GOE 384 AIRFOIL (goe384-il)
GOE 384 AIRFOIL - Gottingen 384 airfoil
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(goe384-il) GOE 384 AIRFOIL Gottingen 384 airfoil Max thickness 19.6% at 29.3% chord. Max camber 6.9% at 39.3% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 384 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0111900 0.0323500
0.0230300 0.0487300
0.0470400 0.0731000
0.0711900 0.0942800
0.0955400 0.1101600
0.1446000 0.1334500
0.1939400 0.1498400
0.2933300 0.1649700
0.3933800 0.1637100
0.4938200 0.1528700
0.5947300 0.1303600
0.6957700 0.1046400
0.7970600 0.0726400
0.8985299 0.0363500
0.9492700 0.0181000
1.0000000 0.0021500
0.0000000 0.0000000
0.0133400 -.0207600
0.0261000 -.0271400
0.0512800 -.0315300
0.0763400 -.0331100
0.1013400 -.0332000
0.1513700 -.0337800
0.2013500 -.0333600
0.3012300 -.0304200
0.4010700 -.0263800
0.5009000 -.0223400
0.6007400 -.0183000
0.7005800 -.0142600
0.8004100 -.0102200
0.9002500 -.0061800
0.9501700 -.0041700
1.0000000 -.0021500
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Polars for GOE 384 AIRFOIL (goe384-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe384-il | 50,000 | 9 | 3.9 at α=12.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe384-il | 50,000 | 5 | 11.7 at α=1.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe384-il | 100,000 | 9 | 27.3 at α=2.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe384-il | 100,000 | 5 | 39.5 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe384-il | 200,000 | 9 | 63.4 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe384-il | 200,000 | 5 | 59.1 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe384-il | 500,000 | 9 | 87.1 at α=2° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe384-il | 500,000 | 5 | 78.4 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe384-il | 1,000,000 | 9 | 105.1 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe384-il | 1,000,000 | 5 | 100.5 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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