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Commit 668a387

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improve docstrings
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src/solver.jl

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@@ -49,6 +49,7 @@ end
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log=false, reference_point=zeros(MVec3))
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Main solving routine for the aerodynamic model. Reference point is in the kite body (KB) frame.
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See also: [solve](@ref)
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# Arguments:
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- solver::Solver: The solver to use, could be a VSM or LLT solver. See: [Solver](@ref)

src/wing_geometry.jl

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@@ -112,7 +112,8 @@ function init!(wing::AbstractWing; aero_center_location::Float64=0.25, control_p
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end
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"""
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add_section!(wing::Wing, LE_point::PosVector, TE_point::PosVector, aero_model, aero_data)
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add_section!(wing::Wing, LE_point::PosVector, TE_point::PosVector,
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aero_model, aero_data::AeroData=nothing)
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Add a new section to the wing.
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