GOE 433 AIRFOIL (goe433-il)
GOE 433 AIRFOIL - Gottingen 433 airfoil
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(goe433-il) GOE 433 AIRFOIL Gottingen 433 airfoil Max thickness 17.4% at 29.2% chord. Max camber 4.8% at 49.2% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 433 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0105700 0.0292000
0.0220900 0.0439700
0.0459400 0.0611500
0.0699500 0.0761400
0.0942000 0.0874500
0.1431200 0.1036000
0.1923400 0.1154700
0.2915400 0.1274600
0.3915600 0.1271000
0.4921600 0.1181800
0.5932800 0.1011900
0.6946200 0.0810200
0.7963099 0.0555700
0.8980700 0.0290300
0.9490300 0.0146200
1.0000000 0.0008000
0.0000000 0.0000000
0.0141200 -.0243600
0.0272700 -.0341900
0.0529800 -.0448800
0.0783400 -.0502000
0.1035500 -.0533200
0.1536400 -.0548000
0.2035700 -.0536800
0.3030400 -.0457800
0.4023000 -.0345900
0.5013200 -.0199100
0.6004600 -.0069300
0.6998800 0.0018700
0.7995099 0.0073900
0.8995301 0.0070300
0.9497800 0.0033700
1.0000000 -.0008000
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Polars for GOE 433 AIRFOIL (goe433-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe433-il | 50,000 | 9 | 5.7 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe433-il | 50,000 | 5 | 22.7 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe433-il | 100,000 | 9 | 48.2 at α=9.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe433-il | 100,000 | 5 | 53.1 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe433-il | 200,000 | 9 | 75.9 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe433-il | 200,000 | 5 | 71.9 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe433-il | 500,000 | 9 | 102.7 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe433-il | 500,000 | 5 | 89 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe433-il | 1,000,000 | 9 | 115.9 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe433-il | 1,000,000 | 5 | 100.3 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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