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lines changed Original file line number Diff line number Diff line change @@ -26,7 +26,7 @@ Represents a panel in a vortex step method simulation. All points and vectors ar
2626- `y_airf::MVec3`: Unit vector parallel to chord line
2727- `z_airf::MVec3`: Unit vector in spanwise direction
2828- `width::Float64`: Panel width
29- - `filaments::Vector{BoundFilament}`: Panel filaments
29+ - `filaments::Vector{BoundFilament}`: Panel filaments, see: [BoundFilament](@ref)
3030"""
3131mutable struct Panel
3232 TE_point_1:: MVec3
Original file line number Diff line number Diff line change @@ -7,10 +7,10 @@ Main solver structure for the Vortex Step Method.
77# Attributes
88
99## General settings
10- - `aerodynamic_model_type`::Symbol
11- - density::Float64
10+ - `aerodynamic_model_type`::Model: The model type, see: [Model](@ref)
11+ - density::Float64: Air density [kg/m³]
1212- `max_iterations`::Int64
13- - `allowed_error`::Float64
13+ - `allowed_error`::Float64: relative error
1414- `tol_reference_error`::Float64
1515- `relaxation_factor`::Float64
1616
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