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Updates to branch, fixing regression
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mclarke2 committed Dec 4, 2022
1 parent f370aac commit 17d6de8
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Showing 7 changed files with 235 additions and 315 deletions.
27 changes: 14 additions & 13 deletions regression/scripts/Vehicles/Propellers/APC_11x4_Propeller.py
Expand Up @@ -34,8 +34,8 @@ def APC_11x4_Propeller():
[0.2952380952380953, 21.8436873747495 ],[0.3500000000000001, 20.741482965931866 ],[0.4023809523809523, 19.138276553106213 ],
[0.44761904761904736, 17.434869739478955 ],[0.5, 15.6312625250501 ],[0.5500000000000003, 14.07815631262525 ],
[0.6000000000000001, 12.725450901803606 ],[0.6499999999999999, 11.57314629258517 ],[0.6976190476190478, 10.470941883767534 ],
[0.7476190476190476, 9.569138276553108 ], [0.7976190476190479, 8.667334669338675 ],[0.8500000000000001, 7.665330661322642 ],
[0.8999999999999999, 6.6633266533066156 ],[0.9500000000000002, 5.360721442885772 ],[0.99, 3.9579158316633247 ]])
[0.7476190476190476, 9.569138276553108 ], [0.7976190476190479, 8.667334669338675 ],[0.8500000000000001, 7.665330661322642 ],
[0.8999999999999999, 6.6633266533066156 ],[0.9500000000000002, 5.360721442885772 ],[0.99, 3.9579158316633247 ]])

r_R = dimensionless_radius_chord[:,0]
b_R = dimensionless_radius_chord[:,1]
Expand All @@ -56,16 +56,17 @@ def APC_11x4_Propeller():
prop.radius_distribution = r_R*prop.tip_radius
prop.mid_chord_alignment = np.zeros_like(prop.chord_distribution)
prop.thickness_to_chord = prop.max_thickness_distribution/prop.chord_distribution
ospath = os.path.abspath(__file__)
separator = os.path.sep
rel_path = os.path.dirname(ospath) + separator
airfoil = SUAVE.Components.Airfoils.Airfoil()
airfoil.coordinate_file = rel_path +'../Airfoils/Clark_y.txt'
airfoil.polar_files = [rel_path +'../Airfoils/Polars/Clark_y_polar_Re_50000.txt',
rel_path +'../Airfoils/Polars/Clark_y_polar_Re_100000.txt',rel_path +'../Airfoils/Polars/Clark_y_polar_Re_200000.txt',
rel_path +'../Airfoils/Polars/Clark_y_polar_Re_500000.txt',rel_path +'../Airfoils/Polars/Clark_y_polar_Re_1000000.txt']
airfoil.geometry = import_airfoil_geometry(airfoil.coordinate_file,airfoil.number_of_points)
airfoil.polars = compute_airfoil_properties(airfoil.geometry,airfoil.polar_files)
ospath = os.path.abspath(__file__)
separator = os.path.sep
rel_path = os.path.dirname(ospath) + separator
airfoil = SUAVE.Components.Airfoils.Airfoil()
airfoil.number_of_points = 300
airfoil.coordinate_file = rel_path +'../Airfoils/Clark_y.txt'
airfoil.polar_files = [rel_path +'../Airfoils/Polars/Clark_y_polar_Re_50000.txt',
rel_path +'../Airfoils/Polars/Clark_y_polar_Re_100000.txt',rel_path +'../Airfoils/Polars/Clark_y_polar_Re_200000.txt',
rel_path +'../Airfoils/Polars/Clark_y_polar_Re_500000.txt',rel_path +'../Airfoils/Polars/Clark_y_polar_Re_1000000.txt']
airfoil.geometry = import_airfoil_geometry(airfoil.coordinate_file,airfoil.number_of_points)
airfoil.polars = compute_airfoil_properties(airfoil.geometry,airfoil.polar_files)
prop.append_airfoil(airfoil)
prop.airfoil_polar_stations = list(np.zeros(len(prop.radius_distribution)).astype(int))
prop.airfoil_polar_stations = list(np.zeros(len(prop.radius_distribution)).astype(int))
return prop
150 changes: 75 additions & 75 deletions regression/scripts/airfoil_import/Transition1.txt
Expand Up @@ -6,99 +6,99 @@ Airfoil Transition 1 between Clark_y.txt and E63.txt
0.0010333445462750398 0.0029214569119531074
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1.0 -0.00039933333333333335
154 changes: 77 additions & 77 deletions regression/scripts/airfoil_import/Transition2.txt
Expand Up @@ -2,103 +2,103 @@ Airfoil Transition 2 between Clark_y.txt and E63.txt
61. 61.

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0.0006618401905067536 -0.0003483181868544319
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