GOE 481 AIRFOIL (goe481-il)
GOE 481 AIRFOIL - Gottingen 481 airfoil
| Details | Dat file | Parser | |
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(goe481-il) GOE 481 AIRFOIL Gottingen 481 airfoil Max thickness 13.4% at 9.6% chord. Max camber 8.8% at 39.4% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 481 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0111400 0.0290200
0.0229300 0.0440800
0.0469600 0.0647100
0.0713000 0.0788500
0.0957500 0.0905000
0.1450000 0.1063200
0.1944700 0.1176400
0.2939700 0.1283200
0.3939600 0.1285200
0.4943000 0.1212300
0.5948600 0.1094600
0.6955700 0.0941900
0.7965300 0.0739400
0.8978500 0.0457000
0.9487300 0.0270900
1.0000000 0.0000000
0.0000000 0.0000000
0.0138600 -.0288500
0.0267000 -.0362400
0.0520000 -.0425600
0.0770600 -.0438800
0.1020300 -.0432000
0.1498800 0.0025400
0.1986200 0.0293400
0.2978900 0.0450000
0.3977600 0.0476900
0.4978400 0.0459000
0.5980700 0.0411100
0.6984600 0.0328300
0.7989600 0.0220500
0.8995200 0.0102800
0.9498100 0.0041400
1.0000000 0.0000000
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Polars for GOE 481 AIRFOIL (goe481-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe481-il | 50,000 | 9 | 7 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe481-il | 50,000 | 5 | 28.9 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe481-il | 100,000 | 9 | 43 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe481-il | 100,000 | 5 | 41.1 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe481-il | 200,000 | 9 | 53.4 at α=9.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe481-il | 200,000 | 5 | 48.9 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe481-il | 500,000 | 9 | 63.4 at α=9.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe481-il | 500,000 | 5 | 58.3 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe481-il | 1,000,000 | 9 | 70.3 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe481-il | 1,000,000 | 5 | 63.8 at α=10° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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