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lines changed Original file line number Diff line number Diff line change @@ -76,7 +76,7 @@ Three kinds of input data is needed:
7676 - how many panels
7777 --> two sections make a panel.
7878
79- There is no input file yet, the input has to be defined in the code.
79+ Apart from the wing geometry there is no input file yet, the input has to be defined in the code.
8080
8181### Example for defining the required input:
8282``` julia
@@ -110,6 +110,7 @@ wa = WingAerodynamics([wing])
110110vel_app = [cos (alpha), 0.0 , sin (alpha)] .* Umag
111111set_va! (wa, (vel_app, 0.0 )) # Second parameter is yaw rate
112112```
113+ It is possible to import the wing geometry using an ` .obj ` file as shown in the example ` ram_air_kite.jl ` .
113114
114115Surfplan files can be converted to an input for ` VortexStepMethod.jl ` using the [ SurfplanAdapter] ( https://github.com/jellepoland/SurfplanAdapter ) .
115116
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