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 79-K-144/17 AIRFOIL (fx79k144-il)

WORTMANN FX 79-K-144/17 AIRFOIL - Wortmann FX 79-K-144/17 sailplane airfoil


Airfoil fx79k144-il
Details Dat file Parser  
(fx79k144-il) WORTMANN FX 79-K-144/17 AIRFOIL
Wortmann FX 79-K-144/17 sailplane airfoil
Max thickness 14.4% at 43.5% chord.
Max camber 2.8% at 40.2% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
WORTMANN FX 79-K-144/17 AIRFOIL
       49.       49.

  0.000000  0.000000
  0.001070  0.004800
  0.004780  0.009900
  0.009610  0.015100
  0.017040  0.020600
  0.026530  0.026500
  0.038060  0.032700
  0.051560  0.039100
  0.066990  0.045400
  0.084270  0.051600
  0.103320  0.057700
  0.124080  0.063700
  0.146450  0.069500
  0.170330  0.074800
  0.195620  0.079900
  0.222210  0.084800
  0.250000  0.089100
  0.278860  0.092600
  0.308660  0.095500
  0.339280  0.097800
  0.370590  0.099200
  0.402450  0.100000
  0.434740  0.100100
  0.467300  0.099300
  0.500000  0.097700
  0.532700  0.095600
  0.565260  0.092700
  0.597550  0.088800
  0.629410  0.084500
  0.660720  0.079800
  0.691340  0.073500
  0.721140  0.065800
  0.750000  0.056900
  0.777790  0.047800
  0.804380  0.039700
  0.829670  0.033400
  0.853550  0.029300
  0.875920  0.025400
  0.896680  0.022000
  0.915730  0.018800
  0.933010  0.015600
  0.948440  0.012700
  0.961940  0.010000
  0.973470  0.007600
  0.982960  0.005700
  0.990390  0.004100
  0.995720  0.002800
  0.998930  0.002200
  1.000000  0.002000

  0.000000  0.000000
  0.001070 -0.004300
  0.004780 -0.008700
  0.009610 -0.012500
  0.017040 -0.015900
  0.026530 -0.019200
  0.038060 -0.022300
  0.051560 -0.025200
  0.066990 -0.027900
  0.084270 -0.030300
  0.103320 -0.032500
  0.124080 -0.034400
  0.146450 -0.036100
  0.170330 -0.037600
  0.195620 -0.038800
  0.222210 -0.039900
  0.250000 -0.040800
  0.278860 -0.041600
  0.308660 -0.042400
  0.339280 -0.043000
  0.370590 -0.043400
  0.402450 -0.043700
  0.434740 -0.043800
  0.467300 -0.043700
  0.500000 -0.043300
  0.532700 -0.042500
  0.565260 -0.041600
  0.597550 -0.040100
  0.629410 -0.038400
  0.660720 -0.036400
  0.691340 -0.034300
  0.721140 -0.031900
  0.750000 -0.028800
  0.777790 -0.024700
  0.804380 -0.020300
  0.829670 -0.015700
  0.853550 -0.011700
  0.875920 -0.008400
  0.896680 -0.005600
  0.915730 -0.003300
  0.933010 -0.001600
  0.948440 -0.000300
  0.961940  0.000500
  0.973470  0.001000
  0.982960  0.001000
  0.990390  0.000800
  0.995720  0.000400
  0.998930  0.000100
  1.000000  0.000000
No parser warnings Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file

Similar airfoils

AH 79-K-143/18PreviewDetails
EPPLER 642 AIRFOILPreviewDetails
NACA 747A415PreviewDetails
NACA 65(2)-415 a=0.5PreviewDetails
AH 88-K-136/16PreviewDetails
AH 82-150 APreviewDetails
NACA 747A315PreviewDetails
EPPLER 682 AIRFOILPreviewDetails
AH 79-K-135/20 BPreviewDetails
EPPLER 433 AIRFOILPreviewDetails

Polars for WORTMANN FX 79-K-144/17 AIRFOIL (fx79k144-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   fx79k144-il50,000924.2 at α=10°Mach=0 Ncrit=9Xfoil predictionDetails
   fx79k144-il50,000522.6 at α=9.75°Mach=0 Ncrit=5Xfoil predictionDetails
   fx79k144-il100,000944.3 at α=8.75°Mach=0 Ncrit=9Xfoil predictionDetails
   fx79k144-il100,000542.7 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
   fx79k144-il200,000975.2 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   fx79k144-il200,000565 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   fx79k144-il500,000991.3 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   fx79k144-il500,000589 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   fx79k144-il1,000,0009110.6 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   fx79k144-il1,000,0005102.7 at α=3.5°Mach=0 Ncrit=5Xfoil predictionDetails
Reynolds number calculator
Set Reynolds number and Ncrit rangeLowHigh
Reynolds Number
NCrit