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TRAINER60 (trainer60-il)

TRAINER60 - Great Planes R/C Trainer 60 airfoil


Airfoil trainer60-il
Details Dat file Parser  
(trainer60-il) TRAINER60
Great Planes R/C Trainer 60 airfoil
Max thickness 18.3% at 27.1% chord.
Max camber 0.1% at 1.3% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
  TRAINER60
 1.000000       0.003185
 0.997540       0.005714
 0.990700       0.010009
 0.980370       0.011484
 0.966980       0.010387
 0.950440       0.010252
 0.930640       0.010684
 0.907750       0.012469
 0.882020       0.016609
 0.853700       0.021789
 0.823090       0.027109
 0.790480       0.032331
 0.756160       0.037557
 0.720430       0.042964
 0.683590       0.048611
 0.645940       0.054465
 0.607780       0.060510
 0.569370       0.066568
 0.530990       0.072239
 0.492650       0.077322
 0.454350       0.081829
 0.416380       0.085729
 0.378870       0.088950
 0.342040       0.091378
 0.306090       0.092819
 0.271200       0.093034
 0.237600       0.091969
 0.205490       0.089867
 0.175040       0.086976
 0.146480       0.083240
 0.119990       0.078439
 0.095760       0.072371
 0.073950       0.065050
 0.054680       0.056881
 0.038110       0.048398
 0.024330       0.039859
 0.013380       0.031019
 0.005480       0.021182
 0.000980       0.009788
 0.000000       0.001166
 0.000980      -0.007076
 0.005480      -0.017397
 0.013380      -0.026742
 0.024330      -0.035600
 0.038110      -0.044257
 0.054680      -0.052773
 0.073950      -0.060946
 0.095760      -0.068412
 0.119990      -0.074764
 0.146480      -0.079792
 0.175040      -0.083671
 0.205490      -0.086674
 0.237600      -0.088864
 0.271200      -0.090048
 0.306090      -0.090043
 0.342040      -0.088848
 0.378870      -0.086658
 0.416380      -0.083707
 0.454350      -0.080022
 0.492650      -0.075530
 0.530990      -0.070300
 0.569370      -0.064622
 0.607780      -0.058941
 0.645940      -0.053447
 0.683590      -0.048006
 0.720430      -0.042495
 0.756160      -0.037036
 0.790480      -0.031861
 0.823090      -0.026990
 0.853700      -0.022223
 0.882020      -0.017468
 0.907750      -0.013184
 0.930640      -0.010637
 0.950440      -0.011123
 0.966980      -0.013591
 0.980370      -0.014815
 0.990700      -0.012156
 0.997540      -0.006587
 0.999997      -0.003499
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Selig format dat file

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Polars for TRAINER60 (trainer60-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   trainer60-il50,000915.3 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   trainer60-il50,000524.5 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
   trainer60-il100,000936.7 at α=9.25°Mach=0 Ncrit=9Xfoil predictionDetails
   trainer60-il100,000538.8 at α=8°Mach=0 Ncrit=5Xfoil predictionDetails
   trainer60-il200,000951.7 at α=8.25°Mach=0 Ncrit=9Xfoil predictionDetails
   trainer60-il200,000550.9 at α=9.25°Mach=0 Ncrit=5Xfoil predictionDetails
   trainer60-il500,000973.1 at α=10°Mach=0 Ncrit=9Xfoil predictionDetails
   trainer60-il500,000565.8 at α=8.75°Mach=0 Ncrit=5Xfoil predictionDetails
   trainer60-il1,000,000985.4 at α=8.25°Mach=0 Ncrit=9Xfoil predictionDetails
   trainer60-il1,000,000579.3 at α=8.5°Mach=0 Ncrit=5Xfoil predictionDetails
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