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WORTMANN FX 77-080 (fx77080-il)

WORTMANN FX 77-080 - Wortmann FX 77-080 symmetrical airfoil


Airfoil fx77080-il
Details Dat file Parser  
(fx77080-il) WORTMANN FX 77-080
Wortmann FX 77-080 symmetrical airfoil
Max thickness 8% at 27.9% chord.
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
WORTMANN FX 77-080
1.00000     0.00000
0.99893     0.00079
0.99572     0.00099
0.99039     0.00150
0.98296     0.00211
0.97347     0.00293
0.96194     0.00390
0.94844     0.00502
0.93301     0.00631
0.91573     0.00777
0.89668     0.00937
0.87592     0.01111
0.85355     0.01294
0.82967     0.01485
0.80438     0.01680
0.77779     0.01877
0.75000     0.02074
0.72114     0.02270
0.69134     0.02463
0.66072     0.02651
0.62941     0.02832
0.59755     0.03007
0.56526     0.03175
0.53270     0.03333
0.50000     0.03477
0.46730     0.03605
0.43474     0.03718
0.40245     0.03817
0.37059     0.03900
0.33928     0.03963
0.30866     0.04004
0.27886     0.04024
0.25000     0.04021
0.22221     0.03994
0.19562     0.03941
0.17033     0.03861
0.14645     0.03756
0.12408     0.03625
0.10332     0.03461
0.08427     0.03254
0.06699     0.02998
0.05156     0.02697
0.03806     0.02362
0.02653     0.02002
0.01704     0.01627
0.00961     0.01234
0.00428     0.00828
0.00107     0.00415
0.00000     0.00000
0.00107     -0.00415
0.00428     -0.00828
0.00961     -0.01234
0.01704     -0.01627
0.02653     -0.02002
0.03806     -0.02362
0.05156     -0.02697
0.06699     -0.02998
0.08427     -0.03254
0.10332     -0.03461
0.12408     -0.03625
0.14645     -0.03756
0.17033     -0.03861
0.19562     -0.03941
0.22221     -0.03994
0.25000     -0.04021
0.27886     -0.04024
0.30866     -0.04004
0.33928     -0.03963
0.37059     -0.03900
0.40245     -0.03817
0.43474     -0.03718
0.46730     -0.03605
0.50000     -0.03477
0.53270     -0.03333
0.56526     -0.03175
0.59755     -0.03007
0.62941     -0.02832
0.66072     -0.02651
0.69134     -0.02463
0.72114     -0.02270
0.75000     -0.02074
0.77779     -0.01877
0.80438     -0.01680
0.82967     -0.01485
0.85355     -0.01294
0.87592     -0.01111
0.89668     -0.00937
0.91573     -0.00777
0.93301     -0.00631
0.94844     -0.00502
0.96194     -0.00390
0.97347     -0.00293
0.98296     -0.00211
0.99039     -0.00150
0.99572     -0.00099
0.99893     -0.00079
1.00000     0.00000
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Polars for WORTMANN FX 77-080 (fx77080-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   fx77080-il50,000924.7 at α=3.25°Mach=0 Ncrit=9Xfoil predictionDetails
   fx77080-il50,000523.9 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   fx77080-il100,000933.7 at α=2.75°Mach=0 Ncrit=9Xfoil predictionDetails
   fx77080-il100,000533.2 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   fx77080-il200,000942 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   fx77080-il200,000543.2 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   fx77080-il500,000958.4 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   fx77080-il500,000558.6 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   fx77080-il1,000,000971.2 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   fx77080-il1,000,000572.7 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
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