Airfoil Comparison
Select airfoils from the airfoil database or add your own airfoils and compare the airfoil shape and lift/drag polars.
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(bqm34-il) RYAN BQM-34 FIREBEE WING AIRFOIL | Ryan BQM-34 Firebee wing airfoil (NACA 63-014A W/NACA 0014 nose and thinned to .09899 to account for sweep) Max thickness 9.9% at 32.5% chord Max camber 0% at 0% chord | Remove Airfoil details Airfoil plotter |
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Polars for (bqm34-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| bqm34-il | 50,000 | 9 | 27.1 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| bqm34-il | 50,000 | 5 | 26.5 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| bqm34-il | 100,000 | 9 | 38.4 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| bqm34-il | 100,000 | 5 | 34.9 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| bqm34-il | 200,000 | 9 | 48.2 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| bqm34-il | 200,000 | 5 | 42.4 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| bqm34-il | 500,000 | 9 | 56.7 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| bqm34-il | 500,000 | 5 | 58.3 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| bqm34-il | 1,000,000 | 9 | 70.8 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| bqm34-il | 1,000,000 | 5 | 72.3 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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