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WASP (smoothed) (waspsm-il)

WASP (smoothed) - Mike Fox WASP low Reynolds number airfoil


Airfoil waspsm-il
Details Dat file Parser  
(waspsm-il) WASP (smoothed)
Mike Fox WASP low Reynolds number airfoil
Max thickness 9.4% at 27.1% chord.
Max camber 3% at 37.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
WASP (smoothed)
       1.00000     0.00007
       0.99754     0.00132
       0.99070     0.00392
       0.98037     0.00632
       0.96698     0.00831
       0.95044     0.01060
       0.93064     0.01373
       0.90775     0.01754
       0.88202     0.02173
       0.85370     0.02616
       0.82309     0.03071
       0.79048     0.03534
       0.75616     0.04001
       0.72043     0.04467
       0.68359     0.04923
       0.64594     0.05362
       0.60778     0.05775
       0.56937     0.06154
       0.53099     0.06495
       0.49265     0.06796
       0.45435     0.07055
       0.41638     0.07265
       0.37887     0.07421
       0.34204     0.07514
       0.30609     0.07537
       0.27120     0.07482
       0.23760     0.07345
       0.20549     0.07122
       0.17504     0.06813
       0.14648     0.06419
       0.11999     0.05944
       0.09576     0.05388
       0.07395     0.04750
       0.05468     0.04040
       0.03811     0.03288
       0.02433     0.02528
       0.01338     0.01779
       0.00548     0.01060
       0.00098     0.00395
       0.00000    -0.00042
       0.00098    -0.00434
       0.00548    -0.00897
       0.01338    -0.01273
       0.02433    -0.01570
       0.03811    -0.01799
       0.05468    -0.01973
       0.07395    -0.02094
       0.09576    -0.02167
       0.11999    -0.02197
       0.14648    -0.02189
       0.17504    -0.02147
       0.20549    -0.02077
       0.23760    -0.01984
       0.27120    -0.01872
       0.30609    -0.01746
       0.34204    -0.01608
       0.37887    -0.01462
       0.41638    -0.01309
       0.45435    -0.01154
       0.49265    -0.01002
       0.53099    -0.00856
       0.56937    -0.00723
       0.60778    -0.00604
       0.64594    -0.00503
       0.68359    -0.00420
       0.72043    -0.00353
       0.75616    -0.00299
       0.79048    -0.00258
       0.82309    -0.00231
       0.85370    -0.00220
       0.88202    -0.00223
       0.90775    -0.00237
       0.93064    -0.00258
       0.95044    -0.00291
       0.96698    -0.00323
       0.98037    -0.00313
       0.99070    -0.00225
       0.99754    -0.00088
       1.00000    -0.00016
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Polars for WASP (smoothed) (waspsm-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   waspsm-il50,000931.1 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   waspsm-il50,000537.5 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   waspsm-il100,000951 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   waspsm-il100,000553.2 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   waspsm-il200,000969.7 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   waspsm-il200,000569.1 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   waspsm-il500,000996 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   waspsm-il500,000591 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   waspsm-il1,000,0009115.8 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   waspsm-il1,000,0005108.1 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
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