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WORTMANN FX 60-126 AIRFOIL (fx60126-il)

WORTMANN FX 60-126 AIRFOIL - Wortmann FX 60-126 airfoil


Airfoil fx60126-il
Details Dat file Parser  
(fx60126-il) WORTMANN FX 60-126 AIRFOIL
Wortmann FX 60-126 airfoil
Max thickness 12.6% at 27.9% chord.
Max camber 3.6% at 56.5% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
WORTMANN FX 60-126 AIRFOIL
      49.0      49.0

 0.0000000 0.0000000
 0.0010700 0.0067500
 0.0042800 0.0134900
 0.0096100 0.0209600
 0.0170400 0.0280200
 0.0265300 0.0349300
 0.0380600 0.0417400
 0.0515600 0.0480800
 0.0669900 0.0545700
 0.0842700 0.0602100
 0.1033200 0.0658500
 0.1240800 0.0707700
 0.1464500 0.0755500
 0.1703300 0.0795800
 0.1956200 0.0832700
 0.2222100 0.0861500
 0.2500000 0.0885900
 0.2788600 0.0901900
 0.3086600 0.0913000
 0.3392800 0.0916000
 0.3705900 0.0913800
 0.4024500 0.0904100
 0.4347400 0.0889300
 0.4673000 0.0867900
 0.5000000 0.0842500
 0.5327000 0.0811800
 0.5652600 0.0778100
 0.5975500 0.0740200
 0.6294100 0.0699400
 0.6607200 0.0654900
 0.6913400 0.0608200
 0.7211400 0.0558900
 0.7500000 0.0508400
 0.7777900 0.0456700
 0.8043800 0.0405500
 0.8296700 0.0355200
 0.8535500 0.0307000
 0.8759200 0.0261100
 0.8966800 0.0218100
 0.9157300 0.0177700
 0.9330100 0.0141200
 0.9484400 0.0108400
 0.9619400 0.0079800
 0.9734700 0.0055400
 0.9829600 0.0035300
 0.9903900 0.0019800
 0.9957200 0.0008800
 0.9989300 0.0002400
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0010700 -.0030100
 0.0042800 -.0064100
 0.0096100 -.0101200
 0.0170400 -.0140400
 0.0265300 -.0179200
 0.0380600 -.0213200
 0.0515600 -.0248200
 0.0669900 -.0276100
 0.0842700 -.0304500
 0.1033200 -.0326200
 0.1240800 -.0346500
 0.1464500 -.0359800
 0.1703300 -.0370700
 0.1956200 -.0374600
 0.2222100 -.0375100
 0.2500000 -.0368300
 0.2788600 -.0357400
 0.3086600 -.0339200
 0.3392800 -.0316700
 0.3705900 -.0287700
 0.4024500 -.0255300
 0.4347400 -.0218800
 0.4673000 -.0181400
 0.5000000 -.0142100
 0.5327000 -.0103600
 0.5652600 -.0065300
 0.5975500 -.0029800
 0.6294100 0.0002900
 0.6607200 0.0030700
 0.6913400 0.0054700
 0.7211400 0.0074100
 0.7500000 0.0089700
 0.7777900 0.0100600
 0.8043800 0.0107300
 0.8296700 0.0109300
 0.8535500 0.0107400
 0.8759200 0.0102200
 0.8966800 0.0094400
 0.9157300 0.0084500
 0.9330100 0.0073200
 0.9484400 0.0061000
 0.9619400 0.0048300
 0.9734700 0.0035700
 0.9829600 0.0023900
 0.9903900 0.0014600
 0.9957200 0.0006800
 0.9989300 0.0001400
 1.0000000 0.0000000
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Lednicer format dat file
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Polars for WORTMANN FX 60-126 AIRFOIL (fx60126-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   fx60126-il50,000934.4 at α=8.5°Mach=0 Ncrit=9Xfoil predictionDetails
   fx60126-il50,000539.1 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   fx60126-il100,000957.6 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   fx60126-il100,000558.5 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   fx60126-il200,000979.7 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   fx60126-il200,000575.2 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   fx60126-il500,0009104 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   fx60126-il500,000588.4 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   fx60126-il1,000,0009112.3 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   fx60126-il1,000,000595.5 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
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