GOE 238 (HANSA-BRANDENBURG) AIRFOIL (goe238-il)
GOE 238 (HANSA-BRANDENBURG) AIRFOIL - Gottingen 238 (HANSA-BRANDENBURG) airfoil
| Details | Dat file | Parser | |
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(goe238-il) GOE 238 (HANSA-BRANDENBURG) AIRFOIL Gottingen 238 (HANSA-BRANDENBURG) airfoil Max thickness 9.8% at 29.8% chord. Max camber 5.5% at 29.8% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 238 (HANSA-BRANDENBURG) AIRFOIL
17. 17.
0.0000000 0.0000000
0.0121300 0.0236900
0.0244700 0.0337800
0.0492600 0.0476700
0.0740700 0.0595600
0.0989100 0.0698400
0.1486800 0.0847200
0.1985400 0.0937000
0.2983800 0.1041500
0.3984200 0.1010200
0.4986200 0.0885800
0.5988900 0.0708400
0.6992000 0.0510100
0.7995000 0.0322700
0.8997400 0.0166400
0.9498600 0.0091200
1.0000000 0.0000000
0.0000000 0.0000000
0.0127200 -.0140000
0.0252400 -.0152100
0.0501900 -.0122200
0.0751400 -.0092300
0.1001200 -.0078400
0.1500400 -.0028600
0.1999700 0.0016200
0.2999100 0.0060800
0.3998900 0.0073400
0.4999100 0.0057000
0.5999500 0.0031600
0.6999800 0.0010200
0.8000100 -.0005200
0.9000000 0.0000400
0.9500100 -.0004800
1.0000000 0.0000000
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Polars for GOE 238 (HANSA-BRANDENBURG) AIRFOIL (goe238-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe238-il | 50,000 | 9 | 9.8 at α=-3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe238-il | 50,000 | 5 | 24.1 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe238-il | 100,000 | 9 | 51.2 at α=10.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe238-il | 100,000 | 5 | 55.1 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe238-il | 200,000 | 9 | 80.8 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe238-il | 200,000 | 5 | 80.8 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe238-il | 500,000 | 9 | 117.1 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe238-il | 500,000 | 5 | 110 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe238-il | 1,000,000 | 9 | 143.6 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe238-il | 1,000,000 | 5 | 130.2 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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