WORTMANN FX 60-126 AIRFOIL (fx60126-il)
WORTMANN FX 60-126 AIRFOIL - Wortmann FX 60-126 airfoil
| Details | Dat file | Parser | |
|
(fx60126-il) WORTMANN FX 60-126 AIRFOIL Wortmann FX 60-126 airfoil Max thickness 12.6% at 27.9% chord. Max camber 3.6% at 56.5% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
WORTMANN FX 60-126 AIRFOIL
49.0 49.0
0.0000000 0.0000000
0.0010700 0.0067500
0.0042800 0.0134900
0.0096100 0.0209600
0.0170400 0.0280200
0.0265300 0.0349300
0.0380600 0.0417400
0.0515600 0.0480800
0.0669900 0.0545700
0.0842700 0.0602100
0.1033200 0.0658500
0.1240800 0.0707700
0.1464500 0.0755500
0.1703300 0.0795800
0.1956200 0.0832700
0.2222100 0.0861500
0.2500000 0.0885900
0.2788600 0.0901900
0.3086600 0.0913000
0.3392800 0.0916000
0.3705900 0.0913800
0.4024500 0.0904100
0.4347400 0.0889300
0.4673000 0.0867900
0.5000000 0.0842500
0.5327000 0.0811800
0.5652600 0.0778100
0.5975500 0.0740200
0.6294100 0.0699400
0.6607200 0.0654900
0.6913400 0.0608200
0.7211400 0.0558900
0.7500000 0.0508400
0.7777900 0.0456700
0.8043800 0.0405500
0.8296700 0.0355200
0.8535500 0.0307000
0.8759200 0.0261100
0.8966800 0.0218100
0.9157300 0.0177700
0.9330100 0.0141200
0.9484400 0.0108400
0.9619400 0.0079800
0.9734700 0.0055400
0.9829600 0.0035300
0.9903900 0.0019800
0.9957200 0.0008800
0.9989300 0.0002400
1.0000000 0.0000000
0.0000000 0.0000000
0.0010700 -.0030100
0.0042800 -.0064100
0.0096100 -.0101200
0.0170400 -.0140400
0.0265300 -.0179200
0.0380600 -.0213200
0.0515600 -.0248200
0.0669900 -.0276100
0.0842700 -.0304500
0.1033200 -.0326200
0.1240800 -.0346500
0.1464500 -.0359800
0.1703300 -.0370700
0.1956200 -.0374600
0.2222100 -.0375100
0.2500000 -.0368300
0.2788600 -.0357400
0.3086600 -.0339200
0.3392800 -.0316700
0.3705900 -.0287700
0.4024500 -.0255300
0.4347400 -.0218800
0.4673000 -.0181400
0.5000000 -.0142100
0.5327000 -.0103600
0.5652600 -.0065300
0.5975500 -.0029800
0.6294100 0.0002900
0.6607200 0.0030700
0.6913400 0.0054700
0.7211400 0.0074100
0.7500000 0.0089700
0.7777900 0.0100600
0.8043800 0.0107300
0.8296700 0.0109300
0.8535500 0.0107400
0.8759200 0.0102200
0.8966800 0.0094400
0.9157300 0.0084500
0.9330100 0.0073200
0.9484400 0.0061000
0.9619400 0.0048300
0.9734700 0.0035700
0.9829600 0.0023900
0.9903900 0.0014600
0.9957200 0.0006800
0.9989300 0.0001400
1.0000000 0.0000000
|
No parser warnings |
Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file |
Similar airfoils
|
Polars for WORTMANN FX 60-126 AIRFOIL (fx60126-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| fx60126-il | 50,000 | 9 | 34.4 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx60126-il | 50,000 | 5 | 39.1 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx60126-il | 100,000 | 9 | 57.6 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx60126-il | 100,000 | 5 | 58.5 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx60126-il | 200,000 | 9 | 79.7 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx60126-il | 200,000 | 5 | 75.2 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx60126-il | 500,000 | 9 | 104 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx60126-il | 500,000 | 5 | 88.4 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx60126-il | 1,000,000 | 9 | 112.3 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx60126-il | 1,000,000 | 5 | 95.5 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| Reynolds number calculator | |||||||