Minor documentation bugs

docs/source/user/aerodyn/examples/NodalOutputs.txt

@@ -41,7 +41,7 @@ END of input file (the word "END" must appear in the first 3 columns of this las
 "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.
+"GeomPhi"   - Geometric phi? If phi was solved using normal BEMT equations, GeomPhi = 0; otherwise, if it was solved geometrically, GeomPhi = 1.
 "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

docs/source/user/hydrodyn/index.rst

@@ -37,7 +37,6 @@ of HydroDyn.
 - :download:`Implementation Plan - 2nd-order Forces Within HydroDyn <../../../OtherSupporting/HydroDyn/HydroDyn_2ndOrderForces_Plan.pdf>`
 - :download:`Implementation Plan - 2nd-order Wave Kinematics Within HydroDyn <../../../OtherSupporting/HydroDyn/WAVE2_document.pdf>`
 - :download:`Plan for Adding Wave Stretching to HydroDyn <../../../OtherSupporting/HydroDyn/HydroDyn_WaveStretching_Plan.docx>`
-- :download:`Breaking Wave Modeling Approach for FAST <../../../OtherSupporting/HydroDyn/Breaking_Wave_Modeling_Approach_for_FAST.docx>`
 
 
 HydroDyn allows for multiple approaches for calculating the hydrodynamic

openfast_io/openfast_io/FAST_vars_out.py

@@ -9328,7 +9328,7 @@
 AeroDyn_Nodes['Ft']           = False     # (N/m); Tangential force (to chord) per unit length at each node - Negative along ya!; airfoil coordinate system
 AeroDyn_Nodes['Gam']          = False     # (m^2/s); Gamma -- circulation on blade; about za, airfoil coordinate system
 AeroDyn_Nodes['Clrnc']        = False     # (m); 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; 
-AeroDyn_Nodes['GeomPhi']      = False     # (1/0); Geometric phi? If phi was solved using normal BEMT equations, GeomPhi = 1; otherwise, if it was solved geometrically, GeomPhi = 0.; 
+AeroDyn_Nodes['GeomPhi']      = False     # (1/0); Geometric phi? If phi was solved using normal BEMT equations, GeomPhi = 0; otherwise, if it was solved geometrically, GeomPhi = 1.; 
 AeroDyn_Nodes['Chi']          = False     # (deg); Skew angle (used in skewed wake correction); 
 AeroDyn_Nodes['UA_Flag']      = False     # (-); Flag indicating if UA is turned on for this node.; 
 AeroDyn_Nodes['UA_x1']        = False     # (rad); time-history of wake vorticity contributing to effective angle of attack;