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NACA-0009 9.0% smoothed (n0009sm-il)

NACA-0009 9.0% smoothed - NACA 0009 airfoil (smoothed)


Airfoil n0009sm-il
Details Dat file Parser  
(n0009sm-il) NACA-0009 9.0% smoothed
NACA 0009 airfoil (smoothed)
Max thickness 9% at 30.9% chord.
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
  NACA-0009 9.0% smoothed
  1.00000  0.0
  0.99572  0.00057
  0.98296  0.00218
  0.96194  0.00463
  0.93301  0.00770
  0.89668  0.01127
  0.85355  0.01522
  0.80438  0.01945
  0.75000  0.02384
  0.69134  0.02823
  0.62941  0.03247
  0.56526  0.03638
  0.50000  0.03978
  0.43474  0.04248
  0.37059  0.04431
  0.33928  0.04484
  0.30866  0.04509
  0.27886  0.04504
  0.25000  0.04466
  0.22221  0.04397
  0.19562  0.04295
  0.17033  0.04161
  0.14645  0.03994
  0.12408  0.03795
  0.10332  0.03564
  0.08427  0.03305
  0.06699  0.03023
  0.05156  0.02720
  0.03806  0.02395
  0.02653  0.02039
  0.01704  0.01646
  0.00961  0.01214
  0.00428  0.00767
  0.00107  0.00349
  0.0      0.0
  0.00107 -0.00349
  0.00428 -0.00767
  0.00961 -0.01214
  0.01704 -0.01646
  0.02653 -0.02039
  0.03806 -0.02395
  0.05156 -0.02720
  0.06699 -0.03023
  0.08427 -0.03305
  0.10332 -0.03564
  0.12408 -0.03795
  0.14645 -0.03994
  0.17033 -0.04161
  0.19562 -0.04295
  0.22221 -0.04397
  0.25000 -0.04466
  0.27886 -0.04504
  0.30866 -0.04509
  0.33928 -0.04484
  0.37059 -0.04431
  0.43474 -0.04248
  0.50000 -0.03978
  0.56526 -0.03638
  0.62941 -0.03247
  0.69134 -0.02823
  0.75000 -0.02384
  0.80438 -0.01945
  0.85355 -0.01522
  0.89668 -0.01127
  0.93301 -0.00770
  0.96194 -0.00463
  0.98296 -0.00218
  0.99572 -0.00057
  1.00000  0.0
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Polars for NACA-0009 9.0% smoothed (n0009sm-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   n0009sm-il50,000927 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   n0009sm-il50,000525.6 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   n0009sm-il100,000937.3 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   n0009sm-il100,000533.4 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   n0009sm-il200,000945.6 at α=3.25°Mach=0 Ncrit=9Xfoil predictionDetails
   n0009sm-il200,000542.2 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   n0009sm-il500,000955.9 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   n0009sm-il500,000560.2 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   n0009sm-il1,000,000974.7 at α=8°Mach=0 Ncrit=9Xfoil predictionDetails
   n0009sm-il1,000,000575.6 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
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