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NACA 63 (naca633418-il)

NACA 63 - NACA 63


Airfoil naca633418-il
Details Dat file Parser  
(naca633418-il) NACA 63
NACA 63
Max thickness 18% at 33.9% chord.
Max camber 2.2% at 50% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
NACA 63,3-418
1.00000     0.00001
0.99893     0.00013
0.99572     0.00077
0.99039     0.00185
0.98296     0.00334
0.97347     0.00526
0.96194     0.00759
0.94844     0.01034
0.93301     0.01352
0.91573     0.01713
0.89668     0.02119
0.87592     0.02573
0.85355     0.03074
0.82967     0.03620
0.80438     0.04206
0.77779     0.04826
0.75000     0.05469
0.72114     0.06127
0.69134     0.06786
0.66072     0.07436
0.62941     0.08064
0.59755     0.08660
0.56526     0.09214
0.53270     0.09715
0.50000     0.10150
0.46730     0.10511
0.43474     0.10786
0.40245     0.10969
0.37059     0.11056
0.33928     0.11039
0.30866     0.10920
0.27886     0.10710
0.25000     0.10419
0.22221     0.10053
0.19562     0.09619
0.17033     0.09123
0.14645     0.08574
0.12408     0.07979
0.10332     0.07344
0.08427     0.06675
0.06699     0.05982
0.05156     0.05272
0.03806     0.04557
0.02653     0.03844
0.01704     0.03134
0.00961     0.02439
0.00428     0.01760
0.00107     0.01121
0.00000     0.00000
0.00107     -0.00329
0.00428     -0.00911
0.00961     -0.01494
0.01704     -0.02058
0.02653     -0.02601
0.03806     -0.03124
0.05156     -0.03627
0.06699     -0.04108
0.08427     -0.04565
0.10332     -0.04994
0.12408     -0.05393
0.14645     -0.05757
0.17033     -0.06083
0.19562     -0.06366
0.22221     -0.06601
0.25000     -0.06784
0.27886     -0.06909
0.30866     -0.06970
0.33928     -0.06959
0.37059     -0.06868
0.40245     -0.06694
0.43474     -0.06442
0.46730     -0.06121
0.50000     -0.05740
0.53270     -0.05308
0.56526     -0.04837
0.59755     -0.04337
0.62941     -0.03819
0.66072     -0.03295
0.69134     -0.02778
0.72114     -0.02281
0.75000     -0.01814
0.77779     -0.01385
0.80438     -0.01002
0.82967     -0.00669
0.85355     -0.00387
0.87592     -0.00156
0.89668     0.00030
0.91573     0.00172
0.93301     0.00260
0.94844     0.00286
0.96194     0.00257
0.97347     0.00199
0.98296     0.00135
0.99039     0.00078
0.99572     0.00036
0.99893     0.00009
1.00000     0.00001
Dat file parser warnings
  • Line 2 - Invalid characters : 3-418
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Polars for NACA 63 (naca633418-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   naca633418-il50,000920.3 at α=12.75°Mach=0 Ncrit=9Xfoil predictionDetails
   naca633418-il50,000516.6 at α=11.75°Mach=0 Ncrit=5Xfoil predictionDetails
   naca633418-il100,000945.4 at α=9.75°Mach=0 Ncrit=9Xfoil predictionDetails
   naca633418-il100,000544.7 at α=8°Mach=0 Ncrit=5Xfoil predictionDetails
   naca633418-il200,000969.3 at α=9.25°Mach=0 Ncrit=9Xfoil predictionDetails
   naca633418-il200,000567.8 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   naca633418-il500,000999.2 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   naca633418-il500,000591.6 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   naca633418-il1,000,0009120.5 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   naca633418-il1,000,0005106.9 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
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