GOE 326 (PFALZ 55) AIRFOIL (goe326-il)
GOE 326 (PFALZ 55) AIRFOIL - Gottingen 326 (Pfalz 55) airfoil
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(goe326-il) GOE 326 (PFALZ 55) AIRFOIL Gottingen 326 (Pfalz 55) airfoil Max thickness 8.2% at 29.9% chord. Max camber 4.7% at 39.9% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 326 (PFALZ 55) AIRFOIL
17. 17.
0.0000000 0.0000000
0.0132100 0.0197000
0.0247300 0.0295300
0.0496100 0.0440000
0.0745100 0.0538800
0.0994400 0.0613000
0.1493300 0.0736600
0.1992700 0.0815000
0.2992000 0.0877200
0.3992200 0.0860300
0.4992800 0.0789400
0.5993700 0.0690500
0.6995100 0.0541700
0.7996500 0.0380800
0.8998200 0.0198900
0.9499000 0.0112400
1.0000000 0.0015000
0.0000000 0.0000000
0.0125900 -.0094000
0.0250900 -.0106000
0.0500800 -.0085400
0.0750600 -.0064200
0.1000400 -.0046900
0.1500200 -.0012300
0.1999800 0.0018200
0.2999500 0.0059300
0.3999200 0.0084400
0.4999200 0.0088500
0.5999300 0.0073600
0.6999500 0.0053700
0.7999800 0.0024800
0.9000000 0.0000900
0.9500100 -.0009500
1.0000000 -.0015000
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Polars for GOE 326 (PFALZ 55) AIRFOIL (goe326-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe326-il | 50,000 | 9 | 32.5 at α=9.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe326-il | 50,000 | 5 | 40 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe326-il | 100,000 | 9 | 56.3 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe326-il | 100,000 | 5 | 59.1 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe326-il | 200,000 | 9 | 77.2 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe326-il | 200,000 | 5 | 77.2 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe326-il | 500,000 | 9 | 104.6 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe326-il | 500,000 | 5 | 100.1 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe326-il | 1,000,000 | 9 | 123.9 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe326-il | 1,000,000 | 5 | 116.7 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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