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EPPLER STE 871-514 AIRFOIL (ste87151-il)

EPPLER STE 871-514 AIRFOIL - Eppler STE 871-514 airfoil


Airfoil ste87151-il
Details Dat file Parser  
(ste87151-il) EPPLER STE 871-514 AIRFOIL
Eppler STE 871-514 airfoil
Max thickness 13.9% at 47.3% chord.
Max camber 2.5% at 79% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
EPPLER STE 871-514 AIRFOIL
      32.0      29.0
 
 0.0004900 0.0074400
 0.0047100 0.0163400
 0.0129500 0.0256100
 0.0256000 0.0343600
 0.0432000 0.0425700
 0.0656500 0.0504900
 0.0925500 0.0581200
 0.1235900 0.0653200
 0.1583900 0.0719700
 0.1966000 0.0779700
 0.2378000 0.0832100
 0.2815500 0.0876200
 0.3274000 0.0911200
 0.3748600 0.0936500
 0.4234300 0.0951600
 0.4726000 0.0956200
 0.5218500 0.0949900
 0.5706700 0.0932700
 0.6185200 0.0901300
 0.6649000 0.0865000
 0.7093000 0.0814400
 0.7512300 0.0752300
 0.7901400 0.0675500
 0.8260800 0.0578000
 0.8608600 0.0466600
 0.8934000 0.0357800
 0.9227600 0.0259400
 0.9481500 0.0171700
 0.9692500 0.0097000
 0.9856200 0.0041200
 0.9962600 0.0009500
 1.0000000 0.0000000
 
 0.0004900 0.0074400
 0.0005900 0.0003900
 0.0067800 -.0049600
 0.0197200 -.0099600
 0.0382700 -.0148400
 0.0620700 -.0195100
 0.0907400 -.0239200
 0.1239000 -.0280100
 0.1611400 -.0317400
 0.2020000 -.0350600
 0.2459900 -.0379100
 0.2925900 -.0402700
 0.3412500 -.0420600
 0.3914000 -.0432500
 0.4424400 -.0437900
 0.4937800 -.0436000
 0.5448200 -.0426100
 0.5949100 -.0406900
 0.6435300 -.0377100
 0.6899400 -.0330200
 0.7348900 -.0256400
 0.7799500 -.0167800
 0.8245200 -.0088300
 0.8667600 -.0028800
 0.9050800 0.0008900
 0.9381700 0.0026000
 0.9649000 0.0026300
 0.9843700 0.0016500
 0.9961000 0.0005000
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Lednicer format dat file
Selig format dat file

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Polars for EPPLER STE 871-514 AIRFOIL (ste87151-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   ste87151-il50,000928 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   ste87151-il50,000525.8 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   ste87151-il100,000940.6 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   ste87151-il100,000536.4 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   ste87151-il200,000955.2 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   ste87151-il200,000552.2 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   ste87151-il500,000981.8 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   ste87151-il500,000579.1 at α=2.5°Mach=0 Ncrit=5Xfoil predictionDetails
   ste87151-il1,000,0009113.9 at α=2.75°Mach=0 Ncrit=9Xfoil predictionDetails
   ste87151-il1,000,0005104.5 at α=1.25°Mach=0 Ncrit=5Xfoil predictionDetails
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