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rename more to body
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examples/ram_air_kite.jl

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@@ -54,7 +54,7 @@ plot && plot_geometry(
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results = solve(VSM, body_aero)
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@time results = solve(VSM, body_aero)
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CAD_y_coordinates = [panel.aero_center[2] for panel in body_aero.panels]
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body_y_coordinates = [panel.aero_center[2] for panel in body_aero.panels]
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plot && plot_distribution(
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[CAD_y_coordinates],

src/panel.jl

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@@ -3,7 +3,7 @@ using LinearAlgebra
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"""
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Panel
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Represents a panel in a vortex step method simulation.
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Represents a panel in a vortex step method simulation. All points and vectors are in the kite body (KB) frame.
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# Fields
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- `TE_point_1::MVec3`: First trailing edge point

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