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Copy file name to clipboardExpand all lines: docs/source/user/aerodyn/examples/NodalOutputs.txt
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@@ -41,7 +41,7 @@ END of input file (the word "END" must appear in the first 3 columns of this las
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"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
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"Vx" - Local axial velocity
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"Vy" - Local tangential velocity
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"GeomPhi" - Geometric phi? If phi was solved using normal BEMT equations, GeomPhi = 1; otherwise, if it was solved geometrically, GeomPhi = 0.
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"GeomPhi" - Geometric phi? If phi was solved using normal BEMT equations, GeomPhi = 0; otherwise, if it was solved geometrically, GeomPhi = 1.
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"Chi" - Skew angle (used in skewed wake correction) -- not available for OLAF
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"UA_Flag" - Flag indicating if UA is turned on for this node. -- not available for OLAF
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