GOE 173 (ALBATROS 6020) AIRFOIL (goe173-il)
GOE 173 (ALBATROS 6020) AIRFOIL - Gottingen 173 (Albatros 6020) airfoil
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(goe173-il) GOE 173 (ALBATROS 6020) AIRFOIL Gottingen 173 (Albatros 6020) airfoil Max thickness 7.8% at 20% chord. Max camber 5.9% at 40% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 173 (ALBATROS 6020) AIRFOIL
17. 17.
0.0000000 0.0000000
0.0124100 0.0195600
0.0248600 0.0311100
0.0497800 0.0472300
0.0747300 0.0593400
0.0996800 0.0689600
0.1496200 0.0836900
0.1995800 0.0915200
0.2995600 0.0964800
0.3995600 0.0953400
0.4996000 0.0878000
0.5996500 0.0755600
0.6997200 0.0599200
0.7998000 0.0429800
0.8998900 0.0248400
0.9499400 0.0139700
1.0000000 0.0009000
0.0000000 0.0000000
0.0125300 -.0054400
0.0250200 -.0043800
0.0500100 -.0019700
0.0750000 0.0008400
0.0999800 0.0036600
0.1499600 0.0091900
0.1999400 0.0139200
0.2999100 0.0198800
0.3998900 0.0228400
0.4998900 0.0230000
0.5999100 0.0205600
0.6999199 0.0167200
0.7999500 0.0115800
0.8999700 0.0056400
0.9499900 0.0028700
1.0000000 -.0009000
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Polars for GOE 173 (ALBATROS 6020) AIRFOIL (goe173-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe173-il | 50,000 | 9 | 33.1 at α=10.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe173-il | 50,000 | 5 | 42.2 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe173-il | 100,000 | 9 | 56.9 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe173-il | 100,000 | 5 | 60.3 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe173-il | 200,000 | 9 | 77.7 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe173-il | 200,000 | 5 | 75.7 at α=2.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe173-il | 500,000 | 9 | 101.6 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe173-il | 500,000 | 5 | 101.5 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe173-il | 1,000,000 | 9 | 124.6 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe173-il | 1,000,000 | 5 | 122.3 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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