END of input file (the word "END" must appear in the first 3 columns of this last OutList line)
---------------------- NODE OUTPUTS --------------------------------------------
          3   BldNd_BladesOut  - Number of blades to output all node information at.  Up to number of blades on turbine. (-)
      "ALL"   BldNd_BlOutNd   - Specify a portion of the nodes to output. {"ALL", "Tip", "Root", or a list of node numbers} (-)
              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
"Fbn"       - Buoyant force normal to chord per unit length at each node
"Fbt"       - Buoyant force tangential to chord per unit length at each node
"Fbs"       - Buoyant spanwise force per unit length at each node
"Mbn"       - Buoyant moment normal to chord per unit length at each node
"Mbt"       - Buoyant moment tangential to chord per unit length at each node
"Mbs"       - Buoyant spanwise moment per unit length at each node
END of input file (the word "END" must appear in the first 3 columns of this last OutList line)
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