GOE 329 (PFALZ 58) AIRFOIL (goe329-il)
GOE 329 (PFALZ 58) AIRFOIL - Gottingen 329 (Pfalz 58) airfoil
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(goe329-il) GOE 329 (PFALZ 58) AIRFOIL Gottingen 329 (Pfalz 58) airfoil Max thickness 10.2% at 29.9% chord. Max camber 5.5% at 29.9% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 329 (PFALZ 58) AIRFOIL
17. 17.
0.0000000 0.0000000
0.0123000 0.0203200
0.0247000 0.0304400
0.0495400 0.0466900
0.0744200 0.0592300
0.0993100 0.0701700
0.1491500 0.0870600
0.1990400 0.0979500
0.2989600 0.1061300
0.3989800 0.1039100
0.4990600 0.0963900
0.5991700 0.0847700
0.6993300 0.0685500
0.7995300 0.0482400
0.8997400 0.0263200
0.9498500 0.0151100
1.0000000 0.0030000
0.0000000 0.0000000
0.0126200 -.0126800
0.0251200 -.0120500
0.0500900 -.0096100
0.0750700 -.0072600
0.1000500 -.0055200
0.1500200 -.0020300
0.1999900 0.0011600
0.2999600 0.0045400
0.3999400 0.0056200
0.4999400 0.0058000
0.5999500 0.0047800
0.6999700 0.0030600
0.7999800 0.0019400
0.9000000 0.0002200
0.9500100 -.0007900
1.0000000 -.0030000
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Polars for GOE 329 (PFALZ 58) AIRFOIL (goe329-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe329-il | 50,000 | 9 | 23.6 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe329-il | 50,000 | 5 | 37.9 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe329-il | 100,000 | 9 | 53.3 at α=10° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe329-il | 100,000 | 5 | 56.2 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe329-il | 200,000 | 9 | 73.9 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe329-il | 200,000 | 5 | 75.2 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe329-il | 500,000 | 9 | 104.5 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe329-il | 500,000 | 5 | 103.3 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe329-il | 1,000,000 | 9 | 129.7 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe329-il | 1,000,000 | 5 | 125.4 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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