Airfoil Tools
Search 1636 airfoils Google+
You have 0 airfoils loaded.
Your Reynold number range is 50,000 to 1,000,000. (set)

WORTMANN FX 05-191 AIRFOIL (fx05191-il)

WORTMANN FX 05-191 AIRFOIL - Wortmann FX 05-191 airfoil


Airfoil fx05191-il
Details Dat file Parser  
(fx05191-il) WORTMANN FX 05-191 AIRFOIL
Wortmann FX 05-191 airfoil
Max thickness 19.1% at 37.1% chord.
Max camber 2.6% at 50% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
WORTMANN FX 05-191 AIRFOIL
      25.0      25.0
 
 0.0000000 0.0000000
 0.0042800 0.0131300
 0.0170400 0.0269600
 0.0380600 0.0414100
 0.0669900 0.0555800
 0.1033300 0.0702000
 0.1464400 0.0839900
 0.1956200 0.0964800
 0.2500000 0.1071300
 0.3086600 0.1151600
 0.3705900 0.1199800
 0.4347400 0.1209100
 0.5000000 0.1179800
 0.5652600 0.1117000
 0.6294100 0.1026600
 0.6913400 0.0912800
 0.7500000 0.0764200
 0.8043800 0.0597500
 0.8535600 0.0445200
 0.8966700 0.0316100
 0.9330100 0.0204300
 0.9616400 0.0124200
 0.9829600 0.0060800
 0.9957200 0.0019100
 1.0000000 0.0000000
 
 0.0000000 0.0000000
 0.0042800 -.0102700
 0.0170400 -.0196800
 0.0380600 -.0283700
 0.0669900 -.0368100
 0.1033300 -.0451000
 0.1464400 -.0527600
 0.1956200 -.0595700
 0.2500000 -.0652500
 0.3086600 -.0691800
 0.3705900 -.0708300
 0.4347400 -.0696400
 0.5000000 -.0655700
 0.5652600 -.0592900
 0.6294100 -.0509900
 0.6913400 -.0406400
 0.7500000 -.0280800
 0.8043800 -.0152600
 0.8535600 -.0053200
 0.8966700 0.0009700
 0.9330100 0.0045400
 0.9616400 0.0046000
 0.9829600 0.0034700
 0.9957200 0.0012900
 1.0000000 0.0000000
No parser warnings Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file

Similar airfoils

WORTMANN FX 05-188 AIRFOILPreviewDetails
FX 78-PK-188/20PreviewDetails
EPPLER 552 AIRFOILPreviewDetails
EPPLER 604 AIRFOILPreviewDetails
EPPLER 1098 AIRFOILPreviewDetails
FX S 03-182 AIRFOILPreviewDetails
NACA 63PreviewDetails
NACA 64(3)-418PreviewDetails
EPPLER 551 AIRFOILPreviewDetails
NACA 63(3)-618PreviewDetails

Polars for WORTMANN FX 05-191 AIRFOIL (fx05191-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   fx05191-il50,000918.1 at α=13.5°Mach=0 Ncrit=9Xfoil predictionDetails
   fx05191-il50,000514 at α=13°Mach=0 Ncrit=5Xfoil predictionDetails
   fx05191-il100,000927.6 at α=11.5°Mach=0 Ncrit=9Xfoil predictionDetails
   fx05191-il100,000529.2 at α=8.75°Mach=0 Ncrit=5Xfoil predictionDetails
   fx05191-il200,000955.6 at α=8.5°Mach=0 Ncrit=9Xfoil predictionDetails
   fx05191-il200,000557.9 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   fx05191-il500,000989.4 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   fx05191-il500,000589.9 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   fx05191-il1,000,0009118.9 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   fx05191-il1,000,0005112.6 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
Reynolds number calculator
Set Reynolds number and Ncrit rangeLowHigh
Reynolds Number
NCrit