GOE 703 AIRFOIL (goe703-il)
GOE 703 AIRFOIL - Gottingen 703 airfoil
| Details | Dat file | Parser | |
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(goe703-il) GOE 703 AIRFOIL Gottingen 703 airfoil Max thickness 19.4% at 30% chord. Max camber 2.3% at 30% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 703 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0125000 0.0305000
0.0250000 0.0435000
0.0500000 0.0610000
0.0750000 0.0750000
0.1000000 0.0850000
0.1500000 0.1000000
0.2000000 0.1105000
0.3000000 0.1200000
0.4000000 0.1185000
0.5000000 0.1080000
0.6000000 0.0915000
0.7000000 0.0720000
0.8000000 0.0490000
0.9000000 0.0255000
0.9500000 0.0135000
1.0000000 0.0000000
0.0000000 0.0000000
0.0125000 -.0275000
0.0250000 -.0360000
0.0500000 -.0465000
0.0750000 -.0540000
0.1000000 -.0595000
0.1500000 -.0665000
0.2000000 -.0705000
0.3000000 -.0740000
0.4000000 -.0750000
0.5000000 -.0730000
0.6000000 -.0680000
0.7000000 -.0595000
0.8000000 -.0460000
0.9000000 -.0260000
0.9500000 -.0135000
1.0000000 0.0000000
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Polars for GOE 703 AIRFOIL (goe703-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe703-il | 50,000 | 9 | 5.5 at α=0.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe703-il | 50,000 | 5 | 22.3 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe703-il | 100,000 | 9 | 40 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe703-il | 100,000 | 5 | 43 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe703-il | 200,000 | 9 | 63.3 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe703-il | 200,000 | 5 | 49.1 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe703-il | 500,000 | 9 | 67 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe703-il | 500,000 | 5 | 57.4 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe703-il | 1,000,000 | 9 | 75.5 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe703-il | 1,000,000 | 5 | 65.6 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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