MUE 139 (mue139-il)
MUE 139 - MUE 139 airfoil
| Details | Dat file | Parser | |
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(mue139-il) MUE 139 MUE 139 airfoil Max thickness 13.9% at 22.2% chord. Max camber 4.7% at 30.9% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Selig format |
MUE 139 1.00000 0.00000 0.99893 0.00026 0.99572 0.00103 0.99039 0.00229 0.98296 0.00399 0.97347 0.00605 0.96194 0.00841 0.94844 0.01102 0.93301 0.01390 0.91573 0.01709 0.89668 0.02061 0.87592 0.02445 0.85355 0.02858 0.82967 0.03297 0.80438 0.03759 0.77779 0.04241 0.75000 0.04744 0.72114 0.05270 0.69134 0.05822 0.66072 0.06397 0.62941 0.06984 0.59755 0.07572 0.56526 0.08145 0.53270 0.08689 0.50000 0.09194 0.46730 0.09655 0.43474 0.10076 0.40245 0.10463 0.37059 0.10815 0.33928 0.11113 0.30866 0.11334 0.27886 0.11462 0.25000 0.11495 0.22221 0.11439 0.19562 0.11281 0.17033 0.10991 0.14645 0.10565 0.12408 0.10024 0.10332 0.09396 0.08427 0.08689 0.06699 0.07895 0.05156 0.07015 0.03806 0.06066 0.02653 0.05040 0.01704 0.03952 0.00961 0.02820 0.00428 0.01698 0.00107 0.00747 0.00000 0.00000 0.00107 -0.00622 0.00428 -0.01222 0.00961 -0.01845 0.01704 -0.02380 0.02653 -0.02767 0.03806 -0.03026 0.05156 -0.03167 0.06699 -0.03209 0.08427 -0.03166 0.10332 -0.03075 0.12408 -0.02961 0.14645 -0.02845 0.17033 -0.02726 0.19562 -0.02595 0.22221 -0.02456 0.25000 -0.02287 0.27886 -0.02082 0.30866 -0.01864 0.33928 -0.01667 0.37059 -0.01513 0.40245 -0.01388 0.43474 -0.01265 0.46730 -0.01141 0.50000 -0.01025 0.53270 -0.00924 0.56526 -0.00841 0.59755 -0.00777 0.62941 -0.00728 0.66072 -0.00688 0.69134 -0.00651 0.72114 -0.00614 0.75000 -0.00574 0.77779 -0.00530 0.80438 -0.00483 0.82967 -0.00435 0.85355 -0.00388 0.87592 -0.00345 0.89668 -0.00307 0.91573 -0.00274 0.93301 -0.00248 0.94844 -0.00222 0.96194 -0.00190 0.97347 -0.00151 0.98296 -0.00106 0.99039 -0.00064 0.99572 -0.00030 0.99893 -0.00008 1.00000 0.00000 |
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Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file |
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Polars for MUE 139 (mue139-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| mue139-il | 50,000 | 9 | 15.7 at α=1.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mue139-il | 50,000 | 5 | 27.3 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mue139-il | 100,000 | 9 | 35.3 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mue139-il | 100,000 | 5 | 44.9 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mue139-il | 200,000 | 9 | 58.3 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mue139-il | 200,000 | 5 | 63.5 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mue139-il | 500,000 | 9 | 89.2 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mue139-il | 500,000 | 5 | 90.9 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mue139-il | 1,000,000 | 9 | 116.5 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mue139-il | 1,000,000 | 5 | 115.3 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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