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St. CYR 234 (Bartel 17-IC) (stcyr234-il)

St. CYR 234 (Bartel 17-IC) - St. CYR 234 (Bartel 17-IC) airfoil


Airfoil stcyr234-il
Details Dat file Parser  
(stcyr234-il) St. CYR 234 (Bartel 17-IC)
St. CYR 234 (Bartel 17-IC) airfoil
Max thickness 16% at 20% chord.
Max camber 5.1% at 50% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
St. CYR 234 (Bartel 17-IC)
1.0000     0.0000
0.9500     0.0200
0.9000     0.0400
0.8000     0.0775
0.7000     0.1080
0.6000     0.1330
0.5000     0.1520
0.4000     0.1610
0.3000     0.1655
0.2000     0.1620
0.1500     0.1570
0.1000     0.1460
0.0750     0.1380
0.0500     0.1270
0.0250     0.1100
0.0125     0.0955
0.0000     0.0642
0.0125     0.0375
0.0250     0.0270
0.0500     0.0140
0.0750     0.0085
0.1000     0.0050
0.1500     0.0025
0.2000     0.0020
0.3000     0.0065
0.4000     0.0110
0.5000     0.0135
0.6000     0.0190
0.7000     0.0135
0.8000     0.0105
0.9000     0.0050
0.9500     0.0025
1.0000     0.0000
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Selig format dat file

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Polars for St. CYR 234 (Bartel 17-IC) (stcyr234-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   stcyr234-il50,000928 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   stcyr234-il50,000526.8 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   stcyr234-il100,000947.2 at α=2.75°Mach=0 Ncrit=9Xfoil predictionDetails
   stcyr234-il100,000542.1 at α=1.75°Mach=0 Ncrit=5Xfoil predictionDetails
   stcyr234-il200,000972.9 at α=1°Mach=0 Ncrit=9Xfoil predictionDetails
   stcyr234-il200,000558 at α=0°Mach=0 Ncrit=5Xfoil predictionDetails
   stcyr234-il500,000987.3 at α=0°Mach=0 Ncrit=9Xfoil predictionDetails
   stcyr234-il500,000566.5 at α=-1.75°Mach=0 Ncrit=5Xfoil predictionDetails
   stcyr234-il1,000,000993.7 at α=-1.25°Mach=0 Ncrit=9Xfoil predictionDetails
   stcyr234-il1,000,000567.8 at α=3.25°Mach=0 Ncrit=5Xfoil predictionDetails
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