EPPLER STE 87(-3)-914 AIRFOIL (ste87391-il)
EPPLER STE 87(-3)-914 AIRFOIL - Eppler STE 87(-3)-914 airfoil
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(ste87391-il) EPPLER STE 87(-3)-914 AIRFOIL Eppler STE 87(-3)-914 airfoil Max thickness 14.6% at 34.1% chord. Max camber 4.2% at 58.3% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
EPPLER STE 87(-3)-914 AIRFOIL
33.0 28.0
0.0000000 0.0058600
0.0029200 0.0143600
0.0104800 0.0245200
0.0223500 0.0355600
0.0383000 0.0469700
0.0581700 0.0583300
0.0817400 0.0692600
0.1088100 0.0792900
0.1394100 0.0879300
0.1737300 0.0952300
0.2115300 0.1013300
0.2524000 0.1063200
0.2958200 0.1101900
0.3413300 0.1129100
0.3884400 0.1144600
0.4366500 0.1148300
0.4854300 0.1140200
0.5342700 0.1120400
0.5826400 0.1089000
0.6300300 0.1046200
0.6759400 0.0992600
0.7198400 0.0928300
0.7612700 0.0853500
0.7996900 0.0766700
0.8351400 0.0663700
0.8681900 0.0548600
0.8986700 0.0431900
0.9259600 0.0318500
0.9498300 0.0212000
0.9700700 0.0120200
0.9859600 0.0051800
0.9963500 0.0012200
1.0000000 0.0000000
0.0000000 0.0058600
0.0033300 -.0011000
0.0132200 -.0077400
0.0283400 -.0143900
0.0482700 -.0207100
0.0726200 -.0263900
0.1010400 -.0311200
0.1333300 -.0343100
0.1698900 -.0356900
0.2108300 -.0358400
0.2555600 -.0352100
0.3034500 -.0339600
0.3538500 -.0322400
0.4060800 -.0301200
0.4594600 -.0276700
0.5132800 -.0249000
0.5668200 -.0218000
0.6193600 -.0182800
0.6701600 -.0139300
0.7194000 -.0080600
0.7679800 -.0013300
0.8155100 0.0044800
0.8604900 0.0083500
0.9014500 0.0098600
0.9367100 0.0089200
0.9646800 0.0062500
0.9844900 0.0031700
0.9961600 0.0008600
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Polars for EPPLER STE 87(-3)-914 AIRFOIL (ste87391-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| ste87391-il | 50,000 | 9 | 32.2 at α=8.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ste87391-il | 50,000 | 5 | 30.9 at α=8.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ste87391-il | 100,000 | 9 | 51.3 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ste87391-il | 100,000 | 5 | 45.5 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ste87391-il | 200,000 | 9 | 69.5 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ste87391-il | 200,000 | 5 | 61.2 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ste87391-il | 500,000 | 9 | 97.4 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ste87391-il | 500,000 | 5 | 92.5 at α=1.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ste87391-il | 1,000,000 | 9 | 146 at α=1.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ste87391-il | 1,000,000 | 5 | 106.6 at α=-0.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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