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1 parent 4785db6 commit 7996139Copy full SHA for 7996139
examples_cp/rectangular_wing.jl
@@ -48,9 +48,9 @@ vsm_solver = Solver(body_aero; aerodynamic_model_type=VSM)
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# Step 5: Solve using both methods
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results_llt = solve(llt_solver, body_aero)
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-@time results_llt = solve(llt_solver, body_aero)
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results_vsm = solve(vsm_solver, body_aero)
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-@time results_vsm = solve(vsm_solver, body_aero)
+@time solve(llt_solver, body_aero)
+@time solve(vsm_solver, body_aero)
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# Print results comparison
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println("\nLifting Line Theory Results:")
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