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WORTMANN FX 60-126/1 AIRFOIL (fx601261-il)

WORTMANN FX 60-126/1 AIRFOIL - Wortmann FX 60-126/1 airfoil


Airfoil fx601261-il
Details Dat file Parser  
(fx601261-il) WORTMANN FX 60-126/1 AIRFOIL
Wortmann FX 60-126/1 airfoil
Max thickness 12.6% at 27.9% chord.
Max camber 4% at 56.5% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
WORTMANN FX 60-126/1 AIRFOIL
       49.       49.

 0.0000000 0.0000000
 0.0010200 0.0035900
 0.0042200 0.0127900
 0.0096000 0.0208600
 0.0170200 0.0285600
 0.0265000 0.0354500
 0.0380200 0.0430700
 0.0515800 0.0496200
 0.0669400 0.0563600
 0.0842200 0.0622400
 0.1033000 0.0681500
 0.1240300 0.0733100
 0.1464300 0.0783500
 0.1703700 0.0826000
 0.1955800 0.0865300
 0.2222100 0.0896200
 0.2499800 0.0922700
 0.2789100 0.0940500
 0.3086100 0.0953300
 0.3393300 0.0957700
 0.3705600 0.0956700
 0.4024300 0.0947800
 0.4346900 0.0933700
 0.4673300 0.0912200
 0.4999700 0.0886200
 0.5327400 0.0854200
 0.5652500 0.0818300
 0.5975000 0.0777400
 0.6293800 0.0733400
 0.6607400 0.0685400
 0.6913300 0.0635400
 0.7211500 0.0582900
 0.7499501 0.0529500
 0.7777300 0.0475900
 0.8043500 0.0423700
 0.8297000 0.0373900
 0.8535000 0.0327000
 0.8759000 0.0283000
 0.8964400 0.0242700
 0.9157100 0.0205400
 0.9329900 0.0170700
 0.9484800 0.0138100
 0.9619200 0.0107200
 0.9734400 0.0078400
 0.9829100 0.0052800
 0.9903400 0.0032300
 0.9957100 0.0016100
 0.9989100 0.0005200
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0010200 -.0047200
 0.0042200 -.0067500
 0.0096000 -.0098300
 0.0170200 -.0130800
 0.0265000 -.0171000
 0.0380200 -.0201700
 0.0515800 -.0234200
 0.0669400 -.0259400
 0.0842200 -.0285200
 0.1033000 -.0304200
 0.1240300 -.0322000
 0.1464300 -.0332700
 0.1703700 -.0341200
 0.1955800 -.0342600
 0.2222100 -.0340900
 0.2499800 -.0331900
 0.2789100 -.0319100
 0.3086100 -.0299200
 0.3393300 -.0275200
 0.3705600 -.0244900
 0.4024300 -.0211700
 0.4346900 -.0174600
 0.4673300 -.0137100
 0.4999700 -.0098500
 0.5327400 -.0061400
 0.5652500 -.0025300
 0.5975000 0.0007200
 0.6293800 0.0036500
 0.6607400 0.0060900
 0.6913300 0.0081500
 0.7211500 0.0097800
 0.7499501 0.0110600
 0.7777300 0.0119000
 0.8043500 0.0123600
 0.8297000 0.0123900
 0.8535000 0.0120800
 0.8759000 0.0114600
 0.8964400 0.0106000
 0.9157100 0.0095500
 0.9329900 0.0083600
 0.9484800 0.0070600
 0.9619200 0.0056800
 0.9734400 0.0042700
 0.9829100 0.0029200
 0.9903400 0.0018200
 0.9957100 0.0008900
 0.9989100 0.0002100
 1.0000000 0.0000000
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Lednicer format dat file
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Polars for WORTMANN FX 60-126/1 AIRFOIL (fx601261-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   fx601261-il50,000934.5 at α=8.75°Mach=0 Ncrit=9Xfoil predictionDetails
   fx601261-il50,000539.4 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   fx601261-il100,000959.4 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   fx601261-il100,000560.5 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   fx601261-il200,000982.9 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   fx601261-il200,000576.2 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   fx601261-il500,0009108.2 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   fx601261-il500,000584.2 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   fx601261-il1,000,0009113.3 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   fx601261-il1,000,000588.2 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
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