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davissm (davissm-il)

davissm - Davis 3R F1B free flight airfoil (smoothed)


Airfoil davissm-il
Details Dat file Parser  
(davissm-il) davissm
Davis 3R F1B free flight airfoil (smoothed)
Max thickness 5.9% at 30.6% chord.
Max camber 5.9% at 45.4% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
davissm
  1.00000  0.00588
  0.99754  0.00719
  0.99070  0.01009
  0.98037  0.01307
  0.96698  0.01585
  0.95044  0.01919
  0.93064  0.02337
  0.90775  0.02831
  0.88202  0.03384
  0.85370  0.03980
  0.82309  0.04598
  0.79048  0.05217
  0.75616  0.05819
  0.72043  0.06387
  0.68359  0.06908
  0.64594  0.07373
  0.60778  0.07774
  0.56937  0.08107
  0.53099  0.08369
  0.49265  0.08559
  0.45435  0.08675
  0.41638  0.08712
  0.37887  0.08671
  0.34204  0.08547
  0.30609  0.08342
  0.27120  0.08053
  0.23760  0.07682
  0.20549  0.07230
  0.17504  0.06696
  0.14648  0.06085
  0.11999  0.05408
  0.09576  0.04697
  0.07395  0.04001
  0.05468  0.03359
  0.03811  0.02757
  0.02433  0.02159
  0.01338  0.01552
  0.00548  0.00957
  0.00098  0.00384
       0.00000    -0.00003
       0.00098    -0.00354
       0.00548    -0.00727
       0.01338    -0.00901
       0.02433    -0.00845
       0.03811    -0.00648
       0.05468    -0.00385
       0.07395    -0.00091
       0.09576     0.00220
       0.11999     0.00545
       0.14648     0.00879
       0.17504     0.01218
       0.20549     0.01557
       0.23760     0.01884
       0.27120     0.02191
       0.30609     0.02468
       0.34204     0.02707
       0.37887     0.02901
       0.41638     0.03047
       0.45435     0.03140
       0.49265     0.03181
       0.53099     0.03168
       0.56937     0.03104
       0.60778     0.02987
       0.64594     0.02822
       0.68359     0.02613
       0.72043     0.02364
       0.75616     0.02082
       0.79048     0.01776
       0.82309     0.01453
       0.85370     0.01124
       0.88202     0.00798
       0.90775     0.00486
       0.93064     0.00191
       0.95044    -0.00086
       0.96698    -0.00339
       0.98037    -0.00530
       0.99070    -0.00620
       0.99754    -0.00612
       1.00000    -0.00590
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Selig format dat file

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Polars for davissm (davissm-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   davissm-il50,000945.4 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   davissm-il50,000545.7 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   davissm-il100,000970.2 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   davissm-il100,000569.4 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   davissm-il200,000996.5 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   davissm-il200,000592.5 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   davissm-il500,0009131.7 at α=3.25°Mach=0 Ncrit=9Xfoil predictionDetails
   davissm-il500,0005118.8 at α=2.25°Mach=0 Ncrit=5Xfoil predictionDetails
   davissm-il1,000,0009154.7 at α=2.25°Mach=0 Ncrit=9Xfoil predictionDetails
   davissm-il1,000,0005128.8 at α=2.75°Mach=0 Ncrit=5Xfoil predictionDetails
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