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AIRFOIL 3024 9.84% (s3024-il)

AIRFOIL 3024 9.84% - Selig S3024 low Reynolds number airfoil


Airfoil s3024-il
Details Dat file Parser  
(s3024-il) AIRFOIL 3024 9.84%
Selig S3024 low Reynolds number airfoil
Max thickness 9.8% at 30.7% chord.
Max camber 3% at 44.7% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
 AIRFOIL 3024    9.84%
  1.00000  0.0
  0.99662  0.00036
  0.98664  0.00162
  0.97044  0.00407
  0.94859  0.00787
  0.92168  0.01299
  0.89037  0.01929
  0.85527  0.02649
  0.81693  0.03428
  0.77588  0.04230
  0.73258  0.05022
  0.68743  0.05770
  0.64084  0.06450
  0.59316  0.07038
  0.54473  0.07523
  0.49598  0.07903
  0.44741  0.08173
  0.39947  0.08324
  0.35259  0.08353
  0.30720  0.08260
  0.26372  0.08047
  0.22258  0.07719
  0.18416  0.07278
  0.14880  0.06727
  0.11676  0.06075
  0.08828  0.05334
  0.06357  0.04520
  0.04278  0.03651
  0.02601  0.02751
  0.01334  0.01848
  0.00476  0.00982
  0.00032  0.00221
  0.00111 -0.00352
  0.00783 -0.00794
  0.02011 -0.01179
  0.03773 -0.01487
  0.06053 -0.01715
  0.08834 -0.01862
  0.12093 -0.01933
  0.15799 -0.01936
  0.19918 -0.01879
  0.24406 -0.01774
  0.29214 -0.01636
  0.34284 -0.01475
  0.39555 -0.01303
  0.44962 -0.01127
  0.50439 -0.00955
  0.55919 -0.00790
  0.61333 -0.00639
  0.66617 -0.00503
  0.71704 -0.00385
  0.76531 -0.00285
  0.81040 -0.00201
  0.85176 -0.00134
  0.88886 -0.00083
  0.92122 -0.00041
  0.94852 -0.00003
  0.97047  0.00023
  0.98666  0.00026
  0.99663  0.00011
  1.00001  0.00000
Dat file parser warnings
  • Line 62 - X value too large but included: 1.00001 0.00000
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Polars for AIRFOIL 3024 9.84% (s3024-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   s3024-il50,000934.4 at α=8.25°Mach=0 Ncrit=9Xfoil predictionDetails
   s3024-il50,000538.3 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   s3024-il100,000957.8 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   s3024-il100,000557.7 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   s3024-il200,000980.9 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   s3024-il200,000576.1 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   s3024-il500,0009110.1 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   s3024-il500,000596.8 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   s3024-il1,000,0009129 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   s3024-il1,000,0005110.1 at α=3.5°Mach=0 Ncrit=5Xfoil predictionDetails
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