Cleanup

Author: ufechner7

src/body_aerodynamics.jl

@@ -441,27 +441,6 @@ function update_effective_angle_of_attack!(alpha_corrected,
 
     # Calculate AIC matrices (keep existing optimized view)
     calculate_AIC_matrices!(body_aero, LLT, core_radius_fraction, va_norm_array, va_unit_array)
-    # AIC_x, AIC_y, AIC_z = @views body_aero.AIC[1, :, :], body_aero.AIC[2, :, :], body_aero.AIC[3, :, :]
-
-    # # Preallocate and calculate induced velocity directly
-    # # TODO rewrite
-    # induced_velocity = cache_body[1][va_array]
-    # induced_velocity[:, 1] .= AIC_x * gamma              # 304 bytes
-    # induced_velocity[:, 2] .= AIC_y * gamma
-    # induced_velocity[:, 3] .= AIC_z * gamma
-
-    # # Get views of AIC matrices without copying
-    # AIC_views = (@view(body_aero.AIC[1, :, :]), 
-    #              @view(body_aero.AIC[2, :, :]), 
-    #              @view(body_aero.AIC[3, :, :]))
-
-    # # Preallocate induced velocity array
-    # induced_velocity = cache_body[1][va_array]
-
-    # # Calculate induced velocity components in-place
-    # for (j, aic) in enumerate(AIC_views)                     # 384 allocated
-    #     mul!(@view(induced_velocity[:, j]), aic, gamma)
-    # end
 
     # Get dimensions from existing data
     n_rows = size(body_aero.AIC, 2)

test/bench.jl

@@ -7,7 +7,7 @@ using BenchmarkTools
 using StaticArrays
 using VortexStepMethod
 using VortexStepMethod: calculate_AIC_matrices!, gamma_loop!, calculate_results,
-                       update_effective_angle_of_attack_if_VSM, calculate_projected_area,
+                       update_effective_angle_of_attack!, calculate_projected_area,
                        calculate_cl, calculate_cd_cm,
                        calculate_velocity_induced_single_ring_semiinfinite!,
                        calculate_velocity_induced_bound_2D!,