WORTMANN FX 05-H-126 AIRFOIL (fx05h126-il)
WORTMANN FX 05-H-126 AIRFOIL - Wortmann FX 05-H-126 rotorcraft airfoil
| Details | Dat file | Parser | |
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(fx05h126-il) WORTMANN FX 05-H-126 AIRFOIL Wortmann FX 05-H-126 rotorcraft airfoil Max thickness 12.6% at 37.1% chord. Max camber 4.4% at 37.1% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
WORTMANN FX 05-H-126 AIRFOIL
25.0 25.0
0.0000000 0.0000000
0.0042800 0.0118500
0.0170400 0.0256700
0.0380600 0.0398200
0.0669900 0.0536200
0.1033300 0.0675700
0.1464400 0.0801300
0.1956200 0.0912900
0.2500000 0.1000200
0.3086600 0.1055300
0.3705900 0.1070600
0.4347400 0.1042600
0.5000000 0.0946200
0.5652600 0.0788900
0.6294100 0.0617200
0.6913400 0.0457000
0.7500000 0.0316300
0.8043800 0.0203800
0.8535600 0.0120000
0.8966700 0.0060900
0.9330100 0.0023200
0.9616400 0.0005500
0.9829600 -.0001900
0.9957200 -.0001300
1.0000000 0.0000000
0.0000000 0.0000000
0.0042800 -.0068800
0.0170400 -.0113700
0.0380600 -.0143600
0.0669900 -.0158800
0.1033300 -.0171900
0.1464400 -.0177900
0.1956200 -.0181700
0.2500000 -.0186100
0.3086600 -.0193000
0.3705900 -.0190300
0.4347400 -.0188000
0.5000000 -.0179800
0.5652600 -.0166000
0.6294100 -.0153000
0.6913400 -.0139600
0.7500000 -.0124900
0.8043800 -.0110800
0.8535600 -.0093300
0.8966700 -.0075300
0.9330100 -.0056800
0.9616400 -.0040700
0.9829600 -.0023800
0.9957200 -.0009200
1.0000000 0.0000000
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Polars for WORTMANN FX 05-H-126 AIRFOIL (fx05h126-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| fx05h126-il | 50,000 | 9 | 19.1 at α=13.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx05h126-il | 50,000 | 5 | 14.5 at α=12.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx05h126-il | 100,000 | 9 | 25.1 at α=11.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx05h126-il | 100,000 | 5 | 24.3 at α=11° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx05h126-il | 200,000 | 9 | 66.3 at α=9.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx05h126-il | 200,000 | 5 | 70.8 at α=8.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx05h126-il | 500,000 | 9 | 121.3 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx05h126-il | 500,000 | 5 | 116.3 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx05h126-il | 1,000,000 | 9 | 158.3 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx05h126-il | 1,000,000 | 5 | 145.9 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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