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FX 71-L-150/20 AIRFOIL (fx711520-il)

FX 71-L-150/20 AIRFOIL - Wortmann FX 71-L-150/20 airfoil


Airfoil fx711520-il
Details Dat file Parser  
(fx711520-il) FX 71-L-150/20 AIRFOIL
Wortmann FX 71-L-150/20 airfoil
Max thickness 15% 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
FX 71-L-150/20 AIRFOIL
       44.       44.

 0.0000000 0.0000000
 0.0010700 0.0082900
 0.0042800 0.0147400
 0.0096100 0.0191700
 0.0170400 0.0246300
 0.0265300 0.0295200
 0.0380600 0.0347100
 0.0515600 0.0395300
 0.0669900 0.0444200
 0.0842700 0.0488700
 0.1033200 0.0533700
 0.1240800 0.0573100
 0.1464500 0.0611400
 0.1703300 0.0644500
 0.1956200 0.0675300
 0.2222100 0.0699700
 0.2500000 0.0721400
 0.2786600 0.0736000
 0.3086600 0.0747000
 0.3392800 0.0750100
 0.3705900 0.0748200
 0.4024500 0.0736900
 0.4347400 0.0720400
 0.4673000 0.0695000
 0.5000000 0.0663000
 0.5327000 0.0622500
 0.5652600 0.0577100
 0.5975500 0.0524400
 0.6294100 0.0469600
 0.6607200 0.0413700
 0.6913400 0.0358200
 0.7211400 0.0303400
 0.7500000 0.0252700
 0.7777900 0.0205000
 0.8043801 0.0164300
 0.8296700 0.0134600
 0.8535500 0.0111600
 0.8759201 0.0093100
 0.9157300 0.0062600
 0.9484400 0.0038400
 0.9734700 0.0021000
 0.9903900 0.0008300
 0.9989300 0.0000900
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0010700 -.0082900
 0.0042800 -.0147400
 0.0096100 -.0191700
 0.0170400 -.0246300
 0.0265300 -.0295200
 0.0380600 -.0347100
 0.0515600 -.0395300
 0.0669900 -.0444200
 0.0842700 -.0488700
 0.1033200 -.0533700
 0.1240800 -.0573100
 0.1464500 -.0611400
 0.1703300 -.0644500
 0.1956200 -.0675300
 0.2222100 -.0699700
 0.2500000 -.0721400
 0.2786600 -.0736000
 0.3086600 -.0747000
 0.3392800 -.0750100
 0.3705900 -.0748200
 0.4024500 -.0736900
 0.4347400 -.0720400
 0.4673000 -.0695000
 0.5000000 -.0663000
 0.5327000 -.0622500
 0.5652600 -.0577100
 0.5975500 -.0524400
 0.6294100 -.0469600
 0.6607200 -.0413700
 0.6913400 -.0358200
 0.7211400 -.0303400
 0.7500000 -.0252700
 0.7777900 -.0205000
 0.8043801 -.0164300
 0.8296700 -.0134600
 0.8535500 -.0111600
 0.8759201 -.0093100
 0.9157300 -.0062600
 0.9484400 -.0038400
 0.9734700 -.0021000
 0.9903900 -.0008300
 0.9989300 -.0000900
 1.0000000 0.0000000
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Polars for FX 71-L-150/20 AIRFOIL (fx711520-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   fx711520-il50,000927.2 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   fx711520-il50,000525.6 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   fx711520-il100,000936.7 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   fx711520-il100,000533.3 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   fx711520-il200,000944.3 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   fx711520-il200,000538.6 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   fx711520-il500,000949.1 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   fx711520-il500,000548 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   fx711520-il1,000,000957.9 at α=8°Mach=0 Ncrit=9Xfoil predictionDetails
   fx711520-il1,000,000556.8 at α=8°Mach=0 Ncrit=5Xfoil predictionDetails
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