GOE 442 AIRFOIL (goe442-il)
GOE 442 AIRFOIL - Gottingen 442 airfoil
| Details | Dat file | Parser | |
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(goe442-il) GOE 442 AIRFOIL Gottingen 442 airfoil Max thickness 7.7% at 19.9% chord. Max camber 4.3% at 39.9% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 442 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0123100 0.0211100
0.0247200 0.0307200
0.0496000 0.0444500
0.0745200 0.0536700
0.0994600 0.0599000
0.1493800 0.0693400
0.1993200 0.0757900
0.2992800 0.0801900
0.3993000 0.0775900
0.4993600 0.0709900
0.5994300 0.0628900
0.6995300 0.0518000
0.7996600 0.0382000
0.8998100 0.0212000
0.9499000 0.0110500
1.0000000 0.0000000
0.0000000 0.0000000
0.0125600 -.0068900
0.0250800 -.0087700
0.0500800 -.0085500
0.0750700 -.0073200
0.1000600 -.0066000
0.1500400 -.0041500
0.2000100 -.0012000
0.2999500 0.0052000
0.3999200 0.0091000
0.4999000 0.0110000
0.5999000 0.0109000
0.6999199 0.0088000
0.7999400 0.0062000
0.8999800 0.0023000
0.9499900 0.0010500
1.0000000 0.0000000
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Polars for GOE 442 AIRFOIL (goe442-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe442-il | 50,000 | 9 | 35.3 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe442-il | 50,000 | 5 | 40.5 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe442-il | 100,000 | 9 | 54.3 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe442-il | 100,000 | 5 | 57.1 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe442-il | 200,000 | 9 | 73.4 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe442-il | 200,000 | 5 | 73 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe442-il | 500,000 | 9 | 97.6 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe442-il | 500,000 | 5 | 93 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe442-il | 1,000,000 | 9 | 115 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe442-il | 1,000,000 | 5 | 106.2 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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