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working example 26
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mayankchetan authored and dzalkind committed Jan 22, 2025
1 parent 923352f commit 5861088
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4 changes: 3 additions & 1 deletion Examples/.gitignore
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*.p
examples_out/
examples_out/
11_robust_tuning_out
*.10
4 changes: 2 additions & 2 deletions Examples/Test_Cases/MHK_RM1/MHK_RM1_Floating.fst
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Expand Up @@ -14,7 +14,7 @@ False Echo - Echo input data to <RootName>.ech (flag)
1 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}
0 CompSeaSt - Compute sea state information (switch) {0=None; 1=SeaState}
1 CompSeaSt - Compute sea state information (switch) {0=None; 1=SeaState}
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}
Expand All @@ -38,7 +38,7 @@ False Echo - Echo input data to <RootName>.ech (flag)
"MHK_RM1_Floating_InflowWind.dat" InflowFile - Name of file containing inflow wind input parameters (quoted string)
"MHK_RM1_Floating_AeroDyn15.dat" AeroFile - Name of file containing aerodynamic input parameters (quoted string)
"MHK_RM1_ServoDyn.dat" ServoFile - Name of file containing control and electrical-drive input parameters (quoted string)
"unused" SeaStFile - Name of file containing sea state input parameters (quoted string)
"MHK_RM1_Floating_SeaState.dat" SeaStFile - Name of file containing sea state input parameters (quoted string)
"MHK_RM1_Floating_HydroDyn.dat" HydroFile - Name of file containing hydrodynamic input parameters (quoted string)
"unused" SubFile - Name of file containing sub-structural input parameters (quoted string)
"MHK_RM1_Floating_MoorDyn.dat" MooringFile - Name of file containing mooring system input parameters (quoted string)
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2 changes: 1 addition & 1 deletion Examples/Test_Cases/MHK_RM1/MHK_RM1_Floating_AeroDyn15.dat
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Expand Up @@ -46,7 +46,7 @@ default SectAvgPsiFwd - Forward azimuth relative to blade where t
"unused" OLAFInputFileName - Input file for OLAF [used only when WakeMod=3]
====== Unsteady Airfoil Aerodynamics Options ====================================================
True AoA34 - Sample the angle of attack (AoA) at the 3/4 chord or the AC point {default=True} [always used]
3 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}
0 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}
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]
3 IntegrationMethod - Switch to indicate which integration method UA uses (1=RK4, 2=AB4, 3=ABM4, 4=BDF2)
0 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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