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FX 84-W-097 (fx84w097-il)

FX 84-W-097 - Wortmann FX 84-W-097 airfoil for use on wind turbines (W)


Airfoil fx84w097-il
Details Dat file Parser  
(fx84w097-il) FX 84-W-097
Wortmann FX 84-W-097 airfoil for use on wind turbines (W)
Max thickness 9.7% at 33.9% chord.
Max camber 2.8% at 37.1% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
FX 84-W-097
1.00000     0.00000
0.99893     0.00006
0.99572     0.00028
0.99039     0.00069
0.98296     0.00135
0.97347     0.00230
0.96194     0.00359
0.94844     0.00524
0.93301     0.00726
0.91573     0.00968
0.89668     0.01250
0.87592     0.01571
0.85355     0.01929
0.82967     0.02320
0.80438     0.02739
0.77779     0.03182
0.75000     0.03643
0.72114     0.04113
0.69134     0.04584
0.66072     0.05050
0.62941     0.05499
0.59755     0.05926
0.56526     0.06322
0.53270     0.06677
0.50000     0.06988
0.46730     0.07247
0.43474     0.07445
0.40245     0.07583
0.37059     0.07654
0.33928     0.07659
0.30866     0.07599
0.27886     0.07469
0.25000     0.07276
0.22221     0.07023
0.19562     0.06711
0.17033     0.06353
0.14645     0.05948
0.12408     0.05502
0.10332     0.05020
0.08427     0.04511
0.06699     0.03985
0.05156     0.03449
0.03806     0.02911
0.02653     0.02376
0.01704     0.01854
0.00961     0.01347
0.00428     0.00867
0.00107     0.00419
0.00000     0.00000
0.00107     -0.00387
0.00428     -0.00742
0.00961     -0.01056
0.01704     -0.01329
0.02653     -0.01563
0.03806     -0.01761
0.05156     -0.01923
0.06699     -0.02052
0.08427     -0.02151
0.10332     -0.02221
0.12408     -0.02267
0.14645     -0.02292
0.17033     -0.02298
0.19562     -0.02288
0.22221     -0.02264
0.25000     -0.02230
0.27886     -0.02188
0.30866     -0.02138
0.33928     -0.02081
0.37059     -0.02019
0.40245     -0.01950
0.43474     -0.01876
0.46730     -0.01797
0.50000     -0.01711
0.53270     -0.01620
0.56526     -0.01521
0.59755     -0.01416
0.62941     -0.01305
0.66072     -0.01188
0.69134     -0.01068
0.72114     -0.00944
0.75000     -0.00819
0.77779     -0.00694
0.80438     -0.00574
0.82967     -0.00460
0.85355     -0.00354
0.87592     -0.00258
0.89668     -0.00175
0.91573     -0.00106
0.93301     -0.00052
0.94844     -0.00014
0.96194     0.00011
0.97347     0.00024
0.98296     0.00026
0.99039     0.00021
0.99572     0.00012
0.99893     0.00003
1.00000     0.00000
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Polars for FX 84-W-097 (fx84w097-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   fx84w097-il50,000936.1 at α=8°Mach=0 Ncrit=9Xfoil predictionDetails
   fx84w097-il50,000536.8 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   fx84w097-il100,000956.5 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   fx84w097-il100,000555.6 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   fx84w097-il200,000976.9 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   fx84w097-il200,000573.5 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   fx84w097-il500,0009104.3 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   fx84w097-il500,000596.2 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   fx84w097-il1,000,0009123.6 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   fx84w097-il1,000,0005112.1 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
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