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RUTAN CANARD AIRFOIL (amsoil1-il)

RUTAN CANARD AIRFOIL - Rutan AMSOIL racer canard airfoil


Airfoil amsoil1-il
Details Dat file Parser  
(amsoil1-il) RUTAN CANARD AIRFOIL
Rutan AMSOIL racer canard airfoil
Max thickness 11.6% at 39% chord.
Max camber 2.1% at 42% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
 RUTAN CANARD AIRFOIL
38.        38.
 
 0.00000   0.00000
  .00194    .00977
  .00388    .01353
  .00775    .01857
  .03000    .03318
  .06000    .04349
  .09000    .05054
  .12000    .05609
  .15000    .06070
  .18000    .06465
  .21000    .06810
  .24000    .07109
  .27000    .07357
  .30000    .07562
  .33000    .07717
  .36000    .07822
  .39000    .07880
  .42000    .07884
  .45000    .07833
  .48000    .07733
  .51000    .07574
  .54000    .07364
  .57000    .07101
  .60000    .06787
  .63000    .06426
  .66000    .06023
  .69000    .05578
  .72000    .05097
  .75000    .04585
  .78000    .04054
  .81000    .03504
  .84000    .02942
  .87000    .02384
  .90000    .01837
  .93000    .01310
  .96000    .00814
  .99000    .00360
 1.00000    .00221
 
 0.00000   0.00000
  .00194   -.00934
  .00388   -.01267
  .00775   -.01690
  .03000   -.02698
  .06000   -.03167
  .09000   -.03364
  .12000   -.03465
  .15000   -.03523
  .18000   -.03566
  .21000   -.03605
  .24000   -.03640
  .27000   -.03674
  .30000   -.03705
  .33000   -.03729
  .36000   -.03740
  .39000   -.03744
  .42000   -.03725
  .45000   -.03690
  .48000   -.03632
  .51000   -.03550
  .54000   -.03446
  .57000   -.03314
  .60000   -.03159
  .63000   -.02977
  .66000   -.02775
  .69000   -.02550
  .72000   -.02310
  .75000   -.02054
  .78000   -.01791
  .81000   -.01523
  .84000   -.01260
  .87000   -.01004
  .90000   -.00767
  .93000   -.00558
  .96000   -.00380
  .99000   -.00252
 1.00000   -.00221
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Lednicer format dat file
Selig format dat file

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Polars for RUTAN CANARD AIRFOIL (amsoil1-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   amsoil1-il50,000933 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   amsoil1-il50,000531.9 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   amsoil1-il100,000948.6 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   amsoil1-il100,000546.8 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   amsoil1-il200,000967.5 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   amsoil1-il200,000559.9 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   amsoil1-il500,000986.2 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   amsoil1-il500,000568.1 at α=2.75°Mach=0 Ncrit=5Xfoil predictionDetails
   amsoil1-il1,000,000993 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   amsoil1-il1,000,000581.1 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
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