GOE 381 AIRFOIL (goe381-il)
GOE 381 AIRFOIL - Gottingen 381 airfoil
| Details | Dat file | Parser | |
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(goe381-il) GOE 381 AIRFOIL Gottingen 381 airfoil Max thickness 6.4% at 30% chord. Max camber 5.8% at 30% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 381 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0124300 0.0162600
0.0248800 0.0271100
0.0498000 0.0434300
0.0747400 0.0571400
0.0997000 0.0653600
0.1496500 0.0773900
0.1996100 0.0837200
0.2995900 0.0894800
0.3995900 0.0883400
0.4996300 0.0807000
0.5996800 0.0703600
0.6997400 0.0570200
0.7998200 0.0398800
0.8999100 0.0203400
0.9499500 0.0103700
1.0000000 0.0008000
0.0000000 0.0000000
0.0125200 -.0053400
0.0250200 -.0038800
0.0500000 0.0002300
0.0749700 0.0057400
0.0999500 0.0115600
0.1499100 0.0195900
0.1999000 0.0225200
0.2998800 0.0256800
0.3998800 0.0261400
0.4998900 0.0239000
0.5999100 0.0195600
0.6999300 0.0143200
0.7999600 0.0096800
0.8999800 0.0041400
0.9499900 0.0016700
1.0000000 -.0008000
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Polars for GOE 381 AIRFOIL (goe381-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe381-il | 50,000 | 9 | 37.6 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe381-il | 50,000 | 5 | 43 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe381-il | 100,000 | 9 | 58.9 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe381-il | 100,000 | 5 | 61.5 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe381-il | 200,000 | 9 | 80 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe381-il | 200,000 | 5 | 76.4 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe381-il | 500,000 | 9 | 100.7 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe381-il | 500,000 | 5 | 92 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe381-il | 1,000,000 | 9 | 111.9 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe381-il | 1,000,000 | 5 | 93.1 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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