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Add test for second plot #40

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Merged
1-Bart-1 merged 2 commits into from
Feb 20, 2025
Merged

Add test for second plot #40

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62368ea
test second plot
ufechner7 Feb 20, 2025
a743eda
Update CI.yml
ufechner7 Feb 20, 2025
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4 changes: 2 additions & 2 deletions .github/workflows/CI.yml
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Original file line number Diff line number Diff line change
Expand Up @@ -31,14 +31,14 @@ jobs:
arch: x64
version: 1
- os: macOS-latest
arch: x64
arch: aarch64
version: 1
steps:
- name: Install matplotlib
run: if [ "$RUNNER_OS" = "Linux" ]; then sudo apt-get install -y python3-matplotlib; fi
shell: bash
- name: Install LaTeX
run: if [ "$RUNNER_OS" = "Linux" ]; then sudo apt-get -qq install texlive-full texlive-fonts-extra cm-super; fi
run: if [ "$RUNNER_OS" = "Linux" ]; then sudo apt-get -qq install texlive-full cm-super; fi
shell: bash
- uses: actions/checkout@v4
- uses: julia-actions/setup-julia@v2
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23 changes: 20 additions & 3 deletions test/test_plotting.jl
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Expand Up @@ -2,7 +2,7 @@ using VortexStepMethod
using ControlPlots
using Test

function result_vsm()
function create_wa()
# Step 1: Define wing parameters
n_panels = 20 # Number of panels
span = 20.0 # Wing span [m]
Expand Down Expand Up @@ -43,7 +43,7 @@ plt.ioff()
@test isfile("/tmp/plot.pdf")
rm("/tmp/plot.pdf")
show_plot(fig)
wa = result_vsm()
wa = create_wa()
if Sys.islinux()
fig = plot_geometry(
wa,
Expand All @@ -61,6 +61,23 @@ plt.ioff()
rm("/tmp/Rectangular_wing_geometry_side_view.pdf")
@test isfile("/tmp/Rectangular_wing_geometry_top_view.pdf")
rm("/tmp/Rectangular_wing_geometry_top_view.pdf")
# Step 5: Initialize the solvers
vsm_solver = Solver(aerodynamic_model_type="VSM")
llt_solver = Solver(aerodynamic_model_type="LLT")
# Step 6: Solve the VSM and LLT
results_vsm = solve(vsm_solver, wa)
results_llt = solve(llt_solver, wa)
# Step 7: Plot spanwise distributions
y_coordinates = [panel.aerodynamic_center[2] for panel in wa.panels]

fig = plot_distribution(
[y_coordinates, y_coordinates],
[results_vsm, results_llt],
["VSM", "LLT"],
title="Spanwise Distributions"
)
@test fig isa plt.PyPlot.Figure
end
end
plt.ion()
plt.ion()
nothing