unused when WakeMod=0]
True HubLoss - Use the Prandtl hub-loss model? (flag) [unused when WakeMod=0]
true TanInd - Include tangential induction in BEMT calculations? (flag) [unused when WakeMod=0]
False AIDrag - Include the drag term in the axial-induction calculation? (flag) [unused when WakeMod=0]
False TIDrag - Include the drag term in the tangential-induction calculation? (flag) [unused when WakeMod=0 or TanInd=FALSE]
“Default” IndToler - Convergence tolerance for BEMT nonlinear solve residual equation {or “default”} (-) [unused when WakeMod=0]
100 MaxIter - Maximum number of iteration steps (-) [unused when WakeMod=0]
====== Dynamic Blade-Element/Momentum Theory Options ============================================== [used only when WakeMod=2]
2 DBEMT_Mod - Type of dynamic BEMT (DBEMT) model {1=constant tau1, 2=time-dependent tau1} (-) [used only when WakeMod=2]
4 tau1_const - Time constant for DBEMT (s) [used only when WakeMod=2 and DBEMT_Mod=1]
====== 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=Minemma/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]
====== Airfoil Information =========================================================================
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 (-)
8 NumAFfiles - Number of airfoil files used (-)
“…/5MW_Baseline/Airfoils/Cylinder1.dat” AFNames - Airfoil file names (NumAFfiles lines) (quoted strings)
“…/5MW_Baseline/Airfoils/Cylinder2.dat”
“…/5MW_Baseline/Airfoils/DU40_A17.dat”
“…/5MW_Baseline/Airfoils/DU35_A17.dat”
“…/5MW_Baseline/Airfoils/DU30_A17.dat”
“…/5MW_Baseline/Airfoils/DU25_A17.dat”
“…/5MW_Baseline/Airfoils/DU21_A17.dat”
“…/5MW_Baseline/Airfoils/NACA64_A17.dat”
====== Rotor/Blade Properties =====================================================================
True UseBlCm - Include aerodynamic pitching moment in calculations? (flag)
“…/5MW_Baseline/NRELOffshrBsline5MW_AeroDyn_blade.dat” ADBlFile(1) - Name of file containing distributed aerodynamic properties for Blade #1 (-)
“…/5MW_Baseline/NRELOffshrBsline5MW_AeroDyn_blade.dat” ADBlFile(2) - Name of file containing distributed aerodynamic properties for Blade #2 (-) [unused if NumBl < 2]
“…/5MW_Baseline/NRELOffshrBsline5MW_AeroDyn_blade.dat” ADBlFile(3) - Name of file containing distributed aerodynamic properties for Blade #3 (-) [unused if NumBl < 3]
====== Tower Influence and Aerodynamics ============================================================= [used only when TwrPotent/=0, TwrShadow=True, or TwrAero=True]
12 NumTwrNds - Number of tower nodes used in the analysis (-) [used only when TwrPotent/=0, TwrShadow=True, or TwrAero=True]
TwrElev TwrDiam TwrCd
(m) (m) (-)
0.0000000E+00 6.0000000E+00 1.0000000E+00
8.5261000E+00 5.7870000E+00 1.0000000E+00
1.7053000E+01 5.5740000E+00 1.0000000E+00
2.5579000E+01 5.3610000E+00 1.0000000E+00
3.4105000E+01 5.1480000E+00 1.0000000E+00
4.2633000E+01 4.9350000E+00 1.0000000E+00
5.1158000E+01 4.7220000E+00 1.0000000E+00
5.9685000E+01 4.5090000E+00 1.0000000E+00
6.8211000E+01 4.2960000E+00 1.0000000E+00
7.6738000E+01 4.0830000E+00 1.0000000E+00
8.5268000E+01 3.8700000E+00 1.0000000E+00
8.7600000E+01 3.8700000E+00 1.0000000E+00
====== Outputs ====================================================================================
True SumPrint - Generate a summary file listing input options and interpolated properties to “.AD.sum”? (flag)
0 NBlOuts - Number of blade node outputs [0 - 9] (-)
1, 9, 19 BlOutNd - Blade nodes whose values will be output (-)
0 NTwOuts - Number of tower node outputs [0 - 9] (-)
1, 2, 6 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, (-)
END of input file (the word “END” must appear in the first 3 columns of this last OutList line)
[/code]
AD15 Echo is:
This file of echoed input was generated by AeroDyn on 06-Mar-2019 at 14:22:06.
Data from AeroDyn primary input file ".\NRELOffshrBsline5MW_Onshore_AeroDyn15.dat":
FTitle - File Header: File Description (line 2)
"NREL 5.0 MW offshore baseline aerodynamic input properties."
T Echo - Echo flag
DTAero - Time interval for aerodynamic calculations {or default} (s)
"default"
1 WakeMod - Type of wake/induction model {0=none, 1=BEMT} (-)
2 AFAeroMod - Type of airfoil aerodynamics model {1=steady model, 2=Beddoes-Leishman unsteady model} (-)
1 TwrPotent - Type tower influence on wind based on potential flow around the tower {0=none, 1=baseline potential flow, 2=potential flow with Bak correction} (-)
F TwrShadow - Calculate tower influence on wind based on downstream tower shadow? (flag)
T TwrAero - Calculate tower aerodynamic loads? (flag)
F FrozenWake - Assume frozen wake during linearization? (flag)
F CavitCheck - Perform cavitation check? (flag)
1.2250E+00 AirDens - Air density (kg/m^3)
1.4640E-05 KinVisc - Kinematic air viscosity (m^2/s)
3.3500E+02 SpdSound - Speed of sound (m/s)
1.0350E+05 Patm - Atmospheric pressure (Pa)
1.7000E+03 Pvap - Vapour pressure of fluid (Pa)
5.0000E-01 FluidDepth - Water depth above mid-hub height (MHK only, for cavitation check) (m)
2 SkewMod - Type of skewed-wake correction model {1=uncoupled, 2=Pitt/Peters, 3=coupled} [used only when WakeMod=1] (-)
T HubLoss - Use the Prandtl hub-loss model? [used only when WakeMod=1] (flag)
T TanInd - Include tangential induction in BEMT calculations? [used only when WakeMod=1] (flag)
T AIDrag - Include the drag term in the axial-induction calculation? [used only when WakeMod=1] (flag)
F TIDrag - Include the drag term in the tangential-induction calculation? [used only when WakeMod=1 and TanInd=TRUE] (flag)
IndToler - Convergence tolerance for BEM induction factors [used only when WakeMod=1] (-)
"False"I tried different values for all three errors, but nothing helped. Default settings seem to be in correct form (numerical/logical).
Regards,
Till