@@ -149,10 +149,11 @@ function solve!(solver::Solver, body_aero::BodyAerodynamics, gamma_distribution=
149149 log= false , reference_point= zeros (MVec3), moment_frac= 0.1 )
150150
151151 # calculate intermediate result
152- converged, reference_point, alpha_array, v_a_array, va_norm_array,
152+ reference_point, alpha_array, v_a_array, va_norm_array,
153153 va_unit_array, panels = solve_base (solver, body_aero, gamma_distribution;
154154 log, reference_point)
155155 gamma_new = solver. lr. gamma_new
156+ converged = solver. lr. converged
156157 if ! isnothing (solver. sol. gamma_distribution)
157158 solver. sol. gamma_distribution .= gamma_new
158159 else
@@ -312,7 +313,7 @@ A dictionary with the results.
312313function solve (solver:: Solver , body_aero:: BodyAerodynamics , gamma_distribution= nothing ;
313314 log= false , reference_point= zeros (MVec3))
314315 # calculate intermediate result
315- converged, reference_point, alpha_array, v_a_array, va_norm_array,
316+ reference_point, alpha_array, v_a_array, va_norm_array,
316317 va_unit_array, panels = solve_base (solver, body_aero, gamma_distribution;
317318 log, reference_point)
318319
@@ -400,7 +401,6 @@ function solve_base(solver::Solver, body_aero::BodyAerodynamics, gamma_distribut
400401
401402 # Return results
402403 return (
403- solver. lr. converged,
404404 reference_point,
405405 solver. lr. alpha_array,
406406 solver. lr. v_a_array,
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