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RAE 103 AIRFOIL (rae103-il)

RAE 103 AIRFOIL - RAE 103 airfoil


Airfoil rae103-il
Details Dat file Parser  
(rae103-il) RAE 103 AIRFOIL
RAE 103 airfoil
Max thickness 10% at 40% chord.
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
RAE 103 AIRFOIL
       86.       86.

  0.000000  0.000000
  0.001000  0.003556
  0.002000  0.005025
  0.003000  0.006151
  0.004000  0.007098
  0.005000  0.007931
  0.006000  0.008682
  0.007000  0.009372
  0.007500  0.009698
  0.008000  0.010013
  0.009000  0.010614
  0.010000  0.011181
  0.012000  0.012232
  0.012500  0.012480
  0.014000  0.013195
  0.016000  0.014088
  0.018000  0.014924
  0.020000  0.015711
  0.025000  0.017509
  0.030000  0.019118
  0.035000  0.020582
  0.040000  0.021931
  0.050000  0.024357
  0.060000  0.026503
  0.070000  0.028432
  0.075000  0.029328
  0.080000  0.030185
  0.090000  0.031792
  0.100000  0.033273
  0.120000  0.035921
  0.140000  0.038221
  0.150000  0.039258
  0.160000  0.040230
  0.180000  0.041992
  0.200000  0.043536
  0.220000  0.044884
  0.240000  0.046052
  0.250000  0.046574
  0.260000  0.047055
  0.280000  0.047900
  0.300000  0.048597
  0.320000  0.049151
  0.340000  0.049565
  0.350000  0.049720
  0.360000  0.049841
  0.380000  0.049982
  0.400000  0.049985
  0.420000  0.049848
  0.440000  0.049565
  0.450000  0.049367
  0.460000  0.049128
  0.480000  0.048523
  0.500000  0.047715
  0.520000  0.046644
  0.540000  0.045380
  0.550000  0.044689
  0.560000  0.043965
  0.580000  0.042423
  0.600000  0.040773
  0.620000  0.039030
  0.640000  0.037206
  0.650000  0.036267
  0.660000  0.035313
  0.680000  0.033362
  0.700000  0.031364
  0.720000  0.029326
  0.740000  0.027260
  0.750000  0.026218
  0.760000  0.025173
  0.780000  0.023074
  0.800000  0.020975
  0.820000  0.018877
  0.840000  0.016780
  0.850000  0.015731
  0.860000  0.014682
  0.880000  0.012585
  0.900000  0.010487
  0.920000  0.008390
  0.925000  0.007865
  0.940000  0.006292
  0.950000  0.005244
  0.960000  0.004195
  0.975000  0.002622
  0.980000  0.002097
  0.987500  0.001311
  1.000000  0.000000

  0.000000  0.000000
  0.001000 -0.003556
  0.002000 -0.005025
  0.003000 -0.006151
  0.004000 -0.007098
  0.005000 -0.007931
  0.006000 -0.008682
  0.007000 -0.009372
  0.007500 -0.009698
  0.008000 -0.010013
  0.009000 -0.010614
  0.010000 -0.011181
  0.012000 -0.012232
  0.012500 -0.012480
  0.014000 -0.013195
  0.016000 -0.014088
  0.018000 -0.014924
  0.020000 -0.015711
  0.025000 -0.017509
  0.030000 -0.019118
  0.035000 -0.020582
  0.040000 -0.021931
  0.050000 -0.024357
  0.060000 -0.026503
  0.070000 -0.028432
  0.075000 -0.029328
  0.080000 -0.030185
  0.090000 -0.031792
  0.100000 -0.033273
  0.120000 -0.035921
  0.140000 -0.038221
  0.150000 -0.039258
  0.160000 -0.040230
  0.180000 -0.041992
  0.200000 -0.043536
  0.220000 -0.044884
  0.240000 -0.046052
  0.250000 -0.046574
  0.260000 -0.047055
  0.280000 -0.047900
  0.300000 -0.048597
  0.320000 -0.049151
  0.340000 -0.049565
  0.350000 -0.049720
  0.360000 -0.049841
  0.380000 -0.049982
  0.400000 -0.049985
  0.420000 -0.049848
  0.440000 -0.049565
  0.450000 -0.049367
  0.460000 -0.049128
  0.480000 -0.048523
  0.500000 -0.047715
  0.520000 -0.046644
  0.540000 -0.045380
  0.550000 -0.044689
  0.560000 -0.043965
  0.580000 -0.042423
  0.600000 -0.040773
  0.620000 -0.039030
  0.640000 -0.037206
  0.650000 -0.036267
  0.660000 -0.035313
  0.680000 -0.033362
  0.700000 -0.031364
  0.720000 -0.029326
  0.740000 -0.027260
  0.750000 -0.026218
  0.760000 -0.025173
  0.780000 -0.023074
  0.800000 -0.020975
  0.820000 -0.018877
  0.840000 -0.016780
  0.850000 -0.015731
  0.860000 -0.014682
  0.880000 -0.012585
  0.900000 -0.010487
  0.920000 -0.008390
  0.925000 -0.007865
  0.940000 -0.006292
  0.950000 -0.005244
  0.960000 -0.004195
  0.975000 -0.002622
  0.980000 -0.002097
  0.987500 -0.001311
  1.000000  0.000000
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Lednicer format dat file
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Polars for RAE 103 AIRFOIL (rae103-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   rae103-il50,000927.8 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   rae103-il50,000527.1 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   rae103-il100,000940.2 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   rae103-il100,000536.5 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   rae103-il200,000948.6 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   rae103-il200,000539.2 at α=3.5°Mach=0 Ncrit=5Xfoil predictionDetails
   rae103-il500,000954.8 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   rae103-il500,000552.6 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   rae103-il1,000,000962.2 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   rae103-il1,000,000566 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
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