@@ -26,7 +26,7 @@ Struct for storing the solution of the [solve!](@ref) function. Must contain all
2626@with_kw mutable struct VSMSolution{P}
2727 # ## private vectors of solve_base!
2828 _x_airf_array:: Matrix{Float64} = zeros(P, 3 )
29- y_airf_array :: Matrix{Float64} = zeros(P, 3 )
29+ _y_airf_array :: Matrix{Float64} = zeros(P, 3 )
3030 z_airf_array:: Matrix{Float64} = zeros(P, 3 )
3131 va_array:: Matrix{Float64} = zeros(P, 3 )
3232 chord_array:: Vector{Float64} = zeros(P)
@@ -339,7 +339,7 @@ function solve(solver::Solver, body_aero::BodyAerodynamics, gamma_distribution=n
339339 solver. lr. v_a_array,
340340 solver. sol. chord_array,
341341 solver. sol. _x_airf_array,
342- solver. sol. y_airf_array ,
342+ solver. sol. _y_airf_array ,
343343 solver. sol. z_airf_array,
344344 solver. sol. va_array,
345345 solver. br. va_norm_array,
@@ -369,15 +369,15 @@ function solve_base!(solver::Solver, body_aero::BodyAerodynamics, gamma_distribu
369369
370370 # Clear arrays
371371 solver. sol. _x_airf_array .= 0
372- solver. sol. y_airf_array .= 0
372+ solver. sol. _y_airf_array .= 0
373373 solver. sol. z_airf_array .= 0
374374 solver. sol. va_array .= 0
375375 solver. sol. chord_array .= 0
376376
377377 # Fill arrays from panels
378378 for (i, panel) in enumerate(panels)
379379 solver. sol. _x_airf_array[i, :] .= panel. x_airf
380- solver. sol. y_airf_array [i, :] .= panel. y_airf
380+ solver. sol. _y_airf_array [i, :] .= panel. y_airf
381381 solver. sol. z_airf_array[i, :] .= panel. z_airf
382382 solver. sol. va_array[i, :] .= panel. va
383383 solver. sol. chord_array[i] = panel. chord
@@ -436,7 +436,7 @@ function gamma_loop!(
436436 va_array = solver. sol. va_array
437437 chord_array = solver. sol. chord_array
438438 x_airf_array = solver. sol. _x_airf_array
439- y_airf_array = solver. sol. y_airf_array
439+ y_airf_array = solver. sol. _y_airf_array
440440 z_airf_array = solver. sol. z_airf_array
441441 solver. lr. converged = false
442442 n_panels = length(body_aero. panels)
0 commit comments