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NACA 747A415 (naca747a415-il)

NACA 747A415 - NACA 747A415 airfoil


Airfoil naca747a415-il
Details Dat file Parser  
(naca747a415-il) NACA 747A415
NACA 747A415 airfoil
Max thickness 15% at 40.2% chord.
Max camber 3% at 35% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
NACA 747A415
1.00000     0.00000
0.95015     0.00639
0.90037     0.01546
0.85066     0.02592
0.80107     0.03692
0.75164     0.04783
0.70273     0.05838
0.65393     0.06878
0.60454     0.07859
0.55474     0.08753
0.50447     0.09516
0.45364     0.10121
0.40176     0.10499
0.34964     0.10497
0.29818     0.10216
0.24698     0.09687
0.19598     0.08897
0.14521     0.07827
0.09476     0.06390
0.06972     0.05488
0.04487     0.04411
0.02041     0.03016
0.00852     0.02106
0.00398     0.01622
0.00183     0.01318
0.00000     0.00000
0.00817     -0.00994
0.01102     -0.01160
0.01648     -0.01406
0.02959     -0.01822
0.05513     -0.02349
0.08028     -0.02730
0.10524     -0.03038
0.15479     -0.03501
0.20402     -0.03845
0.25302     -0.04095
0.30182     -0.04286
0.35036     -0.04411
0.39824     -0.04485
0.44636     -0.04493
0.49553     -0.04462
0.54526     -0.04381
0.59546     -0.04235
0.64607     -0.03992
0.69727     -0.03622
0.74836     -0.03053
0.79893     -0.02344
0.84934     -0.01578
0.89963     -0.00838
0.94985     -0.00247
1.00000     0.00000
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Lednicer format dat file
Selig format dat file

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Polars for NACA 747A415 (naca747a415-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   naca747a415-il50,000919 at α=11.5°Mach=0 Ncrit=9Xfoil predictionDetails
   naca747a415-il50,000517 at α=1°Mach=0 Ncrit=5Xfoil predictionDetails
   naca747a415-il100,000937.4 at α=9.5°Mach=0 Ncrit=9Xfoil predictionDetails
   naca747a415-il100,000544.5 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   naca747a415-il200,000973.8 at α=8°Mach=0 Ncrit=9Xfoil predictionDetails
   naca747a415-il200,000566.4 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
   naca747a415-il500,000997.5 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   naca747a415-il500,000592.6 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   naca747a415-il1,000,0009120.6 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   naca747a415-il1,000,0005110.9 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
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