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

LIEBECK LA5055 AIRFOIL (la5055-il)

LIEBECK LA5055 AIRFOIL - Liebeck high lift airfoil


Airfoil la5055-il
Details Dat file Parser  
(la5055-il) LIEBECK LA5055 AIRFOIL
Liebeck high lift airfoil
Max thickness 15.9% at 35% chord.
Max camber 5.9% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
LIEBECK LA5055 AIRFOIL
       25.       25.

  0.000000  0.000000
  0.012500  0.030600
  0.025000  0.042600
  0.037500  0.052800
  0.050000  0.061100
  0.075000  0.076900
  0.100000  0.088000
  0.150000  0.106500
  0.200000  0.118500
  0.250000  0.128700
  0.300000  0.134300
  0.350000  0.138900
  0.400000  0.137000
  0.450000  0.131500
  0.500000  0.119400
  0.550000  0.103700
  0.600000  0.087000
  0.650000  0.070400
  0.700000  0.058300
  0.750000  0.045400
  0.800000  0.032400
  0.850000  0.022200
  0.900000  0.014800
  0.950000  0.006500
  1.000000  0.000000

  0.000000  0.000000
  0.012500 -0.025900
  0.025000 -0.031500
  0.037500 -0.032400
  0.050000 -0.032400
  0.075000 -0.031500
  0.100000 -0.030600
  0.150000 -0.028700
  0.200000 -0.027800
  0.250000 -0.025000
  0.300000 -0.023100
  0.350000 -0.020400
  0.400000 -0.018500
  0.450000 -0.014800
  0.500000 -0.013900
  0.550000 -0.012000
  0.600000 -0.010200
  0.650000 -0.008300
  0.700000 -0.007400
  0.750000 -0.005600
  0.800000 -0.003700
  0.850000 -0.001900
  0.900000 -0.000900
  0.950000 -0.000500
  1.000000  0.000000

Dat file parser warnings
  • Line 53 - Invalid characters : 
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file

Similar airfoils

DOUGLAS LA203A AIRFOILPreviewDetails
AH 95-160PreviewDetails
Rhode St. Genese 36PreviewDetails
WORTMANN FX 057-816PreviewDetails
GOE 508 AIRFOILPreviewDetails
GOE 527 AIRFOILPreviewDetails
GOE 624 AIRFOILPreviewDetails
FX 76-MP-160PreviewDetails
GOE 481A AIRFOILPreviewDetails
GOE 289 (MVA 289) AIRFOILPreviewDetails

Polars for LIEBECK LA5055 AIRFOIL (la5055-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   la5055-il50,00094.9 at α=9°Mach=0 Ncrit=9Xfoil predictionDetails
   la5055-il50,00058.7 at α=13.25°Mach=0 Ncrit=5Xfoil predictionDetails
   la5055-il100,000918.7 at α=15.25°Mach=0 Ncrit=9Xfoil predictionDetails
   la5055-il100,000515.5 at α=13.25°Mach=0 Ncrit=5Xfoil predictionDetails
   la5055-il200,000924.7 at α=13.25°Mach=0 Ncrit=9Xfoil predictionDetails
   la5055-il200,000546.1 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   la5055-il500,0009116.3 at α=9°Mach=0 Ncrit=9Xfoil predictionDetails
   la5055-il500,0005104.2 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   la5055-il1,000,0009149.6 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   la5055-il1,000,000583.5 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
Reynolds number calculator
Set Reynolds number and Ncrit rangeLowHigh
Reynolds Number
NCrit