WORTMANN FX L V-152 AIRFOIL (fxlv152-il)
WORTMANN FX L V-152 AIRFOIL - Wortmann FX L V-152 airfoil
| Details | Dat file | Parser | |
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(fxlv152-il) WORTMANN FX L V-152 AIRFOIL Wortmann FX L V-152 airfoil Max thickness 15.3% at 33.9% chord. Max camber 0% at 0% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
WORTMANN FX L V-152 AIRFOIL
49. 49.
0.000000 0.000000
0.001020 0.004400
0.004220 0.009200
0.009600 0.016000
0.017620 0.021800
0.026500 0.027600
0.038020 0.033200
0.051580 0.038800
0.066940 0.043800
0.084220 0.048800
0.103300 0.053400
0.124030 0.057600
0.146430 0.061400
0.170370 0.065000
0.195580 0.068400
0.222210 0.071000
0.249980 0.073400
0.278910 0.074800
0.308610 0.075800
0.339330 0.076400
0.370560 0.076400
0.402430 0.075400
0.434690 0.073600
0.467330 0.071000
0.499970 0.068000
0.532740 0.063800
0.565250 0.059000
0.597500 0.054200
0.629380 0.049000
0.660740 0.043800
0.691330 0.039200
0.721150 0.034200
0.749950 0.029600
0.777730 0.025800
0.804350 0.021800
0.829700 0.018200
0.853550 0.015000
0.875900 0.012400
0.896440 0.009800
0.915710 0.007600
0.932990 0.005800
0.948480 0.004600
0.961920 0.003400
0.973440 0.002400
0.982910 0.001800
0.990340 0.001200
0.995710 0.000800
0.998910 0.000400
1.000000 0.000000
0.000000 0.000000
0.000000 0.000000
0.001020 -0.004400
0.004220 -0.009200
0.009600 -0.016000
0.017620 -0.021800
0.026500 -0.027600
0.038020 -0.033200
0.051580 -0.038800
0.066940 -0.043800
0.084220 -0.048800
0.103300 -0.053400
0.124030 -0.057600
0.146430 -0.061400
0.170370 -0.065000
0.195580 -0.068400
0.222210 -0.071000
0.249980 -0.073400
0.278910 -0.074800
0.308610 -0.075800
0.339330 -0.076400
0.370560 -0.076400
0.402430 -0.075400
0.434690 -0.073600
0.467330 -0.071000
0.499970 -0.068000
0.532740 -0.063800
0.565250 -0.059000
0.597500 -0.054200
0.629380 -0.049000
0.660740 -0.043800
0.691330 -0.039200
0.721150 -0.034200
0.749950 -0.029600
0.777730 -0.025800
0.804350 -0.021800
0.829700 -0.018200
0.853550 -0.015000
0.875900 -0.012400
0.896440 -0.009800
0.915710 -0.007600
0.932990 -0.005800
0.948480 -0.004600
0.961920 -0.003400
0.973440 -0.002400
0.982910 -0.001800
0.990340 -0.001200
0.995710 -0.000800
0.998910 -0.000400
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Polars for WORTMANN FX L V-152 AIRFOIL (fxlv152-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| fxlv152-il | 50,000 | 9 | 27.1 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fxlv152-il | 50,000 | 5 | 27.4 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fxlv152-il | 100,000 | 9 | 42.6 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fxlv152-il | 100,000 | 5 | 38.2 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fxlv152-il | 200,000 | 9 | 52.3 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fxlv152-il | 200,000 | 5 | 45.3 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fxlv152-il | 500,000 | 9 | 59.9 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fxlv152-il | 500,000 | 5 | 53.9 at α=9.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fxlv152-il | 1,000,000 | 9 | 66.8 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fxlv152-il | 1,000,000 | 5 | 62.6 at α=8.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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