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UA(2)-180 (University of Alberta/Marsden) (ua2-180-il)

UA(2)-180 (University of Alberta/Marsden) - UA(2)-180 airfoil for ultralight category aircraft


Airfoil ua2-180-il
Details Dat file Parser  
(ua2-180-il) UA(2)-180 (University of Alberta/Marsden)
UA(2)-180 airfoil for ultralight category aircraft
Max thickness 18.1% at 31.5% chord.
Max camber 7% at 36.6% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
UA(2)-180 (University of Alberta/Marsden)
1.0      0.0
0.99707  0.00083
0.98831  0.00299
0.97383  0.007
0.95379  0.01287
0.92843  0.01957
0.89805  0.02862
0.863    0.03857
0.82369  0.04995
0.78059  0.06232
0.7342   0.07579
0.68507  0.09062
0.63376  0.10395
0.58089  0.11821
0.52707  0.1316
0.47293  0.14577
0.41911  0.15593
0.36624  0.16039
0.31493  0.15929
0.2658   0.1554
0.21941  0.14735
0.17631  0.13731
0.137    0.12339
0.10195  0.1074
0.07157  0.08844
0.04621  0.06944
0.02617  0.04917
0.01169  0.03087
0.00293  0.01267
0.0      0.0
0.00293 -0.00976
0.02617 -0.01636
0.04621 -0.01871
0.07157 -0.02075
0.10195 -0.02201
0.137   -0.0231
0.17631 -0.0232
0.21941 -0.02329
0.2658  -0.02256
0.31493 -0.02196
0.36624 -0.02065
0.41911 -0.01958
0.47293 -0.01793
0.52707 -0.0166
0.58089 -0.01474
0.63376 -0.01334
0.68507 -0.01149
0.7342  -0.01013
0.78059 -0.00835
0.82369 -0.00708
0.863   -0.00544
0.89805 -0.00437
0.92843 -0.00303
0.95379 -0.00224
0.97383 -0.00112
0.98831 -0.00062
0.99707  0.0
1.0      0.0
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Polars for UA(2)-180 (University of Alberta/Marsden) (ua2-180-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   ua2-180-il50,00093.9 at α=11.75°Mach=0 Ncrit=9Xfoil predictionDetails
   ua2-180-il50,00056.6 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
   ua2-180-il100,00095 at α=8.25°Mach=0 Ncrit=9Xfoil predictionDetails
   ua2-180-il100,000523.8 at α=2.75°Mach=0 Ncrit=5Xfoil predictionDetails
   ua2-180-il200,000930.2 at α=2.25°Mach=0 Ncrit=9Xfoil predictionDetails
   ua2-180-il200,000555.8 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   ua2-180-il500,0009103.9 at α=9.5°Mach=0 Ncrit=9Xfoil predictionDetails
   ua2-180-il500,0005107 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   ua2-180-il1,000,0009146.2 at α=8.25°Mach=0 Ncrit=9Xfoil predictionDetails
   ua2-180-il1,000,0005139.6 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
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