S8038 (13%) (s8038-il)
S8038 (13%) - Selig S8038 (13%) low Reynolds number airfoil
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(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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Polars for S8038 (13%) (s8038-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| s8038-il | 50,000 | 9 | 29.2 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s8038-il | 50,000 | 5 | 30.3 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s8038-il | 100,000 | 9 | 45.2 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s8038-il | 100,000 | 5 | 43.2 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s8038-il | 200,000 | 9 | 59.8 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s8038-il | 200,000 | 5 | 52.9 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s8038-il | 500,000 | 9 | 71.6 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s8038-il | 500,000 | 5 | 69 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s8038-il | 1,000,000 | 9 | 85.8 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s8038-il | 1,000,000 | 5 | 83.6 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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