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UAG 88-143/20 (uag8814320-il)

UAG 88-143/20 - UAG 88-143/20 airfoil


Airfoil uag8814320-il
Details Dat file Parser  
(uag8814320-il) UAG 88-143/20
UAG 88-143/20 airfoil
Max thickness 14.3% at 43.5% chord.
Max camber 6.2% at 46.7% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
UAG 88-143/20
1.00000     0.00002
0.99893     0.00053
0.99572     0.00196
0.99039     0.00403
0.98296     0.00660
0.97347     0.00967
0.96194     0.01327
0.94844     0.01742
0.93301     0.02218
0.91573     0.02756
0.89668     0.03360
0.87592     0.04036
0.85355     0.04794
0.82967     0.05651
0.80438     0.06628
0.77779     0.07682
0.75000     0.08719
0.72114     0.09659
0.69134     0.10480
0.66072     0.11193
0.62941     0.11801
0.59755     0.12305
0.56526     0.12706
0.53270     0.13006
0.50000     0.13208
0.46730     0.13318
0.43474     0.13338
0.40245     0.13272
0.37059     0.13122
0.33928     0.12892
0.30866     0.12584
0.27886     0.12201
0.25000     0.11747
0.22221     0.11226
0.19562     0.10642
0.17033     0.09998
0.14645     0.09301
0.12408     0.08557
0.10332     0.07774
0.08427     0.06961
0.06699     0.06128
0.05156     0.05288
0.03806     0.04454
0.02653     0.03633
0.01704     0.02829
0.00961     0.02053
0.00428     0.01343
0.00107     0.00789
0.00000     0.00000
0.00107     -0.00090
0.00428     -0.00398
0.00961     -0.00690
0.01704     -0.00956
0.02653     -0.01170
0.03806     -0.01312
0.05156     -0.01405
0.06699     -0.01467
0.08427     -0.01503
0.10332     -0.01518
0.12408     -0.01515
0.14645     -0.01494
0.17033     -0.01456
0.19562     -0.01405
0.22221     -0.01349
0.25000     -0.01294
0.27886     -0.01241
0.30866     -0.01188
0.33928     -0.01134
0.37059     -0.01080
0.40245     -0.01024
0.43474     -0.00968
0.46730     -0.00912
0.50000     -0.00855
0.53270     -0.00798
0.56526     -0.00741
0.59755     -0.00684
0.62941     -0.00628
0.66072     -0.00573
0.69134     -0.00519
0.72114     -0.00466
0.75000     -0.00415
0.77779     -0.00366
0.80438     -0.00319
0.82967     -0.00275
0.85355     -0.00233
0.87592     -0.00194
0.89668     -0.00157
0.91573     -0.00124
0.93301     -0.00094
0.94844     -0.00067
0.96194     -0.00044
0.97347     -0.00022
0.98296     -0.00004
0.99039     0.00006
0.99572     0.00009
0.99893     0.00008
1.00000     0.00002
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Polars for UAG 88-143/20 (uag8814320-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   uag8814320-il50,00095.5 at α=10.25°Mach=0 Ncrit=9Xfoil predictionDetails
   uag8814320-il50,000515.3 at α=13.75°Mach=0 Ncrit=5Xfoil predictionDetails
   uag8814320-il100,000932 at α=11.5°Mach=0 Ncrit=9Xfoil predictionDetails
   uag8814320-il100,000530.3 at α=11°Mach=0 Ncrit=5Xfoil predictionDetails
   uag8814320-il200,000955.1 at α=9.5°Mach=0 Ncrit=9Xfoil predictionDetails
   uag8814320-il200,000553.2 at α=8.75°Mach=0 Ncrit=5Xfoil predictionDetails
   uag8814320-il500,0009127 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   uag8814320-il500,0005123.9 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   uag8814320-il1,000,0009185.1 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   uag8814320-il1,000,0005169.3 at α=3.5°Mach=0 Ncrit=5Xfoil predictionDetails
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