GOE 330 (PFALZ 59) AIRFOIL (goe330-il)
GOE 330 (PFALZ 59) AIRFOIL - Gottingen 330 (Pfalz 59) airfoil
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(goe330-il) GOE 330 (PFALZ 59) AIRFOIL Gottingen 330 (Pfalz 59) airfoil Max thickness 10.2% at 29.9% chord. Max camber 5.8% at 39.9% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 330 (PFALZ 59) AIRFOIL
17. 17.
0.0000000 0.0000000
0.0122600 0.0206400
0.0246400 0.0312800
0.0494400 0.0490700
0.0742800 0.0623500
0.0991500 0.0735400
0.1489900 0.0882100
0.1988700 0.0984900
0.2987600 0.1074400
0.3987700 0.1065900
0.4988400 0.1009400
0.5989800 0.0888900
0.6991500 0.0735400
0.7994000 0.0521900
0.8996700 0.0283500
0.9498300 0.0149200
1.0000000 0.0005000
0.0000000 0.0000000
0.0126200 -.0106500
0.0251300 -.0117100
0.0501200 -.0107200
0.0750900 -.0076400
0.1000700 -.0058500
0.1500300 -.0022700
0.2000000 0.0003000
0.2999400 0.0054500
0.3999000 0.0086000
0.4998800 0.0107500
0.5998700 0.0109000
0.6999000 0.0090500
0.7999300 0.0062000
0.9000000 0.0003500
0.9500000 -.0000700
1.0000000 -.0005000
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Polars for GOE 330 (PFALZ 59) AIRFOIL (goe330-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe330-il | 50,000 | 9 | 24.8 at α=12° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe330-il | 50,000 | 5 | 38.4 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe330-il | 100,000 | 9 | 56.1 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe330-il | 100,000 | 5 | 58.6 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe330-il | 200,000 | 9 | 78.3 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe330-il | 200,000 | 5 | 75.3 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe330-il | 500,000 | 9 | 103.9 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe330-il | 500,000 | 5 | 101.6 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe330-il | 1,000,000 | 9 | 128.1 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe330-il | 1,000,000 | 5 | 121.9 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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