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BOEING BACXXX AIRFOIL (bacxxx-il)

BOEING BACXXX AIRFOIL - Boeing Commercial Airplane Company BACXXX Energy Efficient Transport Program airfoil


Airfoil bacxxx-il
Details Dat file Parser  
(bacxxx-il) BOEING BACXXX AIRFOIL
Boeing Commercial Airplane Company BACXXX Energy Efficient Transport Program airfoil
Max thickness 11.3% at 35% chord.
Max camber 1.4% at 15% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
 BOEING BACXXX AIRFOIL
       31.       31.
 
 0.0000    0.0000
 0.0005    0.0037
 0.0010    0.0050
 0.0025    0.0078
 0.0050    0.0112
 0.0150    0.0207
 0.0200    0.0242
 0.0250    0.0271
 0.0375    0.0334
 0.0500    0.0384
 0.0750    0.0465
 0.1000    0.0521
 0.1250    0.0566
 0.1500    0.0599
 0.2000    0.0643
 0.2500    0.0665
 0.3000    0.0674
 0.3500    0.0673
 0.4000    0.0667
 0.4500    0.0654
 0.5000    0.0636
 0.5500    0.0613
 0.6000    0.0585
 0.6500    0.0548
 0.7000    0.0503
 0.7500    0.0450
 0.8000    0.0384
 0.8500    0.0307
 0.9000    0.0218
 0.9500    0.0116
 1.0000    0.0004
 
 0.0000    0.0000
 0.0005    -.0018
 0.0010    -.0027
 0.0025    -.0043
 0.0050    -.0058
 0.0150    -.0098
 0.0200    -.0112
 0.0250    -.0125
 0.0375    -.0152
 0.0500    -.0175
 0.0750    -.0216
 0.1000    -.0254
 0.1250    -.0288
 0.1500    -.0320
 0.2000    -.0375
 0.2500    -.0417
 0.3000    -.0445
 0.3500    -.0458
 0.4000    -.0457
 0.4500    -.0443
 0.5000    -.0417
 0.5500    -.0383
 0.6000    -.0344
 0.6500    -.0303
 0.7000    -.0260
 0.7500    -.0218
 0.8000    -.0174
 0.8500    -.0132
 0.9000    -.0090
 0.9500    -.0047
 1.0000    -.0004
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Lednicer format dat file
Selig format dat file

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Polars for BOEING BACXXX AIRFOIL (bacxxx-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   bacxxx-il50,000931.2 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   bacxxx-il50,000530.8 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   bacxxx-il100,000944 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   bacxxx-il100,000542.7 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   bacxxx-il200,000958.4 at α=2.75°Mach=0 Ncrit=9Xfoil predictionDetails
   bacxxx-il200,000555.2 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   bacxxx-il500,000975.2 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   bacxxx-il500,000572.8 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   bacxxx-il1,000,000990.3 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   bacxxx-il1,000,000586.5 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
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