GOE 344 (PFALZ 71) AIRFOIL (goe344-il)
GOE 344 (PFALZ 71) AIRFOIL - Gottingen 344 (Pfalz 71) airfoil
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(goe344-il) GOE 344 (PFALZ 71) AIRFOIL Gottingen 344 (Pfalz 71) airfoil Max thickness 7.2% at 19.9% chord. Max camber 2.7% at 39.9% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 344 (PFALZ 71) AIRFOIL
17. 17.
0.0000000 0.0000000
0.0123400 0.0177100
0.0247700 0.0253200
0.0496900 0.0351400
0.0746200 0.0422700
0.0995800 0.0477900
0.1495200 0.0551400
0.1994700 0.0588900
0.2994600 0.0607800
0.3994700 0.0595800
0.4995100 0.0551700
0.5995600 0.0490700
0.6996300 0.0414600
0.7997100 0.0327600
0.8998200 0.0203500
0.9498800 0.0133000
1.0000000 0.0032500
0.0000000 0.0000000
0.0126300 -.0122900
0.0251400 -.0157700
0.0501700 -.0187500
0.0751700 -.0193300
0.1001700 -.0188000
0.1501400 -.0156600
0.2001200 -.0131100
0.3000700 -.0079100
0.4000500 -.0054200
0.5000500 -.0061200
0.6000800 -.0090300
0.7001000 -.0115300
0.8001100 -.0125400
0.9000900 -.0100400
0.9500600 -.0069000
1.0000000 -.0032500
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Polars for GOE 344 (PFALZ 71) AIRFOIL (goe344-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe344-il | 50,000 | 9 | 32.5 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe344-il | 50,000 | 5 | 34.4 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe344-il | 100,000 | 9 | 45.4 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe344-il | 100,000 | 5 | 47.2 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe344-il | 200,000 | 9 | 60.3 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe344-il | 200,000 | 5 | 60.1 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe344-il | 500,000 | 9 | 80.6 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe344-il | 500,000 | 5 | 77.1 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe344-il | 1,000,000 | 9 | 95.3 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe344-il | 1,000,000 | 5 | 89 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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