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S1046 17% (Danny Howell) (s1046-il)

S1046 17% (Danny Howell) - Selig S1046 airfoil


Airfoil s1046-il
Details Dat file Parser  
(s1046-il) S1046 17% (Danny Howell)
Selig S1046 airfoil
Max thickness 17% at 30.8% chord.
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
       S1046 17% (Danny Howell)
       1.00000     0.00000
       0.99616     0.00022
       0.98513     0.00134
       0.96778     0.00347
       0.94451     0.00634
       0.91556     0.01001
       0.88146     0.01459
       0.84282     0.02007
       0.80030     0.02639
       0.75460     0.03341
       0.70644     0.04097
       0.65656     0.04882
       0.60571     0.05665
       0.55447     0.06395
       0.50324     0.07044
       0.45251     0.07597
       0.40277     0.08035
       0.35450     0.08339
       0.30811     0.08495
       0.26398     0.08492
       0.22247     0.08324
       0.18385     0.07984
       0.14834     0.07476
       0.11614     0.06815
       0.08745     0.06017
       0.06246     0.05106
       0.04136     0.04107
       0.02431     0.03052
       0.01149     0.01974
       0.00306     0.00925
       0.00000     0.00000
       0.00306    -0.00925
       0.01149    -0.01974
       0.02431    -0.03052
       0.04136    -0.04107
       0.06246    -0.05106
       0.08745    -0.06017
       0.11614    -0.06815
       0.14834    -0.07476
       0.18385    -0.07984
       0.22247    -0.08324
       0.26398    -0.08492
       0.30811    -0.08495
       0.35450    -0.08339
       0.40277    -0.08035
       0.45251    -0.07597
       0.50324    -0.07044
       0.55447    -0.06395
       0.60571    -0.05665
       0.65656    -0.04882
       0.70644    -0.04097
       0.75460    -0.03341
       0.80030    -0.02639
       0.84282    -0.02007
       0.88146    -0.01459
       0.91556    -0.01001
       0.94451    -0.00634
       0.96778    -0.00347
       0.98513    -0.00134
       0.99616    -0.00022
       1.00000     0.00000
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Selig format dat file

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Polars for S1046 17% (Danny Howell) (s1046-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   s1046-il50,000916.2 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   s1046-il50,000525.3 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   s1046-il100,000937.2 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   s1046-il100,000540.5 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
   s1046-il200,000955 at α=8°Mach=0 Ncrit=9Xfoil predictionDetails
   s1046-il200,000554.6 at α=8.5°Mach=0 Ncrit=5Xfoil predictionDetails
   s1046-il500,000977 at α=9°Mach=0 Ncrit=9Xfoil predictionDetails
   s1046-il500,000570.4 at α=9°Mach=0 Ncrit=5Xfoil predictionDetails
   s1046-il1,000,000990.9 at α=9°Mach=0 Ncrit=9Xfoil predictionDetails
   s1046-il1,000,000580.9 at α=8°Mach=0 Ncrit=5Xfoil predictionDetails
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