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FX 72-LS-160 (fx72ls160-il)

FX 72-LS-160 - Wortmann FX 72-LS-160 airfoil


Airfoil fx72ls160-il
Details Dat file Parser  
(fx72ls160-il) FX 72-LS-160
Wortmann FX 72-LS-160 airfoil
Max thickness 16% at 37.1% chord.
Max camber 8.2% at 43.5% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
FX 72-LS-160
1.00000     0.00000
0.99893     0.00037
0.99572     0.00147
0.99039     0.00330
0.98296     0.00584
0.97347     0.00910
0.96194     0.01305
0.94844     0.01769
0.93301     0.02297
0.91573     0.02887
0.89668     0.03540
0.87592     0.04252
0.85355     0.05022
0.82967     0.05841
0.80438     0.06707
0.77779     0.07620
0.75000     0.08579
0.72114     0.09579
0.69134     0.10605
0.66072     0.11639
0.62941     0.12656
0.59755     0.13615
0.56526     0.14458
0.53270     0.15139
0.50000     0.15643
0.46730     0.15982
0.43474     0.16164
0.40245     0.16188
0.37059     0.16058
0.33928     0.15792
0.30866     0.15415
0.27886     0.14937
0.25000     0.14365
0.22221     0.13710
0.19562     0.12980
0.17033     0.12184
0.14645     0.11333
0.12408     0.10432
0.10332     0.09493
0.08427     0.08525
0.06699     0.07544
0.05156     0.06553
0.03806     0.05557
0.02653     0.04580
0.01704     0.03634
0.00961     0.02746
0.00428     0.01815
0.00107     0.00834
0.00000     0.00000
0.00107     -0.00583
0.00428     -0.00890
0.00961     -0.01096
0.01704     -0.01313
0.02653     -0.01470
0.03806     -0.01563
0.05156     -0.01591
0.06699     -0.01568
0.08427     -0.01512
0.10332     -0.01424
0.12408     -0.01318
0.14645     -0.01196
0.17033     -0.01054
0.19562     -0.00904
0.22221     -0.00746
0.25000     -0.00582
0.27886     -0.00420
0.30866     -0.00259
0.33928     -0.00103
0.37059     0.00046
0.40245     0.00188
0.43474     0.00321
0.46730     0.00443
0.50000     0.00553
0.53270     0.00649
0.56526     0.00731
0.59755     0.00799
0.62941     0.00856
0.66072     0.00898
0.69134     0.00929
0.72114     0.00948
0.75000     0.00959
0.77779     0.00970
0.80438     0.00987
0.82967     0.01007
0.85355     0.01023
0.87592     0.01029
0.89668     0.01017
0.91573     0.00982
0.93301     0.00916
0.94844     0.00817
0.96194     0.00690
0.97347     0.00542
0.98296     0.00390
0.99039     0.00250
0.99572     0.00135
0.99893     0.00044
1.00000     0.00000
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Selig format dat file

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Polars for FX 72-LS-160 (fx72ls160-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   fx72ls160-il50,00095.2 at α=10.75°Mach=0 Ncrit=9Xfoil predictionDetails
   fx72ls160-il50,00058.4 at α=16°Mach=0 Ncrit=5Xfoil predictionDetails
   fx72ls160-il100,000914.5 at α=17.25°Mach=0 Ncrit=9Xfoil predictionDetails
   fx72ls160-il100,000513.3 at α=15°Mach=0 Ncrit=5Xfoil predictionDetails
   fx72ls160-il200,000922.3 at α=15°Mach=0 Ncrit=9Xfoil predictionDetails
   fx72ls160-il200,000558.5 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   fx72ls160-il500,0009121.2 at α=9°Mach=0 Ncrit=9Xfoil predictionDetails
   fx72ls160-il500,0005125.7 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   fx72ls160-il1,000,0009175.1 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   fx72ls160-il1,000,0005174.3 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
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