mohsen ab.1999
i checked all over the points which you mentioned in above massages for me but this give me erorre yet like before :
AqwaCosimulation: Inadequate blade data files (ADBlFile) given in the AeroDyn primary input file (E:\hydraulic pitch system of wind turbin\new reasearch\open fast\r-test-ef6ab575919f1db597702f1c3f86a16bdc2b4338\r-test-ef6ab575919f1db597702f1c3f86a16bdc2b4338\modules\aerodyn\py_ad_5MW_OC4Semi_WSt_WavesWN\ad_primary.dat)
AqwaCosimulation: Failed to prepare the AeroDyn marker data.
now i want to shear with you me Aero Dyn primary input file which actualle relate to NREL 5 mw and please help me to correct this because there is no toturial exist about that yet ..
this is my Aero Dyn primary input file :
------- AERODYN v15 for OpenFAST INPUT FILE -----------------------------------------------
NREL 5.0 MW offshore baseline aerodynamic input properties.
====== General Options ============================================================================
True Echo - Echo the input to "
1 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]
1 AFAeroMod - Type of blade airfoil aerodynamics model (switch) {1=steady model, 2=Beddoes-Leishman unsteady model} [AFAeroMod must be 1 when linearizing]
0 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}
0 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]
True Buoyancy - Include buoyancy effects? (flag)
False CompAA - Flag to compute AeroAcoustics calculation [used only when WakeMod = 1 or 2]
"unused" AA_InputFile - AeroAcoustics input file [used only when CompAA=true]
====== Environmental Conditions ===================================================================
1.225 AirDens - Air density (kg/m^3)
0.00001 KinVisc - Kinematic viscosity of working fluid (m^2/s)
340.3 SpdSound - Speed of sound in working fluid (m/s)
101325 Patm - Atmospheric pressure (Pa) [used only when CavitCheck=True]
2000 Pvap - Vapour pressure of working fluid (Pa) [used only when CavitCheck=True]
====== Blade-Element/Momentum Theory Options ====================================================== [unused when WakeMod=0 or 3]
1 SkewMod - Type of skewed-wake correction model (switch) {1=uncoupled, 2=Pitt/Peters, 3=coupled} [unused when WakeMod=0 or 3]
2 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]
False AIDrag - Include the drag term in the axial-induction calculation? (flag) [unused when WakeMod=0 or 3]
False TIDrag - Include the drag term in the tangential-induction calculation? (flag) [unused when WakeMod=0,3 or TanInd=FALSE]
0.00001 IndToler - Convergence tolerance for BEMT nonlinear solve residual equation {or "default"} (-) [unused when WakeMod=0 or 3]
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, 3=constant tau1 with continuous formulation} (-) [used only when WakeMod=2]
4 tau1_const - Time constant for DBEMT (s) [used only when WakeMod=2 and DBEMT_Mod=1 or 3]
====== OLAF -- cOnvecting LAgrangian Filaments (Free Vortex Wake) Theory Options ================== [used only when WakeMod=3]
"unused" 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) {2=B-L Gonzalez, 3=B-L Minnema/Pierce, 4=B-L HGM 4-states, 5=B-L 5 states, 6=Oye, 7=Boeing-Vertol} [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 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 (-)
8 NumAFfiles - Number of airfoil files used (-)
1 "E:/hydraulic pitch system of wind turbin/new reasearch/open fast/r-test-ef6ab575919f1db597702f1c3f86a16bdc2b4338/r-test-ef6ab575919f1db597702f1c3f86a16bdc2b4338/glue-codes/openfast/5MW_Baseline/Airfoils/Cylinder1.dat" AFNames - Airfoil file names (NumAFfiles lines) (quoted strings)
2 "E:/hydraulic pitch system of wind turbin/new reasearch/open fast/r-test-ef6ab575919f1db597702f1c3f86a16bdc2b4338/r-test-ef6ab575919f1db597702f1c3f86a16bdc2b4338/glue-codes/openfast/5MW_Baseline/Airfoils/Cylinder2.dat"
3 "E:/hydraulic pitch system of wind turbin/new reasearch/open fast/r-test-ef6ab575919f1db597702f1c3f86a16bdc2b4338/r-test-ef6ab575919f1db597702f1c3f86a16bdc2b4338/glue-codes/openfast/5MW_Baseline/Airfoils/DU40_A17.dat"
4 "E:/hydraulic pitch system of wind turbin/new reasearch/open fast/r-test-ef6ab575919f1db597702f1c3f86a16bdc2b4338/r-test-ef6ab575919f1db597702f1c3f86a16bdc2b4338/glue-codes/openfast/5MW_Baseline/Airfoils/DU35_A17.dat"
5 "E:/hydraulic pitch system of wind turbin/new reasearch/open fast/r-test-ef6ab575919f1db597702f1c3f86a16bdc2b4338/r-test-ef6ab575919f1db597702f1c3f86a16bdc2b4338/glue-codes/openfast/5MW_Baseline/Airfoils/DU30_A17.dat"
6 "E:/hydraulic pitch system of wind turbin/new reasearch/open fast/r-test-ef6ab575919f1db597702f1c3f86a16bdc2b4338/r-test-ef6ab575919f1db597702f1c3f86a16bdc2b4338/glue-codes/openfast/5MW_Baseline/Airfoils/DU25_A17.dat"
7 "E:/hydraulic pitch system of wind turbin/new reasearch/open fast/r-test-ef6ab575919f1db597702f1c3f86a16bdc2b4338/r-test-ef6ab575919f1db597702f1c3f86a16bdc2b4338/glue-codes/openfast/5MW_Baseline/Airfoils/DU21_A17.dat"
8 "E:/hydraulic pitch system of wind turbin/new reasearch/open fast/r-test-ef6ab575919f1db597702f1c3f86a16bdc2b4338/r-test-ef6ab575919f1db597702f1c3f86a16bdc2b4338/glue-codes/openfast/5MW_Baseline/Airfoils/NACA64_A17.dat"
====== Rotor/Blade Properties =====================================================================
True UseBlCm - Include aerodynamic pitching moment in calculations? (flag)
"E:/hydraulic pitch system of wind turbin/new reasearch/open fast/r-test-ef6ab575919f1db597702f1c3f86a16bdc2b4338/r-test-ef6ab575919f1db597702f1c3f86a16bdc2b4338/glue-codes/openfast/5MW_Baseline/NRELOffshrBsline5MW_AeroDyn_blade1.dat" ADBlFile(1) - Name of file containing distributed aerodynamic properties for Blade #1 (-)
"E:/hydraulic pitch system of wind turbin/new reasearch/open fast/r-test-ef6ab575919f1db597702f1c3f86a16bdc2b4338/r-test-ef6ab575919f1db597702f1c3f86a16bdc2b4338/glue-codes/openfast/5MW_Baseline/NRELOffshrBsline5MW_AeroDyn_blade2.dat" ADBlFile(2) - Name of file containing distributed aerodynamic properties for Blade #2 (-) [unused if NumBl < 2]
"E:/hydraulic pitch system of wind turbin/new reasearch/open fast/r-test-ef6ab575919f1db597702f1c3f86a16bdc2b4338/r-test-ef6ab575919f1db597702f1c3f86a16bdc2b4338/glue-codes/openfast/5MW_Baseline/NRELOffshrBsline5MW_AeroDyn_blade3.dat" ADBlFile(3) - Name of file containing distributed aerodynamic properties for Blade #3 (-) [unused if NumBl < 3]
====== Hub Properties ============================================================================== [used only when Buoyancy=True]
22 VolHub - Hub volume (m^3)
6.0 HubCenBx - Hub center of buoyancy x direction offset (m)
====== Nacelle Properties ========================================================================== [used only when Buoyancy=True]
40.0 VolNac - Nacelle volume (m^3)
1,2,3 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, TwrAero=True, or Buoyancy=True]
11 NumTwrNds - Number of tower nodes used in the analysis (-) [used only when TwrPotent/=0, TwrShadow/=0, TwrAero=True, or Buoyancy=True]
TwrElev TwrDiam TwrCd TwrTI TwrCb !TwrTI used only with TwrShadow=2, TwrCb used only with Buoyancy=True
(m) (m) (-) (-) (-)
1.0000000E+01 6.5000000E+00 1.0000000E+00 1.0000000E-01 0.0
1.7760000E+01 6.2400000E+00 1.0000000E+00 1.0000000E-01 0.0
2.5520000E+01 5.9700000E+00 1.0000000E+00 1.0000000E-01 0.0
3.3280000E+01 5.7100000E+00 1.0000000E+00 1.0000000E-01 0.0
4.1040000E+01 5.4500000E+00 1.0000000E+00 1.0000000E-01 0.0
4.8800000E+01 5.1800000E+00 1.0000000E+00 1.0000000E-01 0.0
5.6560000E+01 4.9200000E+00 1.0000000E+00 1.0000000E-01 0.0
6.4320000E+01 4.6600000E+00 1.0000000E+00 1.0000000E-01 0.0
7.2080000E+01 4.4000000E+00 1.0000000E+00 1.0000000E-01 0.0
7.9840000E+01 4.1300000E+00 1.0000000E+00 1.0000000E-01 0.0
8.7600000E+01 3.8700000E+00 1.0000000E+00 1.0000000E-01 0.0
====== Outputs ====================================================================================
True SumPrint - Generate a summary file listing input options and interpolated properties to "
3 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, (-)
"RtAeroCp"
"RtAeroCt"
"RtAeroCq"
"RtTSR"
"RtSpeed, RtSkew, B1Azimuth"
"B1N1VDisx, B1N1VDisy, B1N1VDisz" ! disturbed wind velocity at Blade 1, Node 1
"B1N2VDisx, B1N2VDisy, B1N2VDisz" ! disturbed wind velocity at Blade 1, Node 2
"B1N3VDisx, B1N3VDisy, B1N3VDisz" ! disturbed wind velocity at Blade 1, Node 3
"B1N1STVx, B1N1STVy, B1N1STVz" ! structural translational velocity at Blade 1, Node 1
"B1N2STVx, B1N2STVy, B1N2STVz" ! structural translational velocity at Blade 1, Node 2
"B1N3STVx, B1N3STVy, B1N3STVz" ! structural translational velocity at Blade 1, Node 2
"B1N1AxInd, B1N2AxInd, B1N3AxInd"
"B1N1Alpha, B1N2Alpha, B1N3Alpha"
"B1N1Theta, B1N2Theta, B1N3Theta"
END of input file (the word "END" must appear in the first 3 columns of this last OutList line)
#### The following was for testing, but bloats the regression test case too much
#---------------------- NODE OUTPUTS --------------------------------------------
# 3 BldNd_BladesOut - Blades to output
# 99 BldNd_BlOutNd - Blade nodes on each blade (currently unused)
# OutList - The next line(s) contains a list of output parameters. See OutListParameters.xlsx, AeroDyn_Nodes tab for a listing of available output channels, (-)
#"VUndx" - x-component of undisturbed wind velocity at each node
#"VUndy" - y-component of undisturbed wind velocity at each node
#"VUndz" - z-component of undisturbed wind velocity at each node
#"VDisx" - x-component of disturbed wind velocity at each node
#"VDisy" - y-component of disturbed wind velocity at each node
#"VDisz" - z-component of disturbed wind velocity at each node
#"STVx" - x-component of structural translational velocity at each node
#"STVy" - y-component of structural translational velocity at each node
#"STVz" - z-component of structural translational velocity at each node
#"VRel" - Relvative wind speed at each node
#"DynP" - Dynamic pressure at each node
#"Re" - Reynolds number (in millions) at each node
#"M" - Mach number at each node
#"Vindx" - Axial induced wind velocity at each node
#"Vindy" - Tangential induced wind velocity at each node
#"AxInd" - Axial induction factor at each node
#"TnInd" - Tangential induction factor at each node
#"Alpha" - Angle of attack at each node
#"Theta" - Pitch+Twist angle at each node
#"Phi" - Inflow angle at each node
#"Curve" - Curvature angle at each node
#"Cl" - Lift force coefficient at each node
#"Cd" - Drag force coefficient at each node
#"Cm" - Pitching moment coefficient at each node
#"Cx" - Normal force (to plane) coefficient at each node
#"Cy" - Tangential force (to plane) coefficient at each node
#"Cn" - Normal force (to chord) coefficient at each node
#"Ct" - Tangential force (to chord) coefficient at each node
#"Fl" - Lift force per unit length at each node
#"Fd" - Drag force per unit length at each node
#"Mm" - Pitching moment per unit length at each node
#"Fx" - Normal force (to plane) per unit length at each node
#"Fy" - Tangential force (to plane) per unit length at each node
#"Fn" - Normal force (to chord) per unit length at each node
#"Ft" - Tangential force (to chord) per unit length at each node
#"Clrnc" - Tower clearance at each node (based on the absolute distance to the nearest point in the tower from blade node B#N# minus the local tower radius, in the deflected configuration); please note that this clearance is only approximate because the calculation assumes that the blade is a line with no volume (however, the calculation does use the local tower radius); when blade node B#N# is above the tower top (or below the tower base), the absolute distance to the tower top (or base) minus the local tower radius, in the deflected configuration, is output
#"Vx" - Local axial velocity
#"Vy" - Local tangential velocity
#"GeomPhi" - Geometric phi? If phi was solved using normal BEMT equations, GeomPhi = 1; otherwise, if it was solved geometrically, GeomPhi = 0.
#"Chi" - Skew angle (used in skewed wake correction) -- not available for OLAF
#"UA_Flag" - Flag indicating if UA is turned on for this node. -- not available for OLAF
#"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 -- not available for BEMT/DBEMT
#"Cd_Static" - Static portion of drag force coefficient at each node, without unsteady effects -- not available for BEMT/DBEMT
#"Cm_Static" - Static portion of pitching moment coefficient at each node, without unsteady effects -- not available for BEMT/DBEMT
#"Uin" - Axial induced velocity in rotating hub coordinates. Axial aligned with hub axis. rotor plane polar hub rotating coordinates
#"Uit" - Tangential induced velocity in rotating hub coordinates. Tangential to the rotation plane. Perpendicular to blade aziumth. rotor plane polar hub rotating coordinates
#"Uir" - Radial induced velocity in rotating hub coordinates. Radial outwards in rotation plane. Aligned with blade azimuth. rotor plane polar hub rotating coordinates
#END of input file (the word "END" must appear in the first 3 columns of this last OutList line)
#---------------------------------------------------------------------------------------
and in the airfoil input file we should call the airfoil cordinate file with file name or file path?
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