GOE 390 AIRFOIL (goe390-il)
GOE 390 AIRFOIL - Gottingen 390 airfoil
| Details | Dat file | Parser | |
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(goe390-il) GOE 390 AIRFOIL Gottingen 390 airfoil Max thickness 20.3% at 29.2% chord. Max camber 6.9% at 39.2% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 390 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0106900 0.0363300
0.0222600 0.0551100
0.0459200 0.0819800
0.0699600 0.1013800
0.0941800 0.1169900
0.1430700 0.1394200
0.1923400 0.1539700
0.2916400 0.1680100
0.3917100 0.1665900
0.4922700 0.1554900
0.5932900 0.1348200
0.6946300 0.1078600
0.7962400 0.0755100
0.8979900 0.0403800
0.9489800 0.0205100
1.0000000 0.0010500
0.0000000 0.0000000
0.0138000 -.0260100
0.0266400 -.0329700
0.0519800 -.0397100
0.0771000 -.0421600
0.1021900 -.0440200
0.1521400 -.0429300
0.2020300 -.0407500
0.3017200 -.0344900
0.4013900 -.0279300
0.5010500 -.0210700
0.6007200 -.0145100
0.7005000 -.0100500
0.8002900 -.0058900
0.9001700 -.0033200
0.9501200 -.0023300
1.0000000 -.0010500
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Polars for GOE 390 AIRFOIL (goe390-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe390-il | 50,000 | 9 | 3.8 at α=12° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe390-il | 50,000 | 5 | 11.3 at α=1.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe390-il | 100,000 | 9 | 26.1 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe390-il | 100,000 | 5 | 40.4 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe390-il | 200,000 | 9 | 62.9 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe390-il | 200,000 | 5 | 58.8 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe390-il | 500,000 | 9 | 85.2 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe390-il | 500,000 | 5 | 78.8 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe390-il | 1,000,000 | 9 | 105.5 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe390-il | 1,000,000 | 5 | 98.9 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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