SA7036 (sa7036-il)
SA7036 - Selig / Ashok Gopalarathnam SA7036
| Details | Dat file | Parser | |
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(sa7036-il) SA7036 Selig / Ashok Gopalarathnam SA7036 Max thickness 9.2% at 28.1% chord. Max camber 2.6% at 42.1% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Selig format |
SA7036
1.00000 .00000
.99815 .00019
.99266 .00085
.98368 .00210
.97142 .00398
.95608 .00650
.93789 .00963
.91709 .01330
.89388 .01740
.86847 .02182
.84103 .02644
.81174 .03115
.78075 .03588
.74825 .04054
.71441 .04506
.67941 .04942
.64348 .05358
.60686 .05747
.56974 .06103
.53237 .06422
.49495 .06698
.45769 .06926
.42082 .07103
.38453 .07222
.34900 .07285
.31444 .07285
.28101 .07221
.24891 .07094
.21826 .06902
.18921 .06645
.16193 .06326
.13650 .05945
.11301 .05510
.09161 .05022
.07232 .04485
.05524 .03913
.04041 .03309
.02784 .02684
.01758 .02054
.00969 .01434
.00415 .00839
.00101 .00291
.00029 -.00154
.00297 -.00497
.00936 -.00810
.01873 -.01110
.03099 -.01375
.04613 -.01596
.06411 -.01779
.08481 -.01924
.10813 -.02030
.13395 -.02097
.16213 -.02129
.19250 -.02127
.22490 -.02094
.25913 -.02032
.29498 -.01945
.33225 -.01836
.37069 -.01709
.41006 -.01569
.45010 -.01418
.49055 -.01259
.53113 -.01093
.57163 -.00922
.61180 -.00754
.65136 -.00592
.69004 -.00442
.72754 -.00308
.76360 -.00190
.79795 -.00093
.83033 -.00015
.86048 .00043
.88816 .00084
.91320 .00111
.93542 .00123
.95463 .00120
.97067 .00103
.98337 .00075
.99256 .00042
.99813 .00013
1.00000 .00000
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Polars for SA7036 (sa7036-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| sa7036-il | 50,000 | 9 | 33.6 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sa7036-il | 50,000 | 5 | 38.5 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sa7036-il | 100,000 | 9 | 53.9 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sa7036-il | 100,000 | 5 | 54.5 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sa7036-il | 200,000 | 9 | 73 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sa7036-il | 200,000 | 5 | 69.5 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sa7036-il | 500,000 | 9 | 97.1 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sa7036-il | 500,000 | 5 | 88.9 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sa7036-il | 1,000,000 | 9 | 114 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sa7036-il | 1,000,000 | 5 | 103.5 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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