GOE 803 (HACKLINGER) AIRFOIL (goe803h-il)
GOE 803 (HACKLINGER) AIRFOIL - Gottingen 803 (Hacklinger) airfoil
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(goe803h-il) GOE 803 (HACKLINGER) AIRFOIL Gottingen 803 (Hacklinger) airfoil Max thickness 6.3% at 15% chord. Max camber 6.6% at 40% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 803 (HACKLINGER) AIRFOIL
20. 20.
0.0000000 0.0000000
0.0050000 0.0128600
0.0100000 0.0194300
0.0150000 0.0243000
0.0200000 0.0284600
0.0250000 0.0318200
0.0500000 0.0466500
0.0750000 0.0579800
0.1000000 0.0665000
0.1500000 0.0789500
0.2000000 0.0856000
0.3000000 0.0919000
0.4000000 0.0922000
0.5000000 0.0865000
0.6000000 0.0758000
0.7000000 0.0611000
0.8000000 0.0444000
0.9000000 0.0257000
0.9500000 0.0163500
1.0000000 0.0030000
0.0000000 0.0000000
0.0050000 -.0093300
0.0100000 -.0118700
0.0150000 -.0125000
0.0200000 -.0122400
0.0250000 -.0116800
0.0500000 -.0053500
0.0750000 0.0009700
0.1000000 0.0063000
0.1500000 0.0159500
0.2000000 0.0236000
0.3000000 0.0349000
0.4000000 0.0412000
0.5000000 0.0425000
0.6000000 0.0428000
0.7000000 0.0381000
0.8000000 0.0294000
0.9000000 0.0167000
0.9500000 0.0083500
1.0000000 0.0000000
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Polars for GOE 803 (HACKLINGER) AIRFOIL (goe803h-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe803h-il | 50,000 | 9 | 40 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe803h-il | 50,000 | 5 | 48.1 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe803h-il | 100,000 | 9 | 69.1 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe803h-il | 100,000 | 5 | 69.7 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe803h-il | 200,000 | 9 | 95.6 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe803h-il | 200,000 | 5 | 85.8 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe803h-il | 500,000 | 9 | 112.9 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe803h-il | 500,000 | 5 | 103.6 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe803h-il | 1,000,000 | 9 | 128.7 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe803h-il | 1,000,000 | 5 | 122.2 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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