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NACA 64(1)-212 MOD A (n64212ma-il)

NACA 64(1)-212 MOD A - NACA-NASA/AMES/Hicks 63(1)-212 MOD A airfoil


Airfoil n64212ma-il
Details Dat file Parser  
(n64212ma-il) NACA 64(1)-212 MOD A
NACA-NASA/AMES/Hicks 63(1)-212 MOD A airfoil
Max thickness 12% at 41.2% chord.
Max camber 2.5% at 21.5% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
  NACA 64(1)-212 MOD A
       30.       28.

 0.0000000 0.0000000
 0.0017515 0.0139677
 0.0048357 0.0209074
 0.0088714 0.0263278
 0.0138847 0.0315286
 0.0188679 0.0352297
 0.0288103 0.0414320
 0.0387467 0.0473345
 0.0486491 0.0515373
 0.0617421 0.0581767
 0.0917591 0.0646775
 0.1164151 0.0696854
 0.1656920 0.0755010
 0.2149875 0.0788158
 0.2642925 0.0811300
 0.3135933 0.0827444
 0.3628836 0.0828386
 0.4121608 0.0822930
 0.4614075 0.0797175
 0.5105944 0.0756329
 0.5597372 0.0703291
 0.6088307 0.0640261
 0.6578783 0.0568937
 0.7068729 0.0490923
 0.7558185 0.0407918
 0.8047181 0.0321620
 0.8535675 0.0234733
 0.9023817 0.0149853
 0.9511766 0.0070179
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0013356 -.0068281
 0.0041940 -.0111861
 0.0080518 -.0146640
 0.0129090 -.0172616
 0.0226835 -.0194576
 0.0324820 -.0204537
 0.0570021 -.0217444
 0.0962359 -.0237295
 0.1354696 -.0257145
 0.1747054 -.0275996
 0.2139372 -.0296847
 0.2531670 -.0318697
 0.3127909 -.0349728
 0.3616514 -.0367204
 0.4105350 -.0373181
 0.4594425 -.0362260
 0.5084032 -.0339448
 0.5574017 -.0307641
 0.6064432 -.0269042
 0.6555237 -.0225549
 0.7046501 -.0178766
 0.7538183 -.0130790
 0.8030236 -.0083921
 0.8522694 -.0041262
 0.9015374 -.0007209
 0.9508063 0.0012641
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for NACA 64(1)-212 MOD A (n64212ma-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   n64212ma-il50,000929.9 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   n64212ma-il50,000528.1 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   n64212ma-il100,000942.5 at α=2.75°Mach=0 Ncrit=9Xfoil predictionDetails
   n64212ma-il100,000538.7 at α=8°Mach=0 Ncrit=5Xfoil predictionDetails
   n64212ma-il200,000949.2 at α=8.5°Mach=0 Ncrit=9Xfoil predictionDetails
   n64212ma-il200,000548.4 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   n64212ma-il500,000968.5 at α=9.25°Mach=0 Ncrit=9Xfoil predictionDetails
   n64212ma-il500,000568.7 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   n64212ma-il1,000,000983.4 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   n64212ma-il1,000,000579.1 at α=8.5°Mach=0 Ncrit=5Xfoil predictionDetails
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