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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(a63a108c-il) NASA/AMES 63A108 MOD C AIRFOIL | NASA/AMES modification of the NACA 63A-108 airfoil Max thickness 7.7% at 30% chord Max camber 0.5% at 12.5% chord | Remove Airfoil details Airfoil plotter |
(joukowsk-il) 12% JOUKOWSKI AIRFOIL | 12% Joukowski airfoil Max thickness 11.8% at 25% chord Max camber 0% at 9.5% chord | Remove Airfoil details Airfoil plotter |
(e1212mod-il) EPPLER E1212MOD AIRFOIL | Eppler E1212 general aviation airfoil (as modified for use as Quickie wing airfoil) Max thickness 17.7% at 20.1% chord Max camber 2.6% at 35.1% 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 |
(lwk79100-il) LWK 79-100 | LWK 79-100 symmetrical airfoil Max thickness 10% at 27.9% chord Max camber 0% at 0% chord | Remove Airfoil details Airfoil plotter |
(ls421mod-il) NASA/LANGLEY LS(1)-0421MOD AIRFOIL | NASA/Langley LS(1)-0421MOD general aviation airfoil Max thickness 21% at 32.5% chord Max camber 2.3% at 30% chord | Remove Airfoil details Airfoil plotter |
(ls417mod-il) NASA/LANGLEY LS(1)-0417MOD AIRFOIL | NASA/Langley LS(1)-0417MOD general aviation airfoil Max thickness 17% at 30.2% chord Max camber 2.3% at 20.2% chord | Remove Airfoil details Airfoil plotter |
(l188root-il) LOCKHEED L-188 ROOT AIRFOIL | Lockheed L-188/P-3 root airfoil NACA 0014 -1.10 40/1.051 Cli=.3 a=.8 Max thickness 14% at 41.3% chord Max camber 2% at 51.7% chord | Remove Airfoil details Airfoil plotter |
(ls413mod-il) NASA/LANGLEY LS(1)-0413MOD AIRFOIL | NASA/Langley LS(1)-0413MOD general aviation airfoil Max thickness 13% at 35% chord Max camber 2.2% at 40% 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 |
(fx08s176-il) WORTMANN FX 08-S-176 AIRFOIL | Wortmann FX 08-S-176 airfoil Max thickness 17.6% at 37.1% chord Max camber 5.7% at 37.1% chord | Remove Airfoil details Airfoil plotter |
(fx082512-il) WORTMANN FX 082-512 AIRFOIL | Wortmann FX 082-512 airfoil Max thickness 11.8% at 25% chord Max camber 4.2% at 62.9% chord | Remove Airfoil details Airfoil plotter |
(fx601001-il) FX 60-100 (126) AIRFOIL | Wortmann FX 60-100 (126) airfoil Max thickness 10.1% at 30.8% chord Max camber 3.6% at 59.7% chord | Remove Airfoil details Airfoil plotter |
(fx049915-il) WORTMANN FX 049-915 AIRFOIL | Wortmann FX 049-915 airfoil Max thickness 14.7% at 37.1% chord Max camber 5.8% at 37.1% chord | Remove Airfoil details Airfoil plotter |
(p51droot-il) P-51D ROOT (BL17.5) AIRFOIL | P-51D root (BL17.5) airfoil Max thickness 16.5% at 38.9% chord Max camber 1.3% at 68.3% chord | Remove Airfoil details Airfoil plotter |
(fx057816-il) WORTMANN FX 057-816 | Wortmann FX 057-816 airfoil Max thickness 16.2% at 37.1% chord Max camber 5.1% at 37.1% chord | Remove Airfoil details Airfoil plotter |
Drawing Options
Polars for (a63a108c-il,joukowsk-il,e1212mod-il,whitcomb-il,lwk79100-il,ls421mod-il,ls417mod-il,l188root-il,ls413mod-il,bambino6-il,fx08s176-il,fx082512-il,fx601001-il,fx049915-il,p51droot-il,fx057816-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| a63a108c-il | 50,000 | 9 | 24.5 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| a63a108c-il | 50,000 | 5 | 22.8 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| a63a108c-il | 100,000 | 9 | 31.7 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| a63a108c-il | 100,000 | 5 | 31.2 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| a63a108c-il | 200,000 | 9 | 37.1 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| a63a108c-il | 200,000 | 5 | 41.8 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| a63a108c-il | 500,000 | 9 | 54.4 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| a63a108c-il | 500,000 | 5 | 58.8 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| a63a108c-il | 1,000,000 | 9 | 69.5 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| a63a108c-il | 1,000,000 | 5 | 72.7 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| joukowsk-il | 50,000 | 9 | 22.2 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| joukowsk-il | 50,000 | 5 | 26.4 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| joukowsk-il | 100,000 | 9 | 34.8 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| joukowsk-il | 100,000 | 5 | 37.2 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| joukowsk-il | 200,000 | 9 | 47.8 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| joukowsk-il | 200,000 | 5 | 48.7 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| joukowsk-il | 500,000 | 9 | 65.9 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| joukowsk-il | 500,000 | 5 | 65.6 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| joukowsk-il | 1,000,000 | 9 | 80.4 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| joukowsk-il | 1,000,000 | 5 | 79.4 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e1212mod-il | 50,000 | 9 | 5.8 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e1212mod-il | 50,000 | 5 | 20.8 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e1212mod-il | 100,000 | 9 | 28 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e1212mod-il | 100,000 | 5 | 39.7 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e1212mod-il | 200,000 | 9 | 51.6 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e1212mod-il | 200,000 | 5 | 57.6 at α=9° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e1212mod-il | 500,000 | 9 | 81.8 at α=8.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e1212mod-il | 500,000 | 5 | 84.2 at α=9.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e1212mod-il | 1,000,000 | 9 | 108.4 at α=9.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e1212mod-il | 1,000,000 | 5 | 107.6 at α=10° | 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 | |
| lwk79100-il | 50,000 | 9 | 25.9 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| lwk79100-il | 50,000 | 5 | 27.1 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| lwk79100-il | 100,000 | 9 | 37.4 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| lwk79100-il | 100,000 | 5 | 35.5 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| lwk79100-il | 200,000 | 9 | 47.7 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| lwk79100-il | 200,000 | 5 | 44.4 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| lwk79100-il | 500,000 | 9 | 59.5 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| lwk79100-il | 500,000 | 5 | 60.1 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| lwk79100-il | 1,000,000 | 9 | 72.6 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| lwk79100-il | 1,000,000 | 5 | 74.2 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ls421mod-il | 50,000 | 9 | 7.2 at α=0.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ls421mod-il | 50,000 | 5 | 18.6 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ls421mod-il | 100,000 | 9 | 37.2 at α=8.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ls421mod-il | 100,000 | 5 | 38.4 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ls421mod-il | 200,000 | 9 | 51.9 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ls421mod-il | 200,000 | 5 | 56 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ls421mod-il | 500,000 | 9 | 80.8 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ls421mod-il | 500,000 | 5 | 77.1 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ls421mod-il | 1,000,000 | 9 | 100 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ls421mod-il | 1,000,000 | 5 | 90.3 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ls417mod-il | 50,000 | 9 | 24.3 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ls417mod-il | 50,000 | 5 | 26.3 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ls417mod-il | 100,000 | 9 | 33.1 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ls417mod-il | 100,000 | 5 | 41.1 at α=9° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ls417mod-il | 200,000 | 9 | 52.5 at α=10.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ls417mod-il | 200,000 | 5 | 57.3 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ls417mod-il | 500,000 | 9 | 79.9 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ls417mod-il | 500,000 | 5 | 81.6 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ls417mod-il | 1,000,000 | 9 | 103 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ls417mod-il | 1,000,000 | 5 | 100.4 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| l188root-il | 50,000 | 9 | 32.4 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| l188root-il | 50,000 | 5 | 29.9 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| l188root-il | 100,000 | 9 | 51.1 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| l188root-il | 100,000 | 5 | 48.7 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| l188root-il | 200,000 | 9 | 72.5 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| l188root-il | 200,000 | 5 | 65.4 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| l188root-il | 500,000 | 9 | 94.9 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| l188root-il | 500,000 | 5 | 75.8 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| l188root-il | 1,000,000 | 9 | 104 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| l188root-il | 1,000,000 | 5 | 79.9 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ls413mod-il | 50,000 | 9 | 34.9 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ls413mod-il | 50,000 | 5 | 35.8 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ls413mod-il | 100,000 | 9 | 53.3 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ls413mod-il | 100,000 | 5 | 49.2 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ls413mod-il | 200,000 | 9 | 66 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ls413mod-il | 200,000 | 5 | 62 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ls413mod-il | 500,000 | 9 | 86.7 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ls413mod-il | 500,000 | 5 | 77.6 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ls413mod-il | 1,000,000 | 9 | 99.8 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ls413mod-il | 1,000,000 | 5 | 92.5 at α=6° | 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 | |
| fx08s176-il | 50,000 | 9 | 4.2 at α=13° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx08s176-il | 50,000 | 5 | 9.2 at α=-1.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx08s176-il | 100,000 | 9 | 5.1 at α=11.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx08s176-il | 100,000 | 5 | 20.4 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx08s176-il | 200,000 | 9 | 29.1 at α=12.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx08s176-il | 200,000 | 5 | 50.8 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx08s176-il | 500,000 | 9 | 108.8 at α=8.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx08s176-il | 500,000 | 5 | 106.8 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx08s176-il | 1,000,000 | 9 | 142 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx08s176-il | 1,000,000 | 5 | 139.3 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx082512-il | 50,000 | 9 | 31.2 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx082512-il | 50,000 | 5 | 33.4 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx082512-il | 100,000 | 9 | 46.6 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx082512-il | 100,000 | 5 | 47.7 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx082512-il | 200,000 | 9 | 63.6 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx082512-il | 200,000 | 5 | 60.2 at α=1.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx082512-il | 500,000 | 9 | 83.7 at α=0.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx082512-il | 500,000 | 5 | 75.3 at α=-0.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx082512-il | 1,000,000 | 9 | 99.1 at α=-0.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx082512-il | 1,000,000 | 5 | 82.1 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx601001-il | 50,000 | 9 | 38.3 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx601001-il | 50,000 | 5 | 42.5 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx601001-il | 100,000 | 9 | 61 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx601001-il | 100,000 | 5 | 62.5 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx601001-il | 200,000 | 9 | 84.2 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx601001-il | 200,000 | 5 | 76.8 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx601001-il | 500,000 | 9 | 103 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx601001-il | 500,000 | 5 | 92.4 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx601001-il | 1,000,000 | 9 | 116.1 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx601001-il | 1,000,000 | 5 | 101.4 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx049915-il | 50,000 | 9 | 4.9 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx049915-il | 50,000 | 5 | 10.4 at α=0.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx049915-il | 100,000 | 9 | 6.2 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx049915-il | 100,000 | 5 | 24.1 at α=1.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx049915-il | 200,000 | 9 | 25.4 at α=1.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx049915-il | 200,000 | 5 | 49.2 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx049915-il | 500,000 | 9 | 113.5 at α=10.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx049915-il | 500,000 | 5 | 114.6 at α=9.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx049915-il | 1,000,000 | 9 | 155 at α=9.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx049915-il | 1,000,000 | 5 | 152.6 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| p51droot-il | 50,000 | 9 | 28 at α=9.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| p51droot-il | 50,000 | 5 | 23.9 at α=9.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| p51droot-il | 100,000 | 9 | 46.2 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| p51droot-il | 100,000 | 5 | 43.4 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| p51droot-il | 200,000 | 9 | 62.4 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| p51droot-il | 200,000 | 5 | 57.6 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| p51droot-il | 500,000 | 9 | 81.3 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| p51droot-il | 500,000 | 5 | 71.7 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| p51droot-il | 1,000,000 | 9 | 92.5 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| p51droot-il | 1,000,000 | 5 | 79.5 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx057816-il | 50,000 | 9 | 5 at α=10.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx057816-il | 50,000 | 5 | 11.1 at α=15.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx057816-il | 100,000 | 9 | 17.8 at α=13.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx057816-il | 100,000 | 5 | 16.5 at α=13.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx057816-il | 200,000 | 9 | 27.6 at α=12.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx057816-il | 200,000 | 5 | 27.1 at α=11.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx057816-il | 500,000 | 9 | 113.8 at α=9.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx057816-il | 500,000 | 5 | 113.3 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx057816-il | 1,000,000 | 9 | 155.8 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx057816-il | 1,000,000 | 5 | 153 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| Reynolds number calculator | |||||||