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FX S 03-182 AIRFOIL (fxs03182-il)

FX S 03-182 AIRFOIL - Wortmann FX S 03-182 airfoil


Airfoil fxs03182-il
Details Dat file Parser  
(fxs03182-il) FX S 03-182 AIRFOIL
Wortmann FX S 03-182 airfoil
Max thickness 18.2% at 40.2% chord.
Max camber 2.9% at 56.5% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
FX S 03-182 AIRFOIL
       49.       49.

 0.0000000 0.0000000
 0.0010200 0.0050000
 0.0042200 0.0130000
 0.0096000 0.0190900
 0.0170200 0.0263100
 0.0265000 0.0331000
 0.0380200 0.0405400
 0.0515800 0.0475900
 0.0669400 0.0549500
 0.0842200 0.0619000
 0.1033000 0.0689700
 0.1240300 0.0755600
 0.1464300 0.0821000
 0.1703700 0.0881300
 0.1955800 0.0939000
 0.2222100 0.0991000
 0.2499800 0.1039400
 0.2789100 0.1080600
 0.3086100 0.1116900
 0.3393300 0.1145500
 0.3705600 0.1167300
 0.4024300 0.1180300
 0.4346900 0.1185200
 0.4673300 0.1179200
 0.4999700 0.1160800
 0.5327400 0.1127800
 0.5652500 0.1081900
 0.5975000 0.1025800
 0.6293800 0.0963900
 0.6607400 0.0896200
 0.6913300 0.0826300
 0.7211500 0.0754400
 0.7499501 0.0682000
 0.7777300 0.0610200
 0.8043500 0.0540300
 0.8297000 0.0472500
 0.8535000 0.0408600
 0.8759000 0.0347900
 0.8964400 0.0292000
 0.9157100 0.0240300
 0.9329900 0.0193700
 0.9484800 0.0151300
 0.9619200 0.0113900
 0.9734400 0.0081200
 0.9829100 0.0053300
 0.9903400 0.0031000
 0.9957100 0.0014400
 0.9989100 0.0003900
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0010200 -.0020000
 0.0042200 -.0055000
 0.0096000 -.0107600
 0.0170200 -.0148300
 0.0265000 -.0193300
 0.0380200 -.0234100
 0.0515800 -.0278100
 0.0669400 -.0317600
 0.0842200 -.0359100
 0.1033000 -.0396800
 0.1240300 -.0435100
 0.1464300 -.0469600
 0.1703700 -.0503700
 0.1955800 -.0533700
 0.2222100 -.0562300
 0.2499800 -.0586000
 0.2789100 -.0607400
 0.3086100 -.0622900
 0.3393300 -.0634700
 0.3705600 -.0640100
 0.4024300 -.0640900
 0.4346900 -.0634400
 0.4673300 -.0620800
 0.4999700 -.0596200
 0.5327400 -.0559500
 0.5652500 -.0511200
 0.5975000 -.0457000
 0.6293800 -.0399100
 0.6607400 -.0340900
 0.6913300 -.0283300
 0.7211500 -.0228400
 0.7499501 -.0176800
 0.7777300 -.0129800
 0.8043500 -.0087500
 0.8297000 -.0051200
 0.8535000 -.0020900
 0.8759000 0.0003200
 0.8964400 0.0021700
 0.9157100 0.0034100
 0.9329900 0.0041400
 0.9484800 0.0043700
 0.9619200 0.0041600
 0.9734400 0.0035800
 0.9829100 0.0027500
 0.9903400 0.0018200
 0.9957100 0.0009300
 0.9989100 0.0002700
 1.0000000 0.0000000
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Lednicer format dat file
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Polars for FX S 03-182 AIRFOIL (fxs03182-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   fxs03182-il50,000919.6 at α=12.25°Mach=0 Ncrit=9Xfoil predictionDetails
   fxs03182-il50,000516.2 at α=12°Mach=0 Ncrit=5Xfoil predictionDetails
   fxs03182-il100,000927.4 at α=11°Mach=0 Ncrit=9Xfoil predictionDetails
   fxs03182-il100,000528.1 at α=9.75°Mach=0 Ncrit=5Xfoil predictionDetails
   fxs03182-il200,000964.5 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   fxs03182-il200,000566.7 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   fxs03182-il500,000996.8 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   fxs03182-il500,000589.5 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   fxs03182-il1,000,0009110.8 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   fxs03182-il1,000,000596.3 at α=2.25°Mach=0 Ncrit=5Xfoil predictionDetails
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