GOE 534 AIRFOIL (goe534-il)
GOE 534 AIRFOIL - Gottingen 534 airfoil
| Details | Dat file | Parser | |
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(goe534-il) GOE 534 AIRFOIL Gottingen 534 airfoil Max thickness 14.1% at 19.6% chord. Max camber 5.2% at 39.6% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 534 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0111700 0.0374000
0.0231100 0.0533200
0.0474200 0.0726800
0.0719600 0.0855500
0.0966300 0.0949300
0.1462000 0.1071900
0.1959700 0.1134600
0.2958800 0.1160000
0.3961300 0.1090600
0.4965700 0.0966300
0.5971200 0.0812000
0.6978800 0.0620600
0.7985000 0.0423500
0.8992000 0.0224200
0.9495800 0.0117100
1.0000000 0.0000000
0.0000000 0.0000000
0.0130700 -.0160400
0.0257800 -.0220800
0.0510400 -.0291900
0.0760900 -.0308000
0.1011200 -.0314100
0.1510900 -.0306400
0.2009700 -.0273700
0.3006000 -.0168300
0.4001500 -.0042900
0.4997600 0.0067400
0.5995500 0.0127800
0.6995300 0.0133300
0.7996700 0.0093900
0.8998600 0.0039500
0.9499600 0.0012200
1.0000000 0.0000000
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Polars for GOE 534 AIRFOIL (goe534-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe534-il | 50,000 | 9 | 20 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe534-il | 50,000 | 5 | 32.5 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe534-il | 100,000 | 9 | 44 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe534-il | 100,000 | 5 | 50.2 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe534-il | 200,000 | 9 | 65.4 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe534-il | 200,000 | 5 | 67.4 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe534-il | 500,000 | 9 | 93.2 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe534-il | 500,000 | 5 | 91 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe534-il | 1,000,000 | 9 | 114.9 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe534-il | 1,000,000 | 5 | 110.2 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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