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LIEBECK L1003 AIRFOIL (l1003-il)

LIEBECK L1003 AIRFOIL - Liebeck high lift airfoil


Airfoil l1003-il
Details Dat file Parser  
(l1003-il) LIEBECK L1003 AIRFOIL
Liebeck high lift airfoil
Max thickness 17.7% at 30% chord.
Max camber 6.5% at 30% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
LIEBECK L1003 AIRFOIL
       25.       25.

  0.000000  0.000000
  0.012500  0.023070
  0.025000  0.039810
  0.037500  0.050930
  0.050000  0.062960
  0.075000  0.083330
  0.100000  0.097220
  0.150000  0.122220
  0.200000  0.137040
  0.250000  0.148150
  0.300000  0.153700
  0.350000  0.148150
  0.400000  0.135180
  0.450000  0.118520
  0.500000  0.096300
  0.550000  0.080560
  0.600000  0.066670
  0.650000  0.051850
  0.700000  0.040740
  0.750000  0.028700
  0.800000  0.020370
  0.850000  0.012040
  0.900000  0.005560
  0.950000  0.001850
  1.000000  0.000000

  0.000000  0.000000
  0.012500 -0.037040
  0.025000 -0.046300
  0.037500 -0.049070
  0.050000 -0.049070
  0.075000 -0.043520
  0.100000 -0.039810
  0.150000 -0.033330
  0.200000 -0.028700
  0.250000 -0.025930
  0.300000 -0.023150
  0.350000 -0.020370
  0.400000 -0.018520
  0.450000 -0.016670
  0.500000 -0.014810
  0.550000 -0.012960
  0.600000 -0.011110
  0.650000 -0.009260
  0.700000 -0.007410
  0.750000 -0.005560
  0.800000 -0.003700
  0.850000 -0.002780
  0.900000 -0.001850
  0.950000 -0.000930
  1.000000  0.000000

Dat file parser warnings
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Lednicer format dat file
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Polars for LIEBECK L1003 AIRFOIL (l1003-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   l1003-il50,00094.1 at α=14.75°Mach=0 Ncrit=9Xfoil predictionDetails
   l1003-il50,00055.2 at α=17.75°Mach=0 Ncrit=5Xfoil predictionDetails
   l1003-il100,00094.5 at α=14.25°Mach=0 Ncrit=9Xfoil predictionDetails
   l1003-il100,00057 at α=17.25°Mach=0 Ncrit=5Xfoil predictionDetails
   l1003-il200,000910.2 at α=18.75°Mach=0 Ncrit=9Xfoil predictionDetails
   l1003-il200,000510.1 at α=15.25°Mach=0 Ncrit=5Xfoil predictionDetails
   l1003-il500,000974.1 at α=10°Mach=0 Ncrit=9Xfoil predictionDetails
   l1003-il500,000568.3 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   l1003-il1,000,0009104.1 at α=8.25°Mach=0 Ncrit=9Xfoil predictionDetails
   l1003-il1,000,000568.8 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
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