GOE 744 AIRFOIL (goe744-il)
GOE 744 AIRFOIL - Gottingen 744 airfoil
| Details | Dat file | Parser | |
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(goe744-il) GOE 744 AIRFOIL Gottingen 744 airfoil Max thickness 14.5% at 20% chord. Max camber 7% at 30% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 744 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0125000 0.0346400
0.0250000 0.0507700
0.0500000 0.0735500
0.0750000 0.0913200
0.1000000 0.1053000
0.1500000 0.1249500
0.2000000 0.1360000
0.3000000 0.1418000
0.4000000 0.1313000
0.5000000 0.1084000
0.6000000 0.0809000
0.7000000 0.0520000
0.8000000 0.0263000
0.9000000 0.0077000
0.9500000 0.0022500
1.0000000 0.0000000
0.0000000 0.0000000
0.0125000 -.0188600
0.0250000 -.0217200
0.0500000 -.0214500
0.0750000 -.0206800
0.1000000 -.0189000
0.1500000 -.0145500
0.2000000 -.0088000
0.3000000 -.0015000
0.4000000 0.0011000
0.5000000 -.0018000
0.6000000 -.0074000
0.7000000 -.0118000
0.8000000 -.0132000
0.9000000 -.0106000
0.9500000 -.0065500
1.0000000 0.0000000
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Polars for GOE 744 AIRFOIL (goe744-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe744-il | 50,000 | 9 | 3.9 at α=10.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe744-il | 50,000 | 5 | 7.9 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe744-il | 100,000 | 9 | 5 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe744-il | 100,000 | 5 | 35.5 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe744-il | 200,000 | 9 | 56.8 at α=8.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe744-il | 200,000 | 5 | 64.8 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe744-il | 500,000 | 9 | 98.9 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe744-il | 500,000 | 5 | 97.3 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe744-il | 1,000,000 | 9 | 128.4 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe744-il | 1,000,000 | 5 | 114.9 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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