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examples/rectangular_wing.jl

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@@ -40,6 +40,8 @@ vsm_solver = Solver(aerodynamic_model_type="VSM")
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@time results_llt = solve(llt_solver, wa)
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@time results_vsm = solve(vsm_solver, wa)
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@time results_vsm = solve(vsm_solver, wa)
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# time Python: 32.0ms
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# time Julia: 1.5ms
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# Print results comparison
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println("\nLifting Line Theory Results:")

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