UA(2)-180 (University of Alberta/Marsden) (ua2-180-il)
UA(2)-180 (University of Alberta/Marsden) - UA(2)-180 airfoil for ultralight category aircraft
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(ua2-180-il) UA(2)-180 (University of Alberta/Marsden) UA(2)-180 airfoil for ultralight category aircraft Max thickness 18.1% at 31.5% chord. Max camber 7% at 36.6% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Selig format |
UA(2)-180 (University of Alberta/Marsden) 1.0 0.0 0.99707 0.00083 0.98831 0.00299 0.97383 0.007 0.95379 0.01287 0.92843 0.01957 0.89805 0.02862 0.863 0.03857 0.82369 0.04995 0.78059 0.06232 0.7342 0.07579 0.68507 0.09062 0.63376 0.10395 0.58089 0.11821 0.52707 0.1316 0.47293 0.14577 0.41911 0.15593 0.36624 0.16039 0.31493 0.15929 0.2658 0.1554 0.21941 0.14735 0.17631 0.13731 0.137 0.12339 0.10195 0.1074 0.07157 0.08844 0.04621 0.06944 0.02617 0.04917 0.01169 0.03087 0.00293 0.01267 0.0 0.0 0.00293 -0.00976 0.02617 -0.01636 0.04621 -0.01871 0.07157 -0.02075 0.10195 -0.02201 0.137 -0.0231 0.17631 -0.0232 0.21941 -0.02329 0.2658 -0.02256 0.31493 -0.02196 0.36624 -0.02065 0.41911 -0.01958 0.47293 -0.01793 0.52707 -0.0166 0.58089 -0.01474 0.63376 -0.01334 0.68507 -0.01149 0.7342 -0.01013 0.78059 -0.00835 0.82369 -0.00708 0.863 -0.00544 0.89805 -0.00437 0.92843 -0.00303 0.95379 -0.00224 0.97383 -0.00112 0.98831 -0.00062 0.99707 0.0 1.0 0.0 |
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Polars for UA(2)-180 (University of Alberta/Marsden) (ua2-180-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| ua2-180-il | 50,000 | 9 | 3.9 at α=11.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ua2-180-il | 50,000 | 5 | 6.6 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ua2-180-il | 100,000 | 9 | 5 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ua2-180-il | 100,000 | 5 | 23.8 at α=2.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ua2-180-il | 200,000 | 9 | 30.2 at α=2.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ua2-180-il | 200,000 | 5 | 55.8 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ua2-180-il | 500,000 | 9 | 103.9 at α=9.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ua2-180-il | 500,000 | 5 | 107 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ua2-180-il | 1,000,000 | 9 | 146.2 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ua2-180-il | 1,000,000 | 5 | 139.6 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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