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Updates from welib and FAST.Farm examples on github action (#64)
* Updates from welib * Adding IEA15 model * Adding Example 0, update Example 1 so it can run on github action * Adapting Example 2 for FAST.Farm so it can run on github action * Adapting Example 3 for FAST.Farm so it can run on github action * Adding real_all io unittest, and verbose flag to unittest
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‎.github/workflows/development-pipeline.yml‎

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pip install -e .
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- name: Tests
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run: |
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python -m unittest discover
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python -m unittest discover -v

‎Makefile‎

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test:
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python -m unittest discover
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python -m unittest discover -v

‎data/IEA15MW/AD.dat‎

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------- AERODYN v15.03.* INPUT FILE ------------------------------------------------
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IEA 15 MW Offshore Reference Turbine
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====== General Options ============================================================================
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False Echo - Echo the input to "<rootname>.AD.ech"? (flag)
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Default DTAero - Time interval for aerodynamic calculations {or "default"} (s)
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1 Wake_Mod - Wake/induction model (switch) {0=none, 1=BEMT, 3=OLAF} [Wake_Mod cannot be 2 or 3 when linearizing]
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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}
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1 TwrShadow - Calculate tower influence on wind based on downstream tower shadow (switch) {0=none, 1=Powles model, 2=Eames model}
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True TwrAero - Calculate tower aerodynamic loads? (flag)
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False CavitCheck - Perform cavitation check? (flag) [UA_Mod must be 0 when CavitCheck=true]
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False Buoyancy - Include buoyancy effects? (flag)
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False NacelleDrag - Include Nacelle Drag effects? (flag)
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False CompAA - Flag to compute AeroAcoustics calculation [used only when Wake_Mod = 1 or 2]
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AeroAcousticsInput.dat AA_InputFile - AeroAcoustics input file [used only when CompAA=true]
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====== Environmental Conditions ===================================================================
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"default" AirDens - Air density (kg/m^3)
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"default" KinVisc - Kinematic viscosity of working fluid (m^2/s)
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"default" SpdSound - Speed of sound in working fluid (m/s)
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"default" Patm - Atmospheric pressure (Pa) [used only when CavitCheck=True]
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"default" Pvap - Vapour pressure of working fluid (Pa) [used only when CavitCheck=True]
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====== Blade-Element/Momentum Theory Options ====================================================== [unused when Wake_Mod=0 or 3, except for BEM_Mod]
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1 BEM_Mod - BEM model {1=legacy NoSweepPitchTwist, 2=polar} (switch) [used for all Wake_Mod to determine output coordinate system]
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--- Skew correction
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1 Skew_Mod - Skew model {0=No skew model, -1=Remove non-normal component for linearization, 1=skew model active}
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False SkewMomCorr - Turn the skew momentum correction on or off [used only when Skew_Mod=1]
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1 SkewRedistr_Mod - Type of skewed-wake correction model (switch) {0=no redistribution, 1=Glauert/Pitt/Peters, default=1} [used only when Skew_Mod=1]
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default SkewRedistrFactor - Constant used in Pitt/Peters skewed wake model {or "default" is 15/32*pi} (-) [used only when Skew_Mod=1 and SkewRedistr_Mod=1]
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--- BEM algorithm
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True TipLoss - Use the Prandtl tip-loss model? (flag) [unused when Wake_Mod=0 or 3]
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True HubLoss - Use the Prandtl hub-loss model? (flag) [unused when Wake_Mod=0 or 3]
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True TanInd - Include tangential induction in BEMT calculations? (flag) [unused when Wake_Mod=0 or 3]
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True AIDrag - Include the drag term in the axial-induction calculation? (flag) [unused when Wake_Mod=0 or 3]
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True TIDrag - Include the drag term in the tangential-induction calculation? (flag) [unused when Wake_Mod=0,3 or TanInd=FALSE]
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Default IndToler - Convergence tolerance for BEMT nonlinear solve residual equation {or "default"} (-) [unused when Wake_Mod=0 or 3]
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500 MaxIter - Maximum number of iteration steps (-) [unused when Wake_Mod=0]
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--- Shear correction
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False SectAvg - Use sector averaging (flag)
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1 SectAvgWeighting - Weighting function for sector average {1=Uniform, default=1} within a sector centered on the blade (switch) [used only when SectAvg=True]
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default SectAvgNPoints - Number of points per sectors (-) {default=5} [used only when SectAvg=True]
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default SectAvgPsiBwd - Backward azimuth relative to blade where the sector starts (<=0) {default=-60} (deg) [used only when SectAvg=True]
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default SectAvgPsiFwd - Forward azimuth relative to blade where the sector ends (>=0) {default=60} (deg) [used only when SectAvg=True]
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--- Dynamic wake/inflow
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2 DBEMT_Mod - Type of dynamic BEMT (DBEMT) model {0=No Dynamic Wake, -1=Frozen Wake for linearization, 1:constant tau1, 2=time-dependent tau1, 3=constant tau1 with continuous formulation} (-)
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29.03 tau1_const - Time constant for DBEMT (s) [used only when Wake_Mod=2 and DBEMT_Mod=1]
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====== OLAF -- cOnvecting LAgrangian Filaments (Free Vortex Wake) Theory Options ================== [used only when Wake_Mod=3]
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IEA-15-240-RWT_OLAF.dat OLAFInputFileName - Input file for OLAF [used only when Wake_Mod=3]
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====== Unsteady Airfoil Aerodynamics Options ====================================================
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True AoA34 - Sample the angle of attack (AoA) at the 3/4 chord or the AC point {default=True} [always used]
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4 UA_Mod - Unsteady Aero Model Switch (switch) {0=Quasi-steady (no UA), 2=B-L Gonzalez, 3=B-L Minnema/Pierce, 4=B-L HGM 4-states, 5=B-L HGM+vortex 5 states, 6=Oye, 7=Boeing-Vertol}
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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 UA_Mod>0]
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4 IntegrationMethod - Switch to indicate which integration method UA uses (1=RK4, 2=AB4, 3=ABM4, 4=BDF2)
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0.1 UAStartRad - Starting radius for dynamic stall (fraction of rotor radius [0.0,1.0]) [used only when UA_Mod>0; if line is missing UAStartRad=0]
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1 UAEndRad - Ending radius for dynamic stall (fraction of rotor radius [0.0,1.0]) [used only when UA_Mod>0; if line is missing UAEndRad=1]
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====== Airfoil Information =========================================================================
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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} (-)
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1 InCol_Alfa - The column in the airfoil tables that contains the angle of attack (-)
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2 InCol_Cl - The column in the airfoil tables that contains the lift coefficient (-)
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3 InCol_Cd - The column in the airfoil tables that contains the drag coefficient (-)
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4 InCol_Cm - The column in the airfoil tables that contains the pitching-moment coefficient; use zero if there is no Cm column (-)
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0 InCol_Cpmin - The column in the airfoil tables that contains the Cpmin coefficient; use zero if there is no Cpmin column (-)
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50 NumAFfiles - Number of airfoil files used (-)
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"Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_00.dat" AFNames - Airfoil file names (NumAFfiles lines) (quoted strings)
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"Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_01.dat"
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"Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_02.dat"
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"Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_03.dat"
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"Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_04.dat"
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"Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_05.dat"
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"Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_06.dat"
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"Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_07.dat"
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"Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_08.dat"
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"Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_09.dat"
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"Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_10.dat"
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"Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_11.dat"
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"Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_12.dat"
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"Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_13.dat"
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"Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_14.dat"
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"Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_15.dat"
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"Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_16.dat"
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"Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_17.dat"
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"Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_18.dat"
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"Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_19.dat"
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"Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_20.dat"
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"Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_21.dat"
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"Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_22.dat"
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"Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_23.dat"
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"Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_24.dat"
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"Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_25.dat"
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"Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_26.dat"
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"Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_27.dat"
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"Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_28.dat"
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"Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_29.dat"
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"Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_30.dat"
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"Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_31.dat"
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"Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_32.dat"
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"Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_33.dat"
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"Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_34.dat"
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"Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_35.dat"
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"Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_36.dat"
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"Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_37.dat"
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"Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_38.dat"
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"Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_39.dat"
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"Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_40.dat"
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"Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_41.dat"
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"Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_42.dat"
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"Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_43.dat"
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"Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_44.dat"
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"Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_45.dat"
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"Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_46.dat"
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"Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_47.dat"
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"Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_48.dat"
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"Airfoils/IEA-15-240-RWT_AeroDyn15_Polar_49.dat"
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====== Rotor/Blade Properties =====================================================================
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True UseBlCm - Include aerodynamic pitching moment in calculations? (flag)
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"IEA-15-240-RWT_AeroDyn15_blade.dat" ADBlFile(1) - Name of file containing distributed aerodynamic properties for Blade #1 (-)
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"IEA-15-240-RWT_AeroDyn15_blade.dat" ADBlFile(2) - Name of file containing distributed aerodynamic properties for Blade #2 (-) [unused if NumBl < 2]
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"IEA-15-240-RWT_AeroDyn15_blade.dat" ADBlFile(3) - Name of file containing distributed aerodynamic properties for Blade #3 (-) [unused if NumBl < 3]
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====== Hub Properties ============================================================================== [used only when Buoyancy=True]
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0 VolHub - Hub volume (m^3)
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0 HubCenBx - Hub center of buoyancy x direction offset (m)
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====== Nacelle Properties ========================================================================== [used only when Buoyancy=True or NacelleDrag=True]
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0 VolNac - Nacelle volume (m^3)
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0.0, 0.0, 0.0 NacCenB - Position of nacelle center of buoyancy from yaw bearing in nacelle coordinates (m)
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0, 0, 0 NacArea - Projected area of the nacelle in X, Y, Z in the nacelle coordinate system (m^2)
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0, 0, 0 NacCd - Drag coefficient for the nacelle areas defined above (-)
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0, 0, 0 NacDragAC - Position of aerodynamic center of nacelle drag in nacelle coordinates (m)
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====== Tail Fin Aerodynamics =======================================================================
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False TFinAero - Calculate tail fin aerodynamics model (flag)
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"unused" TFinFile - Input file for tail fin aerodynamics [used only when TFinAero=True]
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====== Tower Influence and Aerodynamics ============================================================ [used only when TwrPotent/=0, TwrShadow/=0, TwrAero=True, or Buoyancy=True]
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20 NumTwrNds - Number of tower nodes used in the analysis (-) [used only when TwrPotent/=0, TwrShadow/=0, or TwrAero=True]
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TwrElev TwrDiam TwrCd TwrTI TwrCb !TwrTI used only with TwrShadow=2, TwrCb used only with Buoyancy=True
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(m) (m) (-) (-) (-)
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15.000 10.000 0.5 0.1 0.0
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28.000 10.000 0.5 0.1 0.0
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28.001 10.000 0.5 0.1 0.0
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41.000 9.926 0.5 0.1 0.0
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41.001 9.926 0.5 0.1 0.0
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54.000 9.443 0.5 0.1 0.0
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54.001 9.443 0.5 0.1 0.0
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67.000 8.833 0.5 0.1 0.0
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67.001 8.833 0.5 0.1 0.0
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80.000 8.151 0.5 0.1 0.0
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80.001 8.151 0.5 0.1 0.0
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93.000 7.390 0.5 0.1 0.0
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93.001 7.390 0.5 0.1 0.0
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106.000 6.909 0.5 0.1 0.0
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106.001 6.909 0.5 0.1 0.0
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119.000 6.748 0.5 0.1 0.0
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119.001 6.748 0.5 0.1 0.0
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132.000 6.572 0.5 0.1 0.0
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132.001 6.572 0.5 0.1 0.0
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144.386 6.500 0.5 0.1 0.0
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====== Outputs ====================================================================================
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False SumPrint - Generate a summary file listing input options and interpolated properties to "<rootname>.AD.sum"? (flag)
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9 NBlOuts - Number of blade node outputs [0 - 9] (-)
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6, 11, 16, 21, 25, 30, 35, 40, 45 BlOutNd - Blade nodes whose values will be output (-)
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0 NTwOuts - Number of tower node outputs [0 - 9] (-)
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0 TwOutNd - Tower nodes whose values will be output (-)
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OutList - The next line(s) contains a list of output parameters. See OutListParameters.xlsx for a listing of available output channels, (-)
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"RtArea"
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"RtSpeed"
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"RtTSR"
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"RtSkew"
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"RtAeroFxh"
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"RtAeroFyh"
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"RtAeroFzh"
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"RtAeroMxh"
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"RtAeroMyh"
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"RtAeroMzh"
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"RtVAvgxh"
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"RtAeroPwr"
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"RtArea"
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"RtAeroCp"
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"RtAeroCq"
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"RtAeroCt"
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"RtAeroFxi"
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"RtAeroFyi"
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"RtAeroFzi"
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"RtAeroMxi"
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"RtAeroMyi"
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"RtAeroMzi"
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END of input file (the word "END" must appear in the first 3 columns of this last OutList line)
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====== Outputs for all blade stations (same ending as above for B1N1.... =========================== [optional section]
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1 BldNd_BladesOut - Number of blades to output all node information at. Up to number of blades on turbine. (-)
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"All" BldNd_BlOutNd - Future feature will allow selecting a portion of the nodes to output. Not implemented yet. (-)
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OutList - The next line(s) contains a list of output parameters. See OutListParameters.xlsx for a listing of available output channels, (-)
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END (the word "END" must appear in the first 3 columns of this last OutList line in the optional nodal output section)

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