GOE 693 AIRFOIL (goe693-il)
GOE 693 AIRFOIL - Gottingen 693 airfoil
| Details | Dat file | Parser | |
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(goe693-il) GOE 693 AIRFOIL Gottingen 693 airfoil Max thickness 12% at 30% chord. Max camber 3.6% at 40% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 693 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0125000 0.0204300
0.0250000 0.0303600
0.0500000 0.0452300
0.0750000 0.0555900
0.1000000 0.0644500
0.1500000 0.0761700
0.2000000 0.0855000
0.3000000 0.0943500
0.4000000 0.0963000
0.5000000 0.0922500
0.6000000 0.0817000
0.7000000 0.0666500
0.8000000 0.0491000
0.9000000 0.0285500
0.9500000 0.0167800
1.0000000 0.0050000
0.0000000 0.0000000
0.0125000 -.0160700
0.0250000 -.0216400
0.0500000 -.0272700
0.0750000 -.0299100
0.1000000 -.0305500
0.1500000 -.0303300
0.2000000 -.0291000
0.3000000 -.0256500
0.4000000 -.0222000
0.5000000 -.0187500
0.6000000 -.0153000
0.7000000 -.0118500
0.8000000 -.0084000
0.9000000 -.0049500
0.9500000 -.0027300
1.0000000 0.0000000
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Polars for GOE 693 AIRFOIL (goe693-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe693-il | 50,000 | 9 | 32.3 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe693-il | 50,000 | 5 | 35.6 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe693-il | 100,000 | 9 | 56 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe693-il | 100,000 | 5 | 55.7 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe693-il | 200,000 | 9 | 78.2 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe693-il | 200,000 | 5 | 72.5 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe693-il | 500,000 | 9 | 103.2 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe693-il | 500,000 | 5 | 87.2 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe693-il | 1,000,000 | 9 | 115.5 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe693-il | 1,000,000 | 5 | 97.3 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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