GOE 29B AIRFOIL (goe29b-il)
GOE 29B AIRFOIL - Gottingen 29B airfoil
| Details | Dat file | Parser | |
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(goe29b-il) GOE 29B AIRFOIL Gottingen 29B airfoil Max thickness 9.4% at 19.8% chord. Max camber 6.5% at 29.8% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 29B AIRFOIL
17. 17.
0.0000000 0.0000000
0.0120400 0.0248200
0.0242800 0.0389500
0.0488800 0.0600100
0.0736200 0.0743700
0.0984300 0.0843300
0.1481700 0.0986600
0.1980300 0.1056800
0.2979200 0.1120400
0.3980100 0.1072000
0.4982100 0.0962700
0.5985100 0.0802300
0.6988300 0.0630000
0.7992000 0.0428700
0.8995900 0.0218300
0.9497800 0.0115700
1.0000000 0.0014000
0.0000000 0.0000000
0.0128200 -.0169600
0.0253600 -.0195300
0.0503000 -.0162600
0.0751800 -.0096000
0.1000800 -.0042400
0.1499100 0.0050900
0.1997800 0.0116200
0.2996500 0.0189700
0.3996100 0.0208300
0.4996200 0.0204900
0.5996500 0.0186500
0.6997200 0.0153100
0.7998000 0.0108800
0.8999200 0.0042400
0.9499800 0.0011700
1.0000000 -.0014000
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Polars for GOE 29B AIRFOIL (goe29b-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe29b-il | 50,000 | 9 | 22.9 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe29b-il | 50,000 | 5 | 37.7 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe29b-il | 100,000 | 9 | 52.8 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe29b-il | 100,000 | 5 | 57.8 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe29b-il | 200,000 | 9 | 77.2 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe29b-il | 200,000 | 5 | 75 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe29b-il | 500,000 | 9 | 99.4 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe29b-il | 500,000 | 5 | 94.8 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe29b-il | 1,000,000 | 9 | 118.1 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe29b-il | 1,000,000 | 5 | 116.5 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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