WORTMANN FX 71-120 AIRFOIL (fx71120-il)
WORTMANN FX 71-120 AIRFOIL - Wortmann FX 71-120 airfoil
| Details | Dat file | Parser | |
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(fx71120-il) WORTMANN FX 71-120 AIRFOIL Wortmann FX 71-120 airfoil Max thickness 12% at 25% chord. Max camber 0% at 0% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
WORTMANN FX 71-120 AIRFOIL
43.0 43.0
0.0000000 0.0000000
0.0010700 0.0071400
0.0042800 0.0140800
0.0096100 0.0211800
0.0170400 0.0281200
0.0265300 0.0348200
0.0380600 0.0406900
0.0515600 0.0444300
0.0669900 0.0478800
0.0842700 0.0507200
0.1033200 0.0532300
0.1240800 0.0553100
0.1464500 0.0570800
0.1703300 0.0583300
0.1956200 0.0593100
0.2222100 0.0598300
0.2500000 0.0599300
0.2788600 0.0598300
0.3086600 0.0593700
0.3392800 0.0586200
0.3705900 0.0576300
0.4024500 0.0562700
0.4347400 0.0546600
0.4673000 0.0527500
0.5000000 0.0507200
0.5327000 0.0483600
0.5652600 0.0459500
0.5975500 0.0433100
0.6294100 0.0405300
0.6607200 0.0377100
0.6913400 0.0347800
0.7211400 0.0317900
0.7500000 0.0287900
0.7777900 0.0258300
0.8043800 0.0229300
0.8296700 0.0201100
0.8535500 0.0174500
0.8759200 0.0149300
0.9157300 0.0103700
0.9484400 0.0065500
0.9734700 0.0034400
0.9903900 0.0009500
1.0000000 0.0000000
0.0000000 0.0000000
0.0010700 -.0071400
0.0042800 -.0140800
0.0096100 -.0211800
0.0170400 -.0281200
0.0265300 -.0348200
0.0380600 -.0406900
0.0515600 -.0444300
0.0669900 -.0478800
0.0842700 -.0507200
0.1033200 -.0532300
0.1240800 -.0553100
0.1464500 -.0570800
0.1703300 -.0583300
0.1956200 -.0593100
0.2222100 -.0598300
0.2500000 -.0599300
0.2788600 -.0598300
0.3086600 -.0593700
0.3392800 -.0586200
0.3705900 -.0576300
0.4024500 -.0562700
0.4347400 -.0546600
0.4673000 -.0527500
0.5000000 -.0507200
0.5327000 -.0483600
0.5652600 -.0459500
0.5975500 -.0433100
0.6294100 -.0405300
0.6607200 -.0377100
0.6913400 -.0347800
0.7211400 -.0317900
0.7500000 -.0287900
0.7777900 -.0258300
0.8043800 -.0229300
0.8296700 -.0201100
0.8535500 -.0174500
0.8759200 -.0149300
0.9157300 -.0103700
0.9484400 -.0065500
0.9734700 -.0034400
0.9903900 -.0009500
1.0000000 0.0000000
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Polars for WORTMANN FX 71-120 AIRFOIL (fx71120-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| fx71120-il | 50,000 | 9 | 20.3 at α=2.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx71120-il | 50,000 | 5 | 21.2 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx71120-il | 100,000 | 9 | 26.3 at α=2° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx71120-il | 100,000 | 5 | 29.1 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx71120-il | 200,000 | 9 | 34.5 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx71120-il | 200,000 | 5 | 38.9 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx71120-il | 500,000 | 9 | 50.3 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx71120-il | 500,000 | 5 | 56.3 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx71120-il | 1,000,000 | 9 | 64.4 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx71120-il | 1,000,000 | 5 | 71.8 at α=8.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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