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lines changed Original file line number Diff line number Diff line change @@ -25,10 +25,10 @@ Represents a panel in a vortex step method simulation.
2525- `filaments::Vector{BoundFilament}`: Panel filaments
2626"""
2727mutable struct Panel
28- TE_point_1:: Vector{Float64}
29- LE_point_1:: Vector{Float64}
30- TE_point_2:: Vector{Float64}
31- LE_point_2:: Vector{Float64}
28+ TE_point_1:: MVec3
29+ LE_point_1:: MVec3
30+ TE_point_2:: MVec3
31+ LE_point_2:: MVec3
3232 chord:: Float64
3333 va:: Union{Nothing,Vector{Float64}}
3434 corner_points:: Matrix{Float64}
@@ -37,13 +37,13 @@ mutable struct Panel
3737 cd_coefficients:: Union{Nothing,Vector{Float64}}
3838 cm_coefficients:: Union{Nothing,Vector{Float64}}
3939 panel_polar_data:: Union{Nothing,Matrix{Float64}}
40- aerodynamic_center:: Vector{Float64}
41- control_point:: Vector{Float64}
42- bound_point_1:: Vector{Float64}
43- bound_point_2:: Vector{Float64}
44- x_airf:: Vector{Float64}
45- y_airf:: Vector{Float64}
46- z_airf:: Vector{Float64}
40+ aerodynamic_center:: MVec3
41+ control_point:: MVec3
42+ bound_point_1:: MVec3
43+ bound_point_2:: MVec3
44+ x_airf:: MVec3
45+ y_airf:: MVec3
46+ z_airf:: MVec3
4747 width:: Float64
4848 filaments:: Vector{Union{BoundFilament, SemiInfiniteFilament}}
4949
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