SD7037-092-88 (sd7037-il)
SD7037-092-88 - Selig/Donovan SD7037 low Reynolds number airfoil
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(sd7037-il) SD7037-092-88 Selig/Donovan SD7037 low Reynolds number airfoil Max thickness 9.2% at 26.1% chord. Max camber 2.5% at 44.7% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Selig format |
SD7037-092-88 1.00000 0.0 0.99672 0.00042 0.98707 0.00180 0.97146 0.00436 0.95041 0.00811 0.92450 0.01295 0.89425 0.01865 0.86015 0.02490 0.82261 0.03141 0.78201 0.03788 0.73865 0.04413 0.69294 0.05011 0.64539 0.05572 0.59655 0.06085 0.54693 0.06538 0.49706 0.06917 0.44745 0.07211 0.39862 0.07410 0.35101 0.07504 0.30508 0.07488 0.26125 0.07358 0.21989 0.07113 0.18137 0.06754 0.14601 0.06286 0.11410 0.05715 0.08586 0.05049 0.06146 0.04300 0.04102 0.03486 0.02462 0.02632 0.01232 0.01770 0.00418 0.00936 0.00021 0.00185 0.00127 -0.00393 0.00806 -0.00839 0.02038 -0.01227 0.03800 -0.01541 0.06074 -0.01777 0.08844 -0.01934 0.12084 -0.02017 0.15765 -0.02032 0.19850 -0.01987 0.24296 -0.01891 0.29055 -0.01754 0.34071 -0.01586 0.39288 -0.01396 0.44643 -0.01190 0.50074 -0.00976 0.55519 -0.00760 0.60914 -0.00549 0.66197 -0.00349 0.71305 -0.00168 0.76178 -0.00014 0.80752 0.00104 0.84964 0.00182 0.88756 0.00220 0.92071 0.00218 0.94859 0.00185 0.97077 0.00132 0.98690 0.00071 0.99671 0.00021 1.00000 0.00000 |
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Polars for SD7037-092-88 (sd7037-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| sd7037-il | 50,000 | 9 | 34.5 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sd7037-il | 50,000 | 5 | 39.1 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sd7037-il | 100,000 | 9 | 55.2 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sd7037-il | 100,000 | 5 | 55.4 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sd7037-il | 200,000 | 9 | 74.7 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sd7037-il | 200,000 | 5 | 70.8 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sd7037-il | 500,000 | 9 | 99.3 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sd7037-il | 500,000 | 5 | 90.1 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sd7037-il | 1,000,000 | 9 | 116 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sd7037-il | 1,000,000 | 5 | 104.6 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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