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MARSKE XM-1D AIRFOIL (F14-3.0) (marske1-il)

MARSKE XM-1D AIRFOIL (F14-3.0) - Marske XM-1D airfoil (F14-3.0)


Airfoil marske1-il
Details Dat file Parser  
(marske1-il) MARSKE XM-1D AIRFOIL (F14-3.0)
Marske XM-1D airfoil (F14-3.0)
Max thickness 14% at 25.1% chord.
Max camber 3% at 25.1% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
MARSKE XM-1D AIRFOIL (F14-3.0)
       17.       17.

  0.000000  0.000000
  0.012934  0.033131
  0.025588  0.044865
  0.050800  0.061035
  0.075950  0.072505
  0.101062  0.081076
  0.151221  0.093219
  0.201299  0.099163
  0.251314  0.100308
  0.301279  0.097653
  0.401119  0.085445
  0.500887  0.067738
  0.600603  0.046032
  0.700385  0.029425
  0.800216  0.016517
  0.900097  0.007409
  1.000000  0.000000

  0.000000  0.000000
  0.012274 -0.017261
  0.024717 -0.021624
  0.049677 -0.024651
  0.074602 -0.030377
  0.099569 -0.032904
  0.149516 -0.036959
  0.199489 -0.039013
  0.249480 -0.039668
  0.299472 -0.040323
  0.399455 -0.041633
  0.499437 -0.042943
  0.599473 -0.040253
  0.699552 -0.034164
  0.799669 -0.025276
  0.899821 -0.013688
  1.000000  0.000000
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Lednicer format dat file
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Polars for MARSKE XM-1D AIRFOIL (F14-3.0) (marske1-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   marske1-il50,00099.4 at α=0.5°Mach=0 Ncrit=9Xfoil predictionDetails
   marske1-il50,000517.8 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   marske1-il100,000921.7 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   marske1-il100,000538.4 at α=8°Mach=0 Ncrit=5Xfoil predictionDetails
   marske1-il200,000955.7 at α=11°Mach=0 Ncrit=9Xfoil predictionDetails
   marske1-il200,000560.4 at α=9°Mach=0 Ncrit=5Xfoil predictionDetails
   marske1-il500,000989.8 at α=9.75°Mach=0 Ncrit=9Xfoil predictionDetails
   marske1-il500,000588.8 at α=9.25°Mach=0 Ncrit=5Xfoil predictionDetails
   marske1-il1,000,0009115.3 at α=9.5°Mach=0 Ncrit=9Xfoil predictionDetails
   marske1-il1,000,0005104.7 at α=8.75°Mach=0 Ncrit=5Xfoil predictionDetails
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