WORTMANN FX 08-S-176 AIRFOIL (fx08s176-il)
WORTMANN FX 08-S-176 AIRFOIL - Wortmann FX 08-S-176 airfoil
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(fx08s176-il) WORTMANN FX 08-S-176 AIRFOIL Wortmann FX 08-S-176 airfoil Max thickness 17.6% at 37.1% chord. Max camber 5.7% at 37.1% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
WORTMANN FX 08-S-176 AIRFOIL
25.0 25.0
0.0000000 0.0000000
0.0042800 0.0114000
0.0170400 0.0283200
0.0380600 0.0466800
0.0669900 0.0666300
0.1033300 0.0866100
0.1464400 0.1053900
0.1956200 0.1217100
0.2500000 0.1345800
0.3086600 0.1419300
0.3705900 0.1446200
0.4347400 0.1416200
0.5000000 0.1311800
0.5652600 0.1137700
0.6294100 0.0949300
0.6913400 0.0778800
0.7500000 0.0620800
0.8043800 0.0482900
0.8535600 0.0364400
0.8966700 0.0259600
0.9330100 0.0173600
0.9616400 0.0106500
0.9829600 0.0053700
0.9957200 0.0017700
1.0000000 0.0000000
0.0000000 0.0000000
0.0042800 -.0059100
0.0170400 -.0115600
0.0380600 -.0160000
0.0669900 -.0188600
0.1033300 -.0217700
0.1464400 -.0242000
0.1956200 -.0264400
0.2500000 -.0285900
0.3086600 -.0300000
0.3705900 -.0314300
0.4347400 -.0323100
0.5000000 -.0324500
0.5652600 -.0311600
0.6294100 -.0284500
0.6913400 -.0255600
0.7500000 -.0212000
0.8043800 -.0151900
0.8535600 -.0077000
0.8966700 -.0015700
0.9330100 0.0018400
0.9616400 0.0027000
0.9829600 0.0022500
0.9957200 0.0008200
1.0000000 0.0000000
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Polars for WORTMANN FX 08-S-176 AIRFOIL (fx08s176-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| fx08s176-il | 50,000 | 9 | 4.2 at α=13° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx08s176-il | 50,000 | 5 | 9.2 at α=-1.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx08s176-il | 100,000 | 9 | 5.1 at α=11.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx08s176-il | 100,000 | 5 | 20.4 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx08s176-il | 200,000 | 9 | 29.1 at α=12.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx08s176-il | 200,000 | 5 | 50.8 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx08s176-il | 500,000 | 9 | 108.8 at α=8.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx08s176-il | 500,000 | 5 | 106.8 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx08s176-il | 1,000,000 | 9 | 142 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx08s176-il | 1,000,000 | 5 | 139.3 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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