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EPPLER STF 863-615 AIRFOIL (stf86361-il)

EPPLER STF 863-615 AIRFOIL - Eppler STF 863-615 airfoil


Airfoil stf86361-il
Details Dat file Parser  
(stf86361-il) EPPLER STF 863-615 AIRFOIL
Eppler STF 863-615 airfoil
Max thickness 14.7% at 44.7% chord.
Max camber 4.2% at 72.3% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
EPPLER STF 863-615 AIRFOIL
      33.0      28.0
 
 0.0003200 0.0130400
 0.0015800 0.0183800
 0.0087300 0.0255100
 0.0207500 0.0336300
 0.0373800 0.0422900
 0.0584600 0.0511700
 0.0837300 0.0600300
 0.1129700 0.0686600
 0.1458600 0.0768700
 0.1821000 0.0844900
 0.2213200 0.0914000
 0.2631200 0.0974400
 0.3070800 0.1025300
 0.3527600 0.1068500
 0.3997100 0.1094400
 0.4474300 0.1111200
 0.4954800 0.1118700
 0.5432700 0.1107300
 0.5904100 0.1085900
 0.6363600 0.1051400
 0.6808600 0.1003400
 0.7228000 0.0941700
 0.7622600 0.0863200
 0.7993300 0.0762200
 0.8349100 0.0645300
 0.8686900 0.0527200
 0.8995800 0.0414500
 0.9268900 0.0306700
 0.9505600 0.0205100
 0.9705100 0.0116700
 0.9861600 0.0050400
 0.9964000 0.0011900
 1.0000000 0.0000000
 
 0.0003200 0.0130400
 0.0037000 0.0085000
 0.0172900 0.0038200
 0.0343700 -.0016100
 0.0565800 -.0067200
 0.0835900 -.0117000
 0.1150300 -.0164600
 0.1505000 -.0209000
 0.1895600 -.0249300
 0.2317400 -.0284700
 0.2765200 -.0314200
 0.3233700 -.0336800
 0.3717400 -.0351500
 0.4210400 -.0356900
 0.4706700 -.0351200
 0.5200300 -.0332100
 0.5684100 -.0291500
 0.6168200 -.0217100
 0.6671600 -.0122300
 0.7189100 -.0034400
 0.7700700 0.0033600
 0.8189700 0.0079400
 0.8641800 0.0102000
 0.9044800 0.0103400
 0.9386100 0.0086800
 0.9655900 0.0059100
 0.9848100 0.0029900
 0.9962300 0.0008100
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Lednicer format dat file
Selig format dat file

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Polars for EPPLER STF 863-615 AIRFOIL (stf86361-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   stf86361-il50,000922.2 at α=8.25°Mach=0 Ncrit=9Xfoil predictionDetails
   stf86361-il50,000523.7 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
   stf86361-il100,000932.1 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   stf86361-il100,000534.9 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   stf86361-il200,000954.3 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   stf86361-il200,000556.3 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   stf86361-il500,000992.2 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   stf86361-il500,000598.7 at α=3°Mach=0 Ncrit=5Xfoil predictionDetails
   stf86361-il1,000,0009145.1 at α=2.75°Mach=0 Ncrit=9Xfoil predictionDetails
   stf86361-il1,000,0005142.7 at α=1.75°Mach=0 Ncrit=5Xfoil predictionDetails
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