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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(v13009-il) BOEING VERTOL V(1.95)3009-1.25 AIRFOIL | Boeing-Vertol V(1.9)3006-1.25 rotorcraft airfoil Max thickness 9% at 30.1% chord Max camber 1.3% at 20.1% chord | Remove Airfoil details Airfoil plotter |
(whitcomb-il) WHITCOMB INTEGRAL SUPERCRITICAL AIRFOIL | NASA/Langley Whitcomb integral supercritical airfoil Max thickness 11% at 35% chord Max camber 2.4% at 82.5% chord | Remove Airfoil details Airfoil plotter |
(v13006-il) BOEING VERTOL V13006-.7 AIRFOIL | Boeing-Vertol V13006-.7 rotorcraft airfoil Max thickness 6% at 30.2% chord Max camber 0.9% at 20.2% chord | Remove Airfoil details Airfoil plotter |
(n63415-il) NACA 63-415 AIRFOIL | NACA 63(2)-415 airfoil Max thickness 15% at 34.9% chord Max camber 2.2% at 50% chord | Remove Airfoil details Airfoil plotter |
(ys900-il) YS-900 | YS900 hyrdofoil (Shen / Eppler) Max thickness 9% at 52.5% chord Max camber 0% at 0% chord | Remove Airfoil details Airfoil plotter |
(naca0012h-sa) NACA0012H for VAWT from Sandia report SAND80-2114 | Modified Naca 0012 airfoil for Sandia VAWT tests Max thickness 12.2% at 22.5% chord Max camber 0% at 0% chord | Remove Airfoil details Airfoil plotter |
(n63412-il) NACA 63-412 AIRFOIL | NACA 63(1)-412 airfoil Max thickness 12% at 34.9% chord Max camber 2.2% at 50% chord | Remove Airfoil details Airfoil plotter |
(bambino6-il) Bambino 6 | Bambino 6 airfoil Max thickness 12% at 40% chord Max camber 2.8% at 40% chord | Remove Airfoil details Airfoil plotter |
(daytonwrightt1-il) Dayton-Wright T-1 | Dayton-Wright T-1 airfoil Max thickness 13.4% at 30% chord Max camber 4.4% at 40% chord | Remove Airfoil details Airfoil plotter |
(naca24112-jf) NACA 24112 | NACA 24112 5 digit reflex airfoil Max thickness 12% at 29.4% chord Max camber 1.7% at 20.6% chord | Remove Airfoil details Airfoil plotter |
(n63215-il) NACA 63-215 AIRFOIL | NACA 63(2)-215 airfoil Max thickness 15% at 34.9% chord Max camber 1.1% at 50% chord | Remove Airfoil details Airfoil plotter |
(n63212-il) NACA 63-212 AIRFOIL | NACA 63(1)-212 airfoil Max thickness 12% at 34.9% chord Max camber 1.1% at 55% chord | Remove Airfoil details Airfoil plotter |
(psu-90-125wl-il) PSU-90-125WL | PSU-90-125WL sailplane winglet airfoil Max thickness 12.5% at 35.1% chord Max camber 2% at 54.4% chord | Remove Airfoil details Airfoil plotter |
(usa25-il) USA 25 AIRFOIL | USA-25 airfoil Max thickness 8.3% at 19.9% chord Max camber 5.2% at 29.9% chord | Remove Airfoil details Airfoil plotter |
(n63215b-il) NACA 63(2)-215 MOD B | NACA-NASA/AMES/Hicks 63(2)-215 MOD B airfoil Max thickness 15% at 30% chord Max camber 1.5% at 10% chord | Remove Airfoil details Airfoil plotter |
(ag25-il) AG25 Bubble Dancer DLG by Mark Drela | Drela AG25 airfoil used on the Bubble Dancer R/C DLG Max thickness 7.6% at 24.7% chord Max camber 2.4% at 45.4% chord | Remove Airfoil details Airfoil plotter |
(n63210-il) NACA 63-210 AIRFOIL | NACA 63-210 airfoil Max thickness 10% at 35% chord Max camber 1.1% at 60% chord | Remove Airfoil details Airfoil plotter |
(trainer60-il) TRAINER60 | Great Planes R/C Trainer 60 airfoil Max thickness 18.3% at 27.1% chord Max camber 0.1% at 1.3% chord | Remove Airfoil details Airfoil plotter |
Drawing Options
Polars for (v13009-il,whitcomb-il,v13006-il,n63415-il,ys900-il,naca0012h-sa,n63412-il,bambino6-il,daytonwrightt1-il,naca24112-jf,n63215-il,n63212-il,psu-90-125wl-il,usa25-il,n63215b-il,ag25-il,n63210-il,trainer60-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| v13009-il | 50,000 | 9 | 26.2 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| v13009-il | 50,000 | 5 | 28.7 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| v13009-il | 100,000 | 9 | 36.6 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| v13009-il | 100,000 | 5 | 39.7 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| v13009-il | 200,000 | 9 | 49.7 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| v13009-il | 200,000 | 5 | 53.7 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| v13009-il | 500,000 | 9 | 72.9 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| v13009-il | 500,000 | 5 | 71.7 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| v13009-il | 1,000,000 | 9 | 88.4 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| v13009-il | 1,000,000 | 5 | 86.4 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| whitcomb-il | 50,000 | 9 | 22.1 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| whitcomb-il | 50,000 | 5 | 19.9 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| whitcomb-il | 100,000 | 9 | 22.9 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| whitcomb-il | 100,000 | 5 | 27.8 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| whitcomb-il | 200,000 | 9 | 30.1 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| whitcomb-il | 200,000 | 5 | 39.2 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| whitcomb-il | 500,000 | 9 | 49.1 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| whitcomb-il | 500,000 | 5 | 59.6 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| whitcomb-il | 1,000,000 | 9 | 69 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| whitcomb-il | 1,000,000 | 5 | 76.9 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| v13006-il | 50,000 | 9 | 27.9 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| v13006-il | 50,000 | 5 | 28.1 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| v13006-il | 100,000 | 9 | 37.7 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| v13006-il | 100,000 | 5 | 35.3 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| v13006-il | 200,000 | 9 | 46.3 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| v13006-il | 200,000 | 5 | 41.1 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| v13006-il | 500,000 | 9 | 54.7 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| v13006-il | 500,000 | 5 | 53.7 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| v13006-il | 1,000,000 | 9 | 62.4 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| v13006-il | 1,000,000 | 5 | 64.2 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n63415-il | 50,000 | 9 | 30 at α=9.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n63415-il | 50,000 | 5 | 27.8 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n63415-il | 100,000 | 9 | 53.1 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n63415-il | 100,000 | 5 | 52.3 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n63415-il | 200,000 | 9 | 75.6 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n63415-il | 200,000 | 5 | 70 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n63415-il | 500,000 | 9 | 100.9 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n63415-il | 500,000 | 5 | 90.7 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n63415-il | 1,000,000 | 9 | 118.7 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n63415-il | 1,000,000 | 5 | 103 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ys900-il | 50,000 | 9 | 17.3 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ys900-il | 50,000 | 5 | 17.4 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ys900-il | 100,000 | 9 | 21 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ys900-il | 100,000 | 5 | 21.8 at α=2° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ys900-il | 200,000 | 9 | 21.5 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ys900-il | 200,000 | 5 | 21.6 at α=2.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ys900-il | 500,000 | 9 | 24.2 at α=1.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ys900-il | 500,000 | 5 | 33.4 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ys900-il | 1,000,000 | 9 | 22.7 at α=2° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ys900-il | 1,000,000 | 5 | 49 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca0012h-sa | 50,000 | 9 | 20.3 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca0012h-sa | 50,000 | 5 | 22.8 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca0012h-sa | 100,000 | 9 | 28.2 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca0012h-sa | 100,000 | 5 | 33.5 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca0012h-sa | 200,000 | 9 | 41.5 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca0012h-sa | 200,000 | 5 | 46.6 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca0012h-sa | 500,000 | 9 | 63.7 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca0012h-sa | 500,000 | 5 | 66.2 at α=9.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca0012h-sa | 1,000,000 | 9 | 82 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca0012h-sa | 1,000,000 | 5 | 81.9 at α=9° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n63412-il | 50,000 | 9 | 36.1 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n63412-il | 50,000 | 5 | 36 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n63412-il | 100,000 | 9 | 56.6 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n63412-il | 100,000 | 5 | 54.8 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n63412-il | 200,000 | 9 | 77.2 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n63412-il | 200,000 | 5 | 70.6 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n63412-il | 500,000 | 9 | 99.8 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n63412-il | 500,000 | 5 | 88.1 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n63412-il | 1,000,000 | 9 | 115.7 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n63412-il | 1,000,000 | 5 | 98.7 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| bambino6-il | 50,000 | 9 | 32.7 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| bambino6-il | 50,000 | 5 | 30.2 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| bambino6-il | 100,000 | 9 | 43.5 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| bambino6-il | 100,000 | 5 | 36 at α=1.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| bambino6-il | 200,000 | 9 | 47.8 at α=1.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| bambino6-il | 200,000 | 5 | 36.2 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| bambino6-il | 500,000 | 9 | 54.6 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| bambino6-il | 500,000 | 5 | 39.4 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| bambino6-il | 1,000,000 | 9 | 73.5 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| bambino6-il | 1,000,000 | 5 | 53 at α=12° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| daytonwrightt1-il | 50,000 | 9 | 20.9 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| daytonwrightt1-il | 50,000 | 5 | 33.4 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| daytonwrightt1-il | 100,000 | 9 | 51.2 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| daytonwrightt1-il | 100,000 | 5 | 50.4 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| daytonwrightt1-il | 200,000 | 9 | 71.4 at α=2° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| daytonwrightt1-il | 200,000 | 5 | 65.7 at α=2° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| daytonwrightt1-il | 500,000 | 9 | 95.4 at α=1.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| daytonwrightt1-il | 500,000 | 5 | 84.5 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| daytonwrightt1-il | 1,000,000 | 9 | 109.9 at α=2° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| daytonwrightt1-il | 1,000,000 | 5 | 103.4 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca24112-jf | 50,000 | 9 | 19.9 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca24112-jf | 50,000 | 5 | 27.6 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca24112-jf | 100,000 | 9 | 37.3 at α=10.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca24112-jf | 100,000 | 5 | 43.5 at α=9° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca24112-jf | 200,000 | 9 | 57.7 at α=9.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca24112-jf | 200,000 | 5 | 60.4 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca24112-jf | 500,000 | 9 | 84.9 at α=8.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca24112-jf | 500,000 | 5 | 83 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca24112-jf | 1,000,000 | 9 | 105.5 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca24112-jf | 1,000,000 | 5 | 98.1 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n63215-il | 50,000 | 9 | 29.7 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n63215-il | 50,000 | 5 | 28.5 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n63215-il | 100,000 | 9 | 48.6 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n63215-il | 100,000 | 5 | 46.5 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n63215-il | 200,000 | 9 | 65.5 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n63215-il | 200,000 | 5 | 59.5 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n63215-il | 500,000 | 9 | 85.7 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n63215-il | 500,000 | 5 | 73.6 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n63215-il | 1,000,000 | 9 | 98.9 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n63215-il | 1,000,000 | 5 | 80.8 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n63212-il | 50,000 | 9 | 33.5 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n63212-il | 50,000 | 5 | 32.8 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n63212-il | 100,000 | 9 | 49.6 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n63212-il | 100,000 | 5 | 46.9 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n63212-il | 200,000 | 9 | 65.6 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n63212-il | 200,000 | 5 | 57.4 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n63212-il | 500,000 | 9 | 81.7 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n63212-il | 500,000 | 5 | 69.1 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n63212-il | 1,000,000 | 9 | 91.9 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n63212-il | 1,000,000 | 5 | 74.9 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| psu-90-125wl-il | 50,000 | 9 | 32.2 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| psu-90-125wl-il | 50,000 | 5 | 34.9 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| psu-90-125wl-il | 100,000 | 9 | 54.1 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| psu-90-125wl-il | 100,000 | 5 | 53.2 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| psu-90-125wl-il | 200,000 | 9 | 75.8 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| psu-90-125wl-il | 200,000 | 5 | 70.3 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| psu-90-125wl-il | 500,000 | 9 | 102.5 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| psu-90-125wl-il | 500,000 | 5 | 87.8 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| psu-90-125wl-il | 1,000,000 | 9 | 115.7 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| psu-90-125wl-il | 1,000,000 | 5 | 97.7 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| usa25-il | 50,000 | 9 | 25.6 at α=2.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| usa25-il | 50,000 | 5 | 35.9 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| usa25-il | 100,000 | 9 | 52.6 at α=9.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| usa25-il | 100,000 | 5 | 54.6 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| usa25-il | 200,000 | 9 | 74.1 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| usa25-il | 200,000 | 5 | 73 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| usa25-il | 500,000 | 9 | 102 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| usa25-il | 500,000 | 5 | 97.3 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| usa25-il | 1,000,000 | 9 | 124.6 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| usa25-il | 1,000,000 | 5 | 106.6 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n63215b-il | 50,000 | 9 | 25.9 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n63215b-il | 50,000 | 5 | 24.5 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n63215b-il | 100,000 | 9 | 32.8 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n63215b-il | 100,000 | 5 | 35.3 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n63215b-il | 200,000 | 9 | 44.4 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n63215b-il | 200,000 | 5 | 47.9 at α=8.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n63215b-il | 500,000 | 9 | 66.4 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n63215b-il | 500,000 | 5 | 68.3 at α=9.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n63215b-il | 1,000,000 | 9 | 86.3 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n63215b-il | 1,000,000 | 5 | 83.9 at α=10° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ag25-il | 50,000 | 9 | 35.9 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ag25-il | 50,000 | 5 | 38.9 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ag25-il | 100,000 | 9 | 53.6 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ag25-il | 100,000 | 5 | 53.1 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ag25-il | 200,000 | 9 | 70.9 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ag25-il | 200,000 | 5 | 66.6 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ag25-il | 500,000 | 9 | 92.1 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ag25-il | 500,000 | 5 | 84 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ag25-il | 1,000,000 | 9 | 106.5 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ag25-il | 1,000,000 | 5 | 97 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n63210-il | 50,000 | 9 | 33.5 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n63210-il | 50,000 | 5 | 32 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n63210-il | 100,000 | 9 | 46.7 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n63210-il | 100,000 | 5 | 42.8 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n63210-il | 200,000 | 9 | 59.4 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n63210-il | 200,000 | 5 | 48.7 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n63210-il | 500,000 | 9 | 67.7 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n63210-il | 500,000 | 5 | 55.8 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n63210-il | 1,000,000 | 9 | 69 at α=2° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n63210-il | 1,000,000 | 5 | 66.3 at α=11° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| trainer60-il | 50,000 | 9 | 15.3 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| trainer60-il | 50,000 | 5 | 24.5 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| trainer60-il | 100,000 | 9 | 36.7 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| trainer60-il | 100,000 | 5 | 38.8 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| trainer60-il | 200,000 | 9 | 51.7 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| trainer60-il | 200,000 | 5 | 50.9 at α=9.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| trainer60-il | 500,000 | 9 | 73.1 at α=10° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| trainer60-il | 500,000 | 5 | 65.8 at α=8.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| trainer60-il | 1,000,000 | 9 | 85.4 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| trainer60-il | 1,000,000 | 5 | 79.3 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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