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FX 61-184 AIRFOIL (fx61184-il)

FX 61-184 AIRFOIL - Wortmann FX 61-184 airfoil


Airfoil fx61184-il
Details Dat file Parser  
(fx61184-il) FX 61-184 AIRFOIL
Wortmann FX 61-184 airfoil
Max thickness 18.4% at 37.1% chord.
Max camber 3.1% at 62.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
FX 61-184 AIRFOIL
       49.       49.

 0.0000000 0.0000000
 0.0010200 0.0081200
 0.0042200 0.0152000
 0.0096000 0.0225100
 0.0170200 0.0300600
 0.0265000 0.0379000
 0.0380200 0.0459800
 0.0515800 0.0540700
 0.0669400 0.0620500
 0.0842200 0.0698000
 0.1033000 0.0772400
 0.1240300 0.0842700
 0.1464300 0.0908200
 0.1703700 0.0968100
 0.1955800 0.1022800
 0.2222100 0.1071000
 0.2499800 0.1112700
 0.2789100 0.1146600
 0.3086100 0.1172400
 0.3393300 0.1189300
 0.3705600 0.1197300
 0.4024300 0.1195800
 0.4346900 0.1185000
 0.4673300 0.1164600
 0.4999700 0.1135500
 0.5327400 0.1097400
 0.5652500 0.1051100
 0.5975000 0.0995800
 0.6293800 0.0932300
 0.6607400 0.0861900
 0.6913300 0.0787700
 0.7211500 0.0712500
 0.7499501 0.0639500
 0.7777300 0.0569500
 0.8043500 0.0503500
 0.8297000 0.0441700
 0.8535000 0.0384200
 0.8759000 0.0330900
 0.8964400 0.0281900
 0.9157100 0.0236900
 0.9329900 0.0195700
 0.9484800 0.0158000
 0.9619200 0.0123400
 0.9734400 0.0092000
 0.9829100 0.0064000
 0.9903400 0.0040800
 0.9957100 0.0021800
 0.9989100 0.0007900
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0010200 -.0024300
 0.0042200 -.0067100
 0.0096000 -.0110300
 0.0170200 -.0153800
 0.0265000 -.0197500
 0.0380200 -.0241400
 0.0515800 -.0285100
 0.0669400 -.0328500
 0.0842200 -.0371300
 0.1033000 -.0412900
 0.1240300 -.0452900
 0.1464300 -.0490600
 0.1703700 -.0525100
 0.1955800 -.0556000
 0.2222100 -.0583100
 0.2499800 -.0605500
 0.2789100 -.0623000
 0.3086100 -.0634900
 0.3393300 -.0640700
 0.3705600 -.0640000
 0.4024300 -.0632000
 0.4346900 -.0615600
 0.4673300 -.0589500
 0.4999700 -.0552400
 0.5327400 -.0504200
 0.5652500 -.0446200
 0.5975000 -.0381700
 0.6293800 -.0314800
 0.6607400 -.0249500
 0.6913300 -.0188800
 0.7211500 -.0134000
 0.7499501 -.0085300
 0.7777300 -.0043100
 0.8043500 -.0007500
 0.8297000 0.0021500
 0.8535000 0.0044000
 0.8759000 0.0060100
 0.8964400 0.0070200
 0.9157100 0.0074700
 0.9329900 0.0074200
 0.9484800 0.0069600
 0.9619200 0.0061000
 0.9734400 0.0049400
 0.9829100 0.0036100
 0.9903400 0.0024400
 0.9957100 0.0012900
 0.9989100 0.0003100
 1.0000000 0.0000000
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Lednicer format dat file
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Polars for FX 61-184 AIRFOIL (fx61184-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   fx61184-il50,00095.7 at α=11.25°Mach=0 Ncrit=9Xfoil predictionDetails
   fx61184-il50,000515.2 at α=12°Mach=0 Ncrit=5Xfoil predictionDetails
   fx61184-il100,000939.8 at α=11.25°Mach=0 Ncrit=9Xfoil predictionDetails
   fx61184-il100,000543.4 at α=8.25°Mach=0 Ncrit=5Xfoil predictionDetails
   fx61184-il200,000969.5 at α=8.5°Mach=0 Ncrit=9Xfoil predictionDetails
   fx61184-il200,000571.1 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   fx61184-il500,0009104.9 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   fx61184-il500,0005100.7 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   fx61184-il1,000,0009131.1 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   fx61184-il1,000,0005120.7 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
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