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S8038 (13%) (s8038-il)

S8038 (13%) - Selig S8038 (13%) low Reynolds number airfoil


Airfoil s8038-il
Details Dat file Parser  
(s8038-il) S8038 (13%)
Selig S8038 (13%) low Reynolds number airfoil
Max thickness 13% at 32.9% chord.
Max camber 0.6% at 40.1% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
S8038 (13%)
       1.00000      .00000
        .99783      .00035
        .99175      .00162
        .98242      .00368
        .97012      .00616
        .95478      .00881
        .93639      .01168
        .91506      .01485
        .89102      .01832
        .86445      .02208
        .83559      .02611
        .80467      .03037
        .77194      .03482
        .73765      .03941
        .70207      .04406
        .66547      .04870
        .62813      .05325
        .59031      .05756
        .55220      .06154
        .51406      .06511
        .47608      .06814
        .43840      .07057
        .40126      .07238
        .36481      .07349
        .32917      .07393
        .29456      .07368
        .26115      .07274
        .22909      .07117
        .19857      .06898
        .16975      .06618
        .14280      .06284
        .11789      .05899
        .09517      .05464
        .07479      .04979
        .05681      .04445
        .04135      .03869
        .02845      .03242
        .01797      .02568
        .00996      .01878
        .00441      .01171
        .00110      .00471
        .00013     -.00157
        .00246     -.00701
        .00839     -.01227
        .01726     -.01760
        .02896     -.02284
        .04331     -.02791
        .06027     -.03270
        .07974     -.03716
        .10159     -.04122
        .12574     -.04483
        .15205     -.04800
        .18038     -.05065
        .21059     -.05279
        .24250     -.05442
        .27592     -.05550
        .31068     -.05606
        .34657     -.05607
        .38337     -.05554
        .42086     -.05447
        .45884     -.05281
        .49717     -.05056
        .53557     -.04775
        .57399     -.04435
        .61239     -.04051
        .65048     -.03645
        .68799     -.03230
        .72464     -.02819
        .76014     -.02420
        .79419     -.02043
        .82651     -.01694
        .85680     -.01378
        .88479     -.01099
        .91021     -.00857
        .93280     -.00651
        .95234     -.00477
        .96865     -.00326
        .98171     -.00186
        .99151     -.00074
        .99779     -.00012
       1.00000      .00000
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Selig format dat file

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Polars for S8038 (13%) (s8038-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   s8038-il50,000929.2 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   s8038-il50,000530.3 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   s8038-il100,000945.2 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   s8038-il100,000543.2 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   s8038-il200,000959.8 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   s8038-il200,000552.9 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   s8038-il500,000971.6 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   s8038-il500,000569 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   s8038-il1,000,000985.8 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   s8038-il1,000,000583.6 at α=8.5°Mach=0 Ncrit=5Xfoil predictionDetails
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