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I.S.A. 960 (isa960-il)

I.S.A. 960 - I.S.A. 960 airfoil


Airfoil isa960-il
Details Dat file Parser  
(isa960-il) I.S.A. 960
I.S.A. 960 airfoil
Max thickness 9.5% at 30% chord.
Max camber 4.5% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
I.S.A. 960
1.0000     0.0042
0.9500     0.0170
0.9000     0.0275
0.8000     0.0495
0.7000     0.0677
0.6000     0.0842
0.5000     0.0957
0.4000     0.1030
0.3000     0.1043
0.2000     0.0990
0.1500     0.0935
0.1000     0.0792
0.0750     0.0750
0.0500     0.0637
0.0250     0.0490
0.0125     0.0383
0.0000     0.0180
0.0125     0.0085
0.0250     0.0050
0.0500     0.0005
0.0750     0.0000
0.1000     0.0000
0.1500     0.0030
0.2000     0.0055
0.3000     0.0097
0.4000     0.0112
0.5000     0.0115
0.6000     0.0095
0.7000     0.0075
0.8000     0.0050
0.9000     0.0025
0.9500     0.0010
1.0000     0.0000
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Selig format dat file

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Polars for I.S.A. 960 (isa960-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   isa960-il50,000939.3 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   isa960-il50,000538 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   isa960-il100,000955.9 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   isa960-il100,000549.8 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   isa960-il200,000964.7 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   isa960-il200,000553.7 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   isa960-il500,000968.2 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   isa960-il500,000572.1 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   isa960-il1,000,000990.5 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   isa960-il1,000,000591.6 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
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