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FX 79-L-100 (fx79l100-il)

FX 79-L-100 - Wortmann FX 79-L-100 symmetrical airfoil


Airfoil fx79l100-il
Details Dat file Parser  
(fx79l100-il) FX 79-L-100
Wortmann FX 79-L-100 symmetrical airfoil
Max thickness 10.1% at 33.9% chord.
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
FX 79-L-100
1.00000     0.00000
0.99893     0.00090
0.99572     0.00114
0.99039     0.00156
0.98296     0.00202
0.97347     0.00266
0.96194     0.00343
0.94844     0.00435
0.93301     0.00541
0.91573     0.00662
0.89668     0.00800
0.87592     0.00958
0.85355     0.01136
0.82967     0.01334
0.80438     0.01553
0.77779     0.01790
0.75000     0.02046
0.72114     0.02318
0.69134     0.02605
0.66072     0.02903
0.62941     0.03208
0.59755     0.03515
0.56526     0.03816
0.53270     0.04102
0.50000     0.04362
0.46730     0.04588
0.43474     0.04771
0.40245     0.04907
0.37059     0.04995
0.33928     0.05033
0.30866     0.05023
0.27886     0.04970
0.25000     0.04880
0.22221     0.04754
0.19562     0.04596
0.17033     0.04408
0.14645     0.04193
0.12408     0.03953
0.10332     0.03690
0.08427     0.03406
0.06699     0.03101
0.05156     0.02779
0.03806     0.02438
0.02653     0.02076
0.01704     0.01691
0.00961     0.01284
0.00428     0.00860
0.00107     0.00431
0.00000     0.00000
0.00107     -0.00431
0.00428     -0.00860
0.00961     -0.01284
0.01704     -0.01691
0.02653     -0.02076
0.03806     -0.02438
0.05156     -0.02779
0.06699     -0.03101
0.08427     -0.03406
0.10332     -0.03690
0.12408     -0.03953
0.14645     -0.04193
0.17033     -0.04408
0.19562     -0.04596
0.22221     -0.04754
0.25000     -0.04880
0.27886     -0.04970
0.30866     -0.05023
0.33928     -0.05033
0.37059     -0.04995
0.40245     -0.04907
0.43474     -0.04771
0.46730     -0.04588
0.50000     -0.04362
0.53270     -0.04102
0.56526     -0.03816
0.59755     -0.03515
0.62941     -0.03208
0.66072     -0.02903
0.69134     -0.02605
0.72114     -0.02318
0.75000     -0.02046
0.77779     -0.01790
0.80438     -0.01553
0.82967     -0.01334
0.85355     -0.01136
0.87592     -0.00958
0.89668     -0.00800
0.91573     -0.00662
0.93301     -0.00541
0.94844     -0.00435
0.96194     -0.00343
0.97347     -0.00266
0.98296     -0.00202
0.99039     -0.00156
0.99572     -0.00114
0.99893     -0.00090
1.00000     0.00000
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Selig format dat file

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Polars for FX 79-L-100 (fx79l100-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   fx79l100-il50,000927.7 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   fx79l100-il50,000527 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   fx79l100-il100,000938.6 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   fx79l100-il100,000535.9 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   fx79l100-il200,000950.1 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   fx79l100-il200,000541.5 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   fx79l100-il500,000958 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   fx79l100-il500,000558.1 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   fx79l100-il1,000,000970.6 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   fx79l100-il1,000,000572.7 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
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