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NPL AIRFOIL FROM ARC CP 1372 (nplx-il)

NPL AIRFOIL FROM ARC CP 1372 - NPL transonic airfoil FROM ARC CP 1372


Airfoil nplx-il
Details Dat file Parser  
(nplx-il) NPL AIRFOIL FROM ARC CP 1372
NPL transonic airfoil FROM ARC CP 1372
Max thickness 10.7% at 35.8% chord.
Max camber 1.1% at 73.7% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
NPL AIRFOIL FROM ARC CP 1372
       34.       34.

  0.000000 -0.010150
  0.001000 -0.004300
  0.002990  0.001220
  0.004980  0.004110
  0.007360  0.006760
  0.014540  0.012000
  0.026420  0.016870
  0.042840  0.021490
  0.063730  0.025730
  0.088810  0.029810
  0.117910  0.033980
  0.150700  0.037930
  0.186870  0.041400
  0.226070  0.044170
  0.267960  0.046180
  0.312090  0.047620
  0.358060  0.048700
  0.405420  0.049130
  0.453730  0.049250
  0.502490  0.048730
  0.551240  0.047400
  0.599550  0.045550
  0.646920  0.042770
  0.692890  0.039090
  0.737020  0.034890
  0.778910  0.030510
  0.818110  0.026220
  0.854280  0.022080
  0.887070  0.017910
  0.900000  0.016200
  0.911870  0.014640
  0.937050  0.011130
  0.968520  0.006160
  1.000000  0.000000

  0.000000 -0.010150
  0.001000 -0.015060
  0.002990 -0.018410
  0.004980 -0.020120
  0.007360 -0.021900
  0.014540 -0.025810
  0.026420 -0.029950
  0.042840 -0.033870
  0.063730 -0.037570
  0.088810 -0.040800
  0.117910 -0.044130
  0.150700 -0.047130
  0.186870 -0.049910
  0.226070 -0.052910
  0.267960 -0.055660
  0.312090 -0.057320
  0.358060 -0.057960
  0.405420 -0.057010
  0.453730 -0.054030
  0.502490 -0.049320
  0.551240 -0.043630
  0.599550 -0.037340
  0.646920 -0.030880
  0.692890 -0.024600
  0.737020 -0.018700
  0.778910 -0.013650
  0.818110 -0.009350
  0.854280 -0.005900
  0.887070 -0.003250
  0.900000 -0.002450
  0.911870 -0.001560
  0.937050 -0.000430
  0.968520  0.000260
  1.000000  0.000000
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Lednicer format dat file
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Polars for NPL AIRFOIL FROM ARC CP 1372 (nplx-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   nplx-il50,000922 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   nplx-il50,000522.6 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   nplx-il100,000928.8 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   nplx-il100,000528.8 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   nplx-il200,000941 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   nplx-il200,000538.2 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   nplx-il500,000949.1 at α=2°Mach=0 Ncrit=9Xfoil predictionDetails
   nplx-il500,000554.6 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
   nplx-il1,000,000962.8 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   nplx-il1,000,000570.6 at α=8.75°Mach=0 Ncrit=5Xfoil predictionDetails
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