GOE 184 (MVA H.29) AIRFOIL (goe184-il)
GOE 184 (MVA H.29) AIRFOIL - Gottingen 184 (MVA H.29) airfoil
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(goe184-il) GOE 184 (MVA H.29) AIRFOIL Gottingen 184 (MVA H.29) airfoil Max thickness 8.3% at 19.9% chord. Max camber 5.3% at 39.9% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 184 (MVA H.29) AIRFOIL
17. 17.
0.0000000 0.0000000
0.0122000 0.0202800
0.0245700 0.0294600
0.0493400 0.0449200
0.0741900 0.0553800
0.0990600 0.0641500
0.1488900 0.0760700
0.1987600 0.0852000
0.2986600 0.0916600
0.3986900 0.0898200
0.4988100 0.0814800
0.5989700 0.0706400
0.6991900 0.0555100
0.7994300 0.0390700
0.8996900 0.0209400
0.9498400 0.0110700
1.0000000 0.0011000
0.0000000 0.0000000
0.0126400 -.0099200
0.0251300 -.0117300
0.0502000 -.0138700
0.0751600 -.0112000
0.1001300 -.0086400
0.1500400 -.0029100
0.1999700 0.0023200
0.2998400 0.0110800
0.3997700 0.0159400
0.4997600 0.0162000
0.5997900 0.0143600
0.6998300 0.0113200
0.7999000 0.0071800
0.8999500 0.0036400
0.9499800 0.0015700
1.0000000 -.0011000
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Polars for GOE 184 (MVA H.29) AIRFOIL (goe184-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe184-il | 50,000 | 9 | 34 at α=10° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe184-il | 50,000 | 5 | 39.5 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe184-il | 100,000 | 9 | 57.4 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe184-il | 100,000 | 5 | 60.4 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe184-il | 200,000 | 9 | 79.4 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe184-il | 200,000 | 5 | 79.4 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe184-il | 500,000 | 9 | 107.5 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe184-il | 500,000 | 5 | 102.7 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe184-il | 1,000,000 | 9 | 127.7 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe184-il | 1,000,000 | 5 | 111.9 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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