EPPLER STE 871-514 AIRFOIL (ste87151-il)
EPPLER STE 871-514 AIRFOIL - Eppler STE 871-514 airfoil
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(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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Polars for EPPLER STE 871-514 AIRFOIL (ste87151-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| ste87151-il | 50,000 | 9 | 28 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ste87151-il | 50,000 | 5 | 25.8 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ste87151-il | 100,000 | 9 | 40.6 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ste87151-il | 100,000 | 5 | 36.4 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ste87151-il | 200,000 | 9 | 55.2 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ste87151-il | 200,000 | 5 | 52.2 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ste87151-il | 500,000 | 9 | 81.8 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ste87151-il | 500,000 | 5 | 79.1 at α=2.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ste87151-il | 1,000,000 | 9 | 113.9 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ste87151-il | 1,000,000 | 5 | 104.5 at α=1.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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