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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(lwk80100-il) LWK 80-100 | LWK 80-100 symmetrical airfoil Max thickness 10.1% at 40.2% chord Max camber 0% at 0% chord | Remove Airfoil details Airfoil plotter |
(goe386-il) GOE 386 AIRFOIL | Gottingen 386 airfoil Max thickness 20.3% at 29% chord Max camber 5.4% at 39% chord | Remove Airfoil details Airfoil plotter |
(goe358-il) GOE 358 AIRFOIL | Gottingen 358 airfoil Max thickness 10.9% at 20% chord Max camber 5.6% at 50% chord | Remove Airfoil details Airfoil plotter |
(goe383-il) GOE 383 AIRFOIL | Gottingen 383 airfoil Max thickness 20.2% at 28.7% chord Max camber 5% at 38.7% chord | Remove Airfoil details Airfoil plotter |
(naca747a315-il) NACA 747A315 | NACA 747A315 airfoil Max thickness 15% at 40.2% chord Max camber 2.5% at 35% chord | Remove Airfoil details Airfoil plotter |
(rc510-il) NASA RC(5)-10 AIRFOIL | NASA/Langley RC(5)-10 rotorcraft airfoil Max thickness 10% at 40.1% chord Max camber 2.2% at 25.3% chord | Remove Airfoil details Airfoil plotter |
(goe244-il) GOE 244 (MVA PR.4) AIRFOIL | Gottingen 244 (MVA PR.4) airfoil Max thickness 17.7% at 19.6% chord Max camber 10% at 49.6% chord | Remove Airfoil details Airfoil plotter |
(e195-il) E195 (11.82%) | Eppler E195 low Reynolds number airfoil Max thickness 11.8% at 35% chord Max camber 2.7% at 44.2% chord | Remove Airfoil details Airfoil plotter |
(sc1095-il) SIKORSKY SC1095 AIRFOIL | Sikorsky/Balch SC1095 rotorcraft airfoil Max thickness 9.5% at 26.9% chord Max camber 0.8% at 26.9% chord | Remove Airfoil details Airfoil plotter |
(goe546-il) GOE 546 AIRFOIL | Gottingen 546 airfoil Max thickness 10.4% at 30% chord Max camber 3.6% at 50% chord | Remove Airfoil details Airfoil plotter |
(goe243-il) GOE 243 (MVA PR.3) AIRFOIL | Gottingen 243 (MVA PR.3) airfoil Max thickness 19% at 29.3% chord Max camber 8.4% at 59.4% chord | Remove Airfoil details Airfoil plotter |
(sg6041-il) SG6041 | Selig / Giguere SG6041 wind turbine airfoil (high L/D) Max thickness 10% at 34.9% chord Max camber 1.6% at 49.7% chord | Remove Airfoil details Airfoil plotter |
(goe279-il) GOE 279 (DAIMLER X) AIRFOIL | Gottingen 279 (DAIMLER X) airfoil Max thickness 7.4% at 30% chord Max camber 4.7% at 40% chord | Remove Airfoil details Airfoil plotter |
(nlf1015-il) NASA NLF1015 | NASA/Langley/Somers-Maughmer NLF(1)-1015 natural laminar flow airfoil Max thickness 15% at 39.8% chord Max camber 4.3% at 62.8% chord | Remove Airfoil details Airfoil plotter |
(naca653618-il) NACA 65(3)-618 | NACA 65(3)-618 airfoil Max thickness 18% at 39.8% chord Max camber 3.3% at 50% chord | Remove Airfoil details Airfoil plotter |
(goe571-il) GOE 571 AIRFOIL | Gottingen 571 airfoil Max thickness 24.9% at 29.4% chord Max camber 9.8% at 29.4% chord | Remove Airfoil details Airfoil plotter |
(sm701-il) SM701 | Somers / Maughmer SM701 airfoil Max thickness 16% at 36.3% chord Max camber 3% at 60.3% chord | Remove Airfoil details Airfoil plotter |
Drawing Options
Polars for (lwk80100-il,goe386-il,goe358-il,goe383-il,naca747a315-il,rc510-il,goe244-il,e195-il,sc1095-il,goe546-il,goe243-il,sg6041-il,goe279-il,nlf1015-il,naca653618-il,goe571-il,sm701-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| lwk80100-il | 50,000 | 9 | 26.2 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| lwk80100-il | 50,000 | 5 | 26.4 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| lwk80100-il | 100,000 | 9 | 59.4 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| lwk80100-il | 100,000 | 5 | 31.9 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| lwk80100-il | 200,000 | 9 | 44 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| lwk80100-il | 200,000 | 5 | 38.3 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| lwk80100-il | 500,000 | 9 | 49 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| lwk80100-il | 500,000 | 5 | 51.1 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| lwk80100-il | 1,000,000 | 9 | 60.5 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| lwk80100-il | 1,000,000 | 5 | 61.4 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe386-il | 50,000 | 9 | 3.4 at α=8.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe386-il | 50,000 | 5 | 16.2 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe386-il | 100,000 | 9 | 33.2 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe386-il | 100,000 | 5 | 40.8 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe386-il | 200,000 | 9 | 61.7 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe386-il | 200,000 | 5 | 59.9 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe386-il | 500,000 | 9 | 88.7 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe386-il | 500,000 | 5 | 76.6 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe386-il | 1,000,000 | 9 | 103.6 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe386-il | 1,000,000 | 5 | 94 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe358-il | 50,000 | 9 | 37.5 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe358-il | 50,000 | 5 | 42.2 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe358-il | 100,000 | 9 | 58.5 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe358-il | 100,000 | 5 | 61.8 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe358-il | 200,000 | 9 | 79 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe358-il | 200,000 | 5 | 79 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe358-il | 500,000 | 9 | 105.7 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe358-il | 500,000 | 5 | 99.2 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe358-il | 1,000,000 | 9 | 119.2 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe358-il | 1,000,000 | 5 | 115.3 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe383-il | 50,000 | 9 | 3.6 at α=11.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe383-il | 50,000 | 5 | 13.9 at α=0.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe383-il | 100,000 | 9 | 25 at α=1.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe383-il | 100,000 | 5 | 40.5 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe383-il | 200,000 | 9 | 62.2 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe383-il | 200,000 | 5 | 60.4 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe383-il | 500,000 | 9 | 88.4 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe383-il | 500,000 | 5 | 83.1 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe383-il | 1,000,000 | 9 | 111.7 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe383-il | 1,000,000 | 5 | 106.1 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca747a315-il | 50,000 | 9 | 20.2 at α=10.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca747a315-il | 50,000 | 5 | 17.3 at α=2° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca747a315-il | 100,000 | 9 | 44.4 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca747a315-il | 100,000 | 5 | 46.4 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca747a315-il | 200,000 | 9 | 72 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca747a315-il | 200,000 | 5 | 61.6 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca747a315-il | 500,000 | 9 | 89.8 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca747a315-il | 500,000 | 5 | 85.1 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca747a315-il | 1,000,000 | 9 | 111.5 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca747a315-il | 1,000,000 | 5 | 100.3 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rc510-il | 50,000 | 9 | 31.6 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rc510-il | 50,000 | 5 | 32.2 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rc510-il | 100,000 | 9 | 46.6 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rc510-il | 100,000 | 5 | 43.5 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rc510-il | 200,000 | 9 | 60.8 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rc510-il | 200,000 | 5 | 54.8 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rc510-il | 500,000 | 9 | 76.3 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rc510-il | 500,000 | 5 | 75.7 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rc510-il | 1,000,000 | 9 | 94.4 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rc510-il | 1,000,000 | 5 | 92.4 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe244-il | 50,000 | 9 | 7.9 at α=0.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe244-il | 50,000 | 5 | 25 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe244-il | 100,000 | 9 | 50.1 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe244-il | 100,000 | 5 | 47.8 at α=0.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe244-il | 200,000 | 9 | 73.3 at α=0.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe244-il | 200,000 | 5 | 64.3 at α=0.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe244-il | 500,000 | 9 | 92.3 at α=-0.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe244-il | 500,000 | 5 | 79.5 at α=1.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe244-il | 1,000,000 | 9 | 105.6 at α=1.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe244-il | 1,000,000 | 5 | 98.8 at α=2.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e195-il | 50,000 | 9 | 32.8 at α=9.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e195-il | 50,000 | 5 | 31.8 at α=8.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e195-il | 100,000 | 9 | 55.9 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e195-il | 100,000 | 5 | 56.3 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e195-il | 200,000 | 9 | 80.1 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e195-il | 200,000 | 5 | 78.2 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e195-il | 500,000 | 9 | 112.4 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e195-il | 500,000 | 5 | 105.2 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e195-il | 1,000,000 | 9 | 137.1 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e195-il | 1,000,000 | 5 | 124.2 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sc1095-il | 50,000 | 9 | 25.3 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sc1095-il | 50,000 | 5 | 26.6 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sc1095-il | 100,000 | 9 | 34.2 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sc1095-il | 100,000 | 5 | 36.4 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sc1095-il | 200,000 | 9 | 45.3 at α=11° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sc1095-il | 200,000 | 5 | 48.8 at α=10° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sc1095-il | 500,000 | 9 | 69.5 at α=10° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sc1095-il | 500,000 | 5 | 70.2 at α=8.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sc1095-il | 1,000,000 | 9 | 87 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sc1095-il | 1,000,000 | 5 | 85.6 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe546-il | 50,000 | 9 | 38.4 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe546-il | 50,000 | 5 | 38.6 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe546-il | 100,000 | 9 | 59.4 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe546-il | 100,000 | 5 | 58.6 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe546-il | 200,000 | 9 | 80.5 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe546-il | 200,000 | 5 | 76.2 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe546-il | 500,000 | 9 | 106.7 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe546-il | 500,000 | 5 | 93.5 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe546-il | 1,000,000 | 9 | 124.7 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe546-il | 1,000,000 | 5 | 101.7 at α=2.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe243-il | 50,000 | 9 | 5.7 at α=-0.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe243-il | 50,000 | 5 | 17.9 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe243-il | 100,000 | 9 | 44.6 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe243-il | 100,000 | 5 | 49.4 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe243-il | 200,000 | 9 | 70.4 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe243-il | 200,000 | 5 | 69.4 at α=2.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe243-il | 500,000 | 9 | 99.1 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe243-il | 500,000 | 5 | 90.3 at α=2.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe243-il | 1,000,000 | 9 | 119.1 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe243-il | 1,000,000 | 5 | 107.9 at α=2.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sg6041-il | 50,000 | 9 | 35.4 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sg6041-il | 50,000 | 5 | 35.1 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sg6041-il | 100,000 | 9 | 53.5 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sg6041-il | 100,000 | 5 | 49.8 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sg6041-il | 200,000 | 9 | 72.8 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sg6041-il | 200,000 | 5 | 63.9 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sg6041-il | 500,000 | 9 | 91.5 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sg6041-il | 500,000 | 5 | 74.2 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sg6041-il | 1,000,000 | 9 | 96.5 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sg6041-il | 1,000,000 | 5 | 88 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe279-il | 50,000 | 9 | 37.6 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe279-il | 50,000 | 5 | 42.3 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe279-il | 100,000 | 9 | 58.3 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe279-il | 100,000 | 5 | 59 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe279-il | 200,000 | 9 | 77.4 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe279-il | 200,000 | 5 | 73.5 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe279-il | 500,000 | 9 | 96.9 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe279-il | 500,000 | 5 | 93 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe279-il | 1,000,000 | 9 | 113.9 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe279-il | 1,000,000 | 5 | 105 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| nlf1015-il | 50,000 | 9 | 25.8 at α=11.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| nlf1015-il | 50,000 | 5 | 21.9 at α=11.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| nlf1015-il | 100,000 | 9 | 40.7 at α=10.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| nlf1015-il | 100,000 | 5 | 38.6 at α=9.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| nlf1015-il | 200,000 | 9 | 75.6 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| nlf1015-il | 200,000 | 5 | 77.2 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| nlf1015-il | 500,000 | 9 | 130.6 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| nlf1015-il | 500,000 | 5 | 125.9 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| nlf1015-il | 1,000,000 | 9 | 167.7 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| nlf1015-il | 1,000,000 | 5 | 154.6 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca653618-il | 50,000 | 9 | 17.8 at α=12.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca653618-il | 50,000 | 5 | 15.3 at α=12.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca653618-il | 100,000 | 9 | 27.8 at α=11° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca653618-il | 100,000 | 5 | 29 at α=10.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca653618-il | 200,000 | 9 | 67.7 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca653618-il | 200,000 | 5 | 70.2 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca653618-il | 500,000 | 9 | 110.3 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca653618-il | 500,000 | 5 | 105.2 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca653618-il | 1,000,000 | 9 | 138.3 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca653618-il | 1,000,000 | 5 | 128.4 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe571-il | 50,000 | 9 | 3.7 at α=-12° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe571-il | 50,000 | 5 | 5.7 at α=-7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe571-il | 100,000 | 9 | 8.1 at α=-8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe571-il | 100,000 | 5 | 8.6 at α=0.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe571-il | 200,000 | 9 | 33.1 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe571-il | 200,000 | 5 | 34 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe571-il | 500,000 | 9 | 56.1 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe571-il | 500,000 | 5 | 42.8 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe571-il | 1,000,000 | 9 | 62.8 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe571-il | 1,000,000 | 5 | 52.5 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sm701-il | 50,000 | 9 | 27 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sm701-il | 50,000 | 5 | 30.5 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sm701-il | 100,000 | 9 | 50.8 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sm701-il | 100,000 | 5 | 46.8 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sm701-il | 200,000 | 9 | 68.6 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sm701-il | 200,000 | 5 | 64.4 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sm701-il | 500,000 | 9 | 95.9 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sm701-il | 500,000 | 5 | 79.6 at α=2° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sm701-il | 1,000,000 | 9 | 110.9 at α=2.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sm701-il | 1,000,000 | 5 | 93.6 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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