GOE 510 AIRFOIL (goe510-il)
GOE 510 AIRFOIL - Gottingen 510 airfoil
| Details | Dat file | Parser | |
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(goe510-il) GOE 510 AIRFOIL Gottingen 510 airfoil Max thickness 13.7% at 19.7% chord. Max camber 5.8% at 39.7% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 510 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0122400 0.0218800
0.0242300 0.0350300
0.0487100 0.0585700
0.0733600 0.0746100
0.0980900 0.0866600
0.1477100 0.1042500
0.1974600 0.1153400
0.2972500 0.1250400
0.3972900 0.1232400
0.4974500 0.1159400
0.5977400 0.1026500
0.6981199 0.0853600
0.7986100 0.0630700
0.8992100 0.0357800
0.9495800 0.0188900
1.0000000 0.0000000
0.0000000 0.0000000
0.0130400 -.0209900
0.0255800 -.0264400
0.0506200 -.0283900
0.0756300 -.0288400
0.1006300 -.0287900
0.1505800 -.0261900
0.2004800 -.0215900
0.3002400 -.0108900
0.4001400 -.0062000
0.5002000 -.0090000
0.6002900 -.0132900
0.7003300 -.0150900
0.8002800 -.0128900
0.9001700 -.0077000
0.9500800 -.0036000
1.0000000 0.0000000
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Polars for GOE 510 AIRFOIL (goe510-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe510-il | 50,000 | 9 | 8.4 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe510-il | 50,000 | 5 | 29.5 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe510-il | 100,000 | 9 | 48.4 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe510-il | 100,000 | 5 | 48.1 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe510-il | 200,000 | 9 | 65.9 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe510-il | 200,000 | 5 | 61.6 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe510-il | 500,000 | 9 | 84.8 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe510-il | 500,000 | 5 | 82.4 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe510-il | 1,000,000 | 9 | 106.9 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe510-il | 1,000,000 | 5 | 99.5 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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