WORTMANN FX 71-089A AIRFOIL (fx71089a-il)
WORTMANN FX 71-089A AIRFOIL - Wortmann FX 71-089A airfoil
| Details | Dat file | Parser | |
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(fx71089a-il) WORTMANN FX 71-089A AIRFOIL Wortmann FX 71-089A airfoil Max thickness 8.9% at 22.2% chord. Max camber 0% at 0% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
WORTMANN FX 71-089A AIRFOIL
43.0 43.0
0.0000000 0.0000000
0.0010700 0.0062000
0.0042800 0.0122000
0.0096100 0.0180400
0.0170400 0.0238100
0.0265300 0.0281800
0.0380600 0.0311600
0.0515600 0.0341100
0.0669900 0.0364600
0.0842700 0.0386500
0.1033200 0.0403700
0.1240800 0.0417100
0.1464500 0.0429100
0.1703300 0.0437600
0.1956200 0.0443500
0.2222100 0.0446800
0.2500000 0.0446700
0.2788600 0.0445600
0.3086600 0.0441600
0.3392800 0.0435900
0.3705900 0.0428000
0.4024500 0.0417900
0.4347400 0.0405700
0.4673000 0.0391500
0.5000000 0.0376300
0.5327000 0.0358600
0.5652600 0.0340600
0.5975500 0.0320900
0.6294100 0.0300500
0.6607200 0.0279400
0.6913400 0.0257900
0.7211400 0.0235600
0.7500000 0.0213300
0.7777900 0.0191200
0.8043800 0.0170100
0.8296700 0.0149100
0.8535500 0.0129500
0.8759200 0.0110700
0.9157300 0.0076900
0.9484400 0.0048700
0.9734700 0.0025700
0.9903900 0.0008800
1.0000000 0.0000000
0.0000000 0.0000000
0.0010700 -.0062000
0.0042800 -.0122000
0.0096100 -.0180400
0.0170400 -.0238100
0.0265300 -.0281800
0.0380600 -.0311600
0.0515600 -.0341100
0.0669900 -.0364600
0.0842700 -.0386500
0.1033200 -.0403700
0.1240800 -.0417100
0.1464500 -.0429100
0.1703300 -.0437600
0.1956200 -.0443500
0.2222100 -.0446800
0.2500000 -.0446700
0.2788600 -.0445600
0.3086600 -.0441600
0.3392800 -.0435900
0.3705900 -.0428000
0.4024500 -.0417900
0.4347400 -.0405700
0.4673000 -.0391500
0.5000000 -.0376300
0.5327000 -.0358600
0.5652600 -.0340600
0.5975500 -.0320900
0.6294100 -.0300500
0.6607200 -.0279400
0.6913400 -.0257900
0.7211400 -.0235600
0.7500000 -.0213300
0.7777900 -.0191200
0.8043800 -.0170100
0.8296700 -.0149100
0.8535500 -.0129500
0.8759200 -.0110700
0.9157300 -.0076900
0.9484400 -.0048700
0.9734700 -.0025700
0.9903900 -.0008800
1.0000000 0.0000000
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Polars for WORTMANN FX 71-089A AIRFOIL (fx71089a-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| fx71089a-il | 50,000 | 9 | 19.7 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx71089a-il | 50,000 | 5 | 19.6 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx71089a-il | 100,000 | 9 | 25.6 at α=2° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx71089a-il | 100,000 | 5 | 26.9 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx71089a-il | 200,000 | 9 | 31.3 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx71089a-il | 200,000 | 5 | 36.4 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx71089a-il | 500,000 | 9 | 46.1 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx71089a-il | 500,000 | 5 | 52.3 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx71089a-il | 1,000,000 | 9 | 59.9 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx71089a-il | 1,000,000 | 5 | 68 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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