Fix moment dist calculation

Author: 1-Bart-1

src/solver.jl

@@ -266,7 +266,7 @@ function solve!(solver::Solver, body_aero::BodyAerodynamics, gamma_distribution=
 
         # Calculate the moment distribution (moment on each panel)
         arm = (moment_frac - 0.25) * panel.chord
-        moment_distribution[i] = (ftotal_induced_va ⋅ panel.z_airf) * arm
+        moment_distribution[i] = (ftotal_induced_va ⋅ panel.z_airf) * arm + moment[i] * panel.width
         moment_coefficient_distribution[i] = moment_distribution[i] / (q_inf * projected_area)
     end