Clean up test folder, move non-tests to examples folders

sandialabs · Jun 14, 2024 · 872cd0c · 872cd0c
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diff --git a/test/Example34mHVAWTConfiguration.jl → ...es/SNL34m/Example34mHVAWTConfiguration.jl b/test/Example34mHVAWTConfiguration.jl → ...es/SNL34m/Example34mHVAWTConfiguration.jl
diff --git a/...ravity_Fig4.4_Steady40RPMCentrifugalGX.jl → ...ravity_Fig4.4_Steady40RPMCentrifugalGX.jl b/...ravity_Fig4.4_Steady40RPMCentrifugalGX.jl → ...ravity_Fig4.4_Steady40RPMCentrifugalGX.jl
diff --git a/test/Fig5_11_EmergStop_torque_flatwise.jl → ...L34m/Fig5_11_EmergStop_torque_flatwise.jl b/test/Fig5_11_EmergStop_torque_flatwise.jl → ...L34m/Fig5_11_EmergStop_torque_flatwise.jl
diff --git a/...ation_torque_flatwise_generatorControl.jl → ...ation_torque_flatwise_generatorControl.jl b/...ation_torque_flatwise_generatorControl.jl → ...ation_torque_flatwise_generatorControl.jl
diff --git a/test/SNL34mVAWTNormalOperation.jl → examples/SNL34m/SNL34mVAWTNormalOperation.jl b/test/SNL34mVAWTNormalOperation.jl → examples/SNL34m/SNL34mVAWTNormalOperation.jl
diff --git a/test/SNL34m_Inputs.yml → examples/SNL34m/SNL34m_Inputs.yml b/test/SNL34m_Inputs.yml → examples/SNL34m/SNL34m_Inputs.yml
diff --git a/test/SNL34m_InputsAeroDyn.yml → examples/SNL34m/SNL34m_InputsAeroDyn.yml b/test/SNL34m_InputsAeroDyn.yml → examples/SNL34m/SNL34m_InputsAeroDyn.yml
diff --git a/examples/SNL34m/airfoils/Airfoils.txt b/examples/SNL34m/airfoils/Airfoils.txt
@@ -0,0 +1,39 @@
+04/10/97
+
+Coordinates for the SNL airfoils:
+
+	SNL 0015/47	SNL 0018/50	SNL 0021/50
+	X	(Y	X	(Y	X	(Y
+0.00000	0.00000	0.00000	0.00000	0.00000	0.00000
+0.00020	0.00166	0.00337	0.00646	0.00343	0.00790
+0.00508	0.01091	0.01274	0.01431	0.01291	0.01728
+0.01507	0.02060	0.02713	0.02282	0.02740	0.02735
+0.02872	0.02867	0.04621	0.03160	0.04653	0.03771
+0.04729	0.03615	0.06970	0.04042	0.07001	0.04806
+0.07062	0.04329	0.09730	0.04903	0.09753	0.05814
+0.09832	0.05006	0.12870	0.05726	0.12878	0.06772
+0.13002	0.05630	0.16353	0.06491	0.16339	0.07660
+0.16533	0.06192	0.20142	0.07183	0.20098	0.08460
+0.20386	0.06678	0.24193	0.07786	0.24113	0.09152
+0.24517	0.07080	0.28464	0.08283	0.28339	0.09721
+0.28880	0.07383	0.32907	0.08663	0.32730	0.10149
+0.33426	0.07575	0.37471	0.08908	0.37235	0.10417
+0.38104	0.07643	0.42107	0.09000	0.41805	0.10507
+0.42860	0.07556	0.46759	0.08902	0.46384	0.10379
+0.47688	0.07272	0.51422	0.08561	0.50965	0.09968
+0.52610	0.06808	0.56140	0.07982	0.55603	0.09272
+0.57603	0.06216	0.60914	0.07234	0.60311	0.08368
+0.62618	0.05535	0.65698	0.06379	0.65048	0.07323
+0.67600	0.04801	0.70440	0.05462	0.69767	0.06193
+0.72489	0.04046	0.75083	0.04535	0.74412	0.05037
+0.77244	0.03306	0.79560	0.03642	0.78921	0.03911
+0.81734	0.02608	0.83798	0.02827	0.83220	0.02869
+0.85951	0.01979	0.87718	0.02125	0.87224	0.01959
+0.89801	0.01441	0.91233	0.01562	0.90843	0.01217
+0.93212	0.01005	0.94258	0.01150	0.93980	0.00663
+0.96114	0.00676	0.96711	0.00881	0.96541	0.00296
+0.98447	0.00448	0.98519	0.00740	0.98439	0.00095
+0.99685	0.00349	0.99627	0.00687	0.99606	0.00015
+1.00000	0.00000	1.00000	0.00678	1.00000	0.00000
+
+The 18/50 was thickened up near the trailing edge so we could actually build it (we can't make a razor-edged extrusion).  Although we had to do a similar thing with the other two airfoils when we built models, I don't have those coordinates available.