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FX S 02-196 AIRFOIL (fxs02196-il)

FX S 02-196 AIRFOIL - Wortmann FX S 02-196 airfoil


Airfoil fxs02196-il
Details Dat file Parser  
(fxs02196-il) FX S 02-196 AIRFOIL
Wortmann FX S 02-196 airfoil
Max thickness 19.6% at 37.1% chord.
Max camber 3.7% at 43.5% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
FX S 02-196 AIRFOIL
       49.       49.

 0.0000000 0.0000000
 0.0010200 0.0085000
 0.0042200 0.0179100
 0.0096000 0.0260000
 0.0170200 0.0336900
 0.0265000 0.0404700
 0.0380200 0.0504400
 0.0515800 0.0578100
 0.0669400 0.0673900
 0.0842200 0.0748300
 0.1033000 0.0838400
 0.1240300 0.0909300
 0.1464300 0.0991400
 0.1703700 0.1055700
 0.1955800 0.1126200
 0.2222100 0.1179400
 0.2499800 0.1234700
 0.2789100 0.1273200
 0.3086100 0.1309900
 0.3393300 0.1330600
 0.3705600 0.1344400
 0.4024300 0.1338500
 0.4346900 0.1317600
 0.4673300 0.1277600
 0.4999700 0.1229400
 0.5327400 0.1169500
 0.5652500 0.1104600
 0.5975000 0.1033400
 0.6293800 0.0960200
 0.6607400 0.0882800
 0.6913300 0.0805800
 0.7211500 0.0727400
 0.7499501 0.0651200
 0.7777300 0.0575400
 0.8043500 0.0503200
 0.8297000 0.0433800
 0.8535000 0.0369500
 0.8759000 0.0309400
 0.8964400 0.0255100
 0.9157100 0.0206000
 0.9329900 0.0162700
 0.9484800 0.0124400
 0.9619200 0.0091800
 0.9734400 0.0064300
 0.9829100 0.0041500
 0.9903400 0.0023500
 0.9957100 0.0010700
 0.9989100 0.0002600
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0010200 -.0035000
 0.0042200 -.0080000
 0.0096000 -.0129300
 0.0170200 -.0160300
 0.0265000 -.0216400
 0.0380200 -.0248400
 0.0515800 -.0299300
 0.0669400 -.0331500
 0.0842200 -.0379000
 0.1033000 -.0410400
 0.1240300 -.0454000
 0.1464300 -.0482600
 0.1703700 -.0520800
 0.1955800 -.0544700
 0.2222100 -.0574700
 0.2499800 -.0590600
 0.2789100 -.0610300
 0.3086100 -.0616200
 0.3393300 -.0622500
 0.3705600 -.0614300
 0.4024300 -.0602600
 0.4346900 -.0569900
 0.4673300 -.0532200
 0.4999700 -.0482600
 0.5327400 -.0433700
 0.5652500 -.0379300
 0.5975000 -.0327800
 0.6293800 -.0274400
 0.6607400 -.0225900
 0.6913300 -.0178300
 0.7211500 -.0136200
 0.7499501 -.0097000
 0.7777300 -.0063300
 0.8043500 -.0033300
 0.8297000 -.0009300
 0.8535000 0.0011100
 0.8759000 0.0025800
 0.8964400 0.0036300
 0.9157100 0.0042500
 0.9329900 0.0045000
 0.9484800 0.0043800
 0.9619200 0.0039500
 0.9734400 0.0032400
 0.9829100 0.0023600
 0.9903400 0.0014700
 0.9957100 0.0007000
 0.9989100 0.0001900
 1.0000000 0.0000000
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Lednicer format dat file
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Polars for FX S 02-196 AIRFOIL (fxs02196-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   fxs02196-il50,00094.7 at α=11.25°Mach=0 Ncrit=9Xfoil predictionDetails
   fxs02196-il50,000510.2 at α=13.75°Mach=0 Ncrit=5Xfoil predictionDetails
   fxs02196-il100,000916.8 at α=13.75°Mach=0 Ncrit=9Xfoil predictionDetails
   fxs02196-il100,000537.5 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   fxs02196-il200,000968.4 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   fxs02196-il200,000556 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   fxs02196-il500,000953.1 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   fxs02196-il500,000546.5 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   fxs02196-il1,000,000960.1 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   fxs02196-il1,000,000554.9 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
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