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Expose alpha corrected (angle of attack of each panel) #167

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Merged
1-Bart-1 merged 1 commit into from
Apr 13, 2025
Merged

Expose alpha corrected (angle of attack of each panel) #167

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5 changes: 3 additions & 2 deletions src/solver.jl
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Original file line number Diff line number Diff line change
Expand Up @@ -6,6 +6,7 @@ Struct for storing the solution of the [solve!](@ref) function. Must contain all

# Attributes
- `panel_width_array`::Vector{Float64}: Width of the panels [m]
- `alpha_array`::Vector{Float64}: Angle of attack of each panel relative to the apparent wind [rad]
- cl_array::Vector{Float64}: Lift coefficients of the panels [-]
- cd_array::Vector{Float64}: Drag coefficients of the panels [-]
- cm_array::Vector{Float64}: Pitching moment coefficients of the panels [-]
Expand All @@ -32,6 +33,7 @@ Struct for storing the solution of the [solve!](@ref) function. Must contain all
_chord_array::Vector{Float64} = zeros(P)
### end of private vectors
panel_width_array::Vector{Float64} = zeros(P)
alpha_array::Vector{Float64} = zeros(P)
cl_array::Vector{Float64} = zeros(P)
cd_array::Vector{Float64} = zeros(P)
cm_array::Vector{Float64} = zeros(P)
Expand Down Expand Up @@ -123,7 +125,6 @@ sol::VSMSolution = VSMSolution(): The result of calling [solve!](@ref)
br::BaseResult{P} = BaseResult{P}()
cache::Vector{PreallocationTools.LazyBufferCache{typeof(identity), typeof(identity)}} = [LazyBufferCache() for _ in 1:11]
cache_base::Vector{PreallocationTools.LazyBufferCache{typeof(identity), typeof(identity)}} = [LazyBufferCache()]
cache_solve::Vector{PreallocationTools.LazyBufferCache{typeof(identity), typeof(identity)}} = [LazyBufferCache()]
cache_lin::Vector{PreallocationTools.LazyBufferCache{typeof(identity), typeof(identity)}} = [LazyBufferCache() for _ in 1:4]

# Solution
Expand Down Expand Up @@ -175,7 +176,7 @@ function solve!(solver::Solver, body_aero::BodyAerodynamics, gamma_distribution=
cm_array = solver.sol.cm_array
converged = solver.lr.converged
alpha_array = solver.lr.alpha_array
alpha_corrected = solver.cache_solve[1][alpha_array]
alpha_corrected = solver.sol.alpha_array
v_a_array = solver.lr.v_a_array
panels = body_aero.panels

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