GOE 804 (EA 8) AIRFOIL (goe804-il)
GOE 804 (EA 8) AIRFOIL - Gottingen 804 (EA 8) airfoil
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(goe804-il) GOE 804 (EA 8) AIRFOIL Gottingen 804 (EA 8) airfoil Max thickness 6% at 40% chord. Max camber 6.3% at 50% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 804 (EA 8) AIRFOIL
16. 16.
0.0000000 0.0000000
0.0250000 0.0231800
0.0500000 0.0343500
0.0750000 0.0435200
0.1000000 0.0507000
0.1500000 0.0630500
0.2000000 0.0714000
0.3000000 0.0841000
0.4000000 0.0898000
0.5000000 0.0915000
0.6000000 0.0872000
0.7000000 0.0779000
0.8000000 0.0616000
0.9000000 0.0363000
0.9500000 0.0206500
1.0000000 0.0000000
0.0000000 0.0000000
0.0250000 -.0058200
0.0500000 -.0036500
0.0750000 -.0004700
0.1000000 0.0037000
0.1500000 0.0100500
0.2000000 0.0164000
0.3000000 0.0241000
0.4000000 0.0298000
0.5000000 0.0335000
0.6000000 0.0342000
0.7000000 0.0319000
0.8000000 0.0286000
0.9000000 0.0223000
0.9500000 0.0146500
1.0000000 0.0000000
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Polars for GOE 804 (EA 8) AIRFOIL (goe804-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe804-il | 50,000 | 9 | 43.7 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe804-il | 50,000 | 5 | 41.1 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe804-il | 100,000 | 9 | 70.6 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe804-il | 100,000 | 5 | 67.6 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe804-il | 200,000 | 9 | 107.1 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe804-il | 200,000 | 5 | 107 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe804-il | 500,000 | 9 | 169.1 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe804-il | 500,000 | 5 | 157.3 at α=1.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe804-il | 1,000,000 | 9 | 211.4 at α=1.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe804-il | 1,000,000 | 5 | 147 at α=0° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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