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NASA/AMES 63A108 MOD C AIRFOIL (a63a108c-il)

NASA/AMES 63A108 MOD C AIRFOIL - NASA/AMES modification of the NACA 63A-108 airfoil


Airfoil a63a108c-il
Details Dat file Parser  
(a63a108c-il) NASA/AMES 63A108 MOD C AIRFOIL
NASA/AMES modification of the NACA 63A-108 airfoil
Max thickness 7.7% at 30% chord.
Max camber 0.5% at 12.5% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
NASA/AMES 63A108 MOD C AIRFOIL
50.        50.
 
.0         .0
.0002      .00445
.0004      .00549
.0006      .00626
.0008      .00687
.001       .00741
.002       .00943
.003       .01091
.004       .01212
.005       .01315
.010       .01695
.02        .02192
.03        .02539
.04        .02807
.05        .03024
.06        .03206
.07        .03360
.08        .03493
.09        .03608
.10        .03709
.125       .03911
.15        .04062
.175       .04173
.20        .04255
.25        .04351
.30        .04385
.35        .04362
.40        .04293
.45        .04176
.50        .04015
.55        .03810
.60        .03559
.65        .03258
.70        .02906
.725       .0272
.75        .0252
.775       .0231
.80        .0209
.825       .0187
.85        .0164
.875       .0141
.90        .0120
.925       .0101
.95        .0086
.96        .0080
.97        .0076
.98        .0073
.99        .0071
.995       .0070
1.         .0070
 
.0         .0
.0002     -.00277
.0004     -.00379
.0006     -.00440
.0008     -.00489
.001      -.00531
.002      -.00686
.003      -.00796
.004      -.00885
.005      -.00959
.010      -.01228
.02       -.01569
.03       -.01808
.04       -.01996
.05       -.02152
.06       -.02286
.07       -.02403
.08       -.02506
.09       -.02598
.10       -.02680
.125      -.02852
.15       -.02989
.175      -.03097
.20       -.03183
.25       -.03297
.30       -.03350
.35       -.03340
.40       -.03269
.45       -.03140
.50       -.02957
.55       -.02728
.60       -.02459
.65       -.02157
.70       -.01830
.725      -.01661
.75       -.01492
.775      -.01327
.80       -.01167
.825      -.01018
.85       -.00874
.875      -.00729
.90       -.00584
.925      -.00438
.95       -.00292
.96       -.00234
.97       -.00176
.98       -.00117
.99       -.00059
.995      -.00029
1.         .0
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Lednicer format dat file
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Polars for NASA/AMES 63A108 MOD C AIRFOIL (a63a108c-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   a63a108c-il50,000924.5 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   a63a108c-il50,000522.8 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   a63a108c-il100,000931.7 at α=3.25°Mach=0 Ncrit=9Xfoil predictionDetails
   a63a108c-il100,000531.2 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   a63a108c-il200,000937.1 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   a63a108c-il200,000541.8 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   a63a108c-il500,000954.4 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   a63a108c-il500,000558.8 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
   a63a108c-il1,000,000969.5 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   a63a108c-il1,000,000572.7 at α=8.25°Mach=0 Ncrit=5Xfoil predictionDetails
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