GOE 770 AIRFOIL (goe770-il)
GOE 770 AIRFOIL - Gottingen 770 airfoil
| Details | Dat file | Parser | |
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(goe770-il) GOE 770 AIRFOIL Gottingen 770 airfoil Max thickness 21% at 30% chord. Max camber 4% at 30% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 770 AIRFOIL
16. 16.
0.0000000 0.0000000
0.0125000 0.0427200
0.0250000 0.0562300
0.0500000 0.0769600
0.1000000 0.1056200
0.1500000 0.1242800
0.2000000 0.1369400
0.3000000 0.1453600
0.4000000 0.1394800
0.5000000 0.1223000
0.6000000 0.0991200
0.7000000 0.0750400
0.8000000 0.0505600
0.9000000 0.0266800
0.9500000 0.0146400
1.0000000 0.0026000
0.0000000 0.0000000
0.0125000 -.0174800
0.0250000 -.0255700
0.0500000 -.0356400
0.1000000 -.0473800
0.1500000 -.0558200
0.2000000 -.0613600
0.3000000 -.0645400
0.4000000 -.0640200
0.5000000 -.0563000
0.6000000 -.0454800
0.7000000 -.0341600
0.8000000 -.0227400
0.9000000 -.0114200
0.9500000 -.0059600
1.0000000 0.0000000
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Polars for GOE 770 AIRFOIL (goe770-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe770-il | 50,000 | 9 | 2.9 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe770-il | 50,000 | 5 | 11.3 at α=2.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe770-il | 100,000 | 9 | 19.2 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe770-il | 100,000 | 5 | 36.6 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe770-il | 200,000 | 9 | 53.6 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe770-il | 200,000 | 5 | 59.3 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe770-il | 500,000 | 9 | 87.7 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe770-il | 500,000 | 5 | 86.1 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe770-il | 1,000,000 | 9 | 112.7 at α=8.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe770-il | 1,000,000 | 5 | 109 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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