Eiffel 371 (Monge) (eiffel371-il)
Eiffel 371 (Monge) - Eiffel 371 (Monge) airfoil
Details | Dat file | Parser | |
(eiffel371-il) Eiffel 371 (Monge) Eiffel 371 (Monge) airfoil Max thickness 14.4% at 30% chord. Max camber 3.3% at 30% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Selig format |
Eiffel 371 (Monge) 1.0000 0.0395 0.9500 0.0522 0.9000 0.0638 0.8000 0.0855 0.7000 0.1033 0.6000 0.1188 0.5000 0.1322 0.4000 0.1421 0.3000 0.1447 0.2000 0.1395 0.1500 0.1320 0.1000 0.1195 0.0750 0.1110 0.0500 0.0983 0.0250 0.0800 0.0125 0.0660 0.0000 0.0395 0.0125 0.0304 0.0250 0.0260 0.0500 0.0200 0.0750 0.0162 0.1000 0.0132 0.1500 0.0088 0.2000 0.0053 0.3000 0.0007 0.4000 0.0013 0.5000 0.0046 0.6000 0.0099 0.7000 0.0045 0.8000 0.0224 0.9000 0.0288 0.9500 0.0345 1.0000 0.0395 |
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Polars for Eiffel 371 (Monge) (eiffel371-il)
Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
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eiffel371-il | 50,000 | 9 | 19.9 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
eiffel371-il | 50,000 | 5 | 31.6 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
eiffel371-il | 100,000 | 9 | 47.9 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
eiffel371-il | 100,000 | 5 | 42.6 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
eiffel371-il | 200,000 | 9 | 56.2 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
eiffel371-il | 200,000 | 5 | 52 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
eiffel371-il | 500,000 | 9 | 70.1 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
eiffel371-il | 500,000 | 5 | 69.7 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
eiffel371-il | 1,000,000 | 9 | 89.5 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
eiffel371-il | 1,000,000 | 5 | 80.7 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
Reynolds number calculator |