WORTMANN FX 60-126/1 AIRFOIL (fx601261-il)
WORTMANN FX 60-126/1 AIRFOIL - Wortmann FX 60-126/1 airfoil
| Details | Dat file | Parser | |
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(fx601261-il) WORTMANN FX 60-126/1 AIRFOIL Wortmann FX 60-126/1 airfoil Max thickness 12.6% at 27.9% chord. Max camber 4% at 56.5% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
WORTMANN FX 60-126/1 AIRFOIL
49. 49.
0.0000000 0.0000000
0.0010200 0.0035900
0.0042200 0.0127900
0.0096000 0.0208600
0.0170200 0.0285600
0.0265000 0.0354500
0.0380200 0.0430700
0.0515800 0.0496200
0.0669400 0.0563600
0.0842200 0.0622400
0.1033000 0.0681500
0.1240300 0.0733100
0.1464300 0.0783500
0.1703700 0.0826000
0.1955800 0.0865300
0.2222100 0.0896200
0.2499800 0.0922700
0.2789100 0.0940500
0.3086100 0.0953300
0.3393300 0.0957700
0.3705600 0.0956700
0.4024300 0.0947800
0.4346900 0.0933700
0.4673300 0.0912200
0.4999700 0.0886200
0.5327400 0.0854200
0.5652500 0.0818300
0.5975000 0.0777400
0.6293800 0.0733400
0.6607400 0.0685400
0.6913300 0.0635400
0.7211500 0.0582900
0.7499501 0.0529500
0.7777300 0.0475900
0.8043500 0.0423700
0.8297000 0.0373900
0.8535000 0.0327000
0.8759000 0.0283000
0.8964400 0.0242700
0.9157100 0.0205400
0.9329900 0.0170700
0.9484800 0.0138100
0.9619200 0.0107200
0.9734400 0.0078400
0.9829100 0.0052800
0.9903400 0.0032300
0.9957100 0.0016100
0.9989100 0.0005200
1.0000000 0.0000000
0.0000000 0.0000000
0.0010200 -.0047200
0.0042200 -.0067500
0.0096000 -.0098300
0.0170200 -.0130800
0.0265000 -.0171000
0.0380200 -.0201700
0.0515800 -.0234200
0.0669400 -.0259400
0.0842200 -.0285200
0.1033000 -.0304200
0.1240300 -.0322000
0.1464300 -.0332700
0.1703700 -.0341200
0.1955800 -.0342600
0.2222100 -.0340900
0.2499800 -.0331900
0.2789100 -.0319100
0.3086100 -.0299200
0.3393300 -.0275200
0.3705600 -.0244900
0.4024300 -.0211700
0.4346900 -.0174600
0.4673300 -.0137100
0.4999700 -.0098500
0.5327400 -.0061400
0.5652500 -.0025300
0.5975000 0.0007200
0.6293800 0.0036500
0.6607400 0.0060900
0.6913300 0.0081500
0.7211500 0.0097800
0.7499501 0.0110600
0.7777300 0.0119000
0.8043500 0.0123600
0.8297000 0.0123900
0.8535000 0.0120800
0.8759000 0.0114600
0.8964400 0.0106000
0.9157100 0.0095500
0.9329900 0.0083600
0.9484800 0.0070600
0.9619200 0.0056800
0.9734400 0.0042700
0.9829100 0.0029200
0.9903400 0.0018200
0.9957100 0.0008900
0.9989100 0.0002100
1.0000000 0.0000000
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Polars for WORTMANN FX 60-126/1 AIRFOIL (fx601261-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| fx601261-il | 50,000 | 9 | 34.5 at α=8.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx601261-il | 50,000 | 5 | 39.4 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx601261-il | 100,000 | 9 | 59.4 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx601261-il | 100,000 | 5 | 60.5 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx601261-il | 200,000 | 9 | 82.9 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx601261-il | 200,000 | 5 | 76.2 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx601261-il | 500,000 | 9 | 108.2 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx601261-il | 500,000 | 5 | 84.2 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx601261-il | 1,000,000 | 9 | 113.3 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx601261-il | 1,000,000 | 5 | 88.2 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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