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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(marske7-il) RONCZ LOW DRAG FLYING WING AIRFOIL | Roncz/Marske-7 low drag flying wing airfoil Max thickness 12.1% at 42.8% chord Max camber 2.8% at 39.1% chord | Remove Airfoil details Airfoil plotter |
(s813-nr) NREL's S813 Airfoil | NREL HAWT airfoil S813 tip Max thickness 16% at 40.4% chord Max camber 2.3% at 54.4% chord | Remove Airfoil details Airfoil plotter |
(hq3014-il) HQ 3.0/14 AIRFOIL | Quabeck HQ 3.0/14 R/C sailplane airfoil Max thickness 14% at 35% chord Max camber 3% at 50% chord | Remove Airfoil details Airfoil plotter |
(s819-nr) NREL's S819 Airfoil | NREL HAWT airfoil S819 primary 21.0% Dia=10 to 20 m Re=1.0E+6 Clmax(S)=1.20 Clmax(R)=1.16 Restrained max lift coef Max thickness 21.1% at 28.4% chord Max camber 1.3% at 77.3% chord | Remove Airfoil details Airfoil plotter |
(s821-nr) NREL's S821 Airfoil | NREL HAWT airfoil S821 root 24.0% Dia=10 to 20 m Re=8.0E+5 Clmax(S)=1.40 Clmax(R)=1.35 Restrained max lift coef Max thickness 24.2% at 24.6% chord Max camber 2.6% at 77.6% chord | Remove Airfoil details Airfoil plotter |
(s834-nr) NREL's S834 Airfoil | NREL HAWT airfoil S834 tip 15.0% Dia=1 to 3 m Re=4.0E+5 Clmax(S)=1.00 Clmax(R)=1.02 High max lift coef Max thickness 15% at 39.5% chord Max camber 1.6% at 60% chord | Remove Airfoil details Airfoil plotter |
(s832-nr) NREL's S832 Airfoil | NREL HAWT airfoil S832 Max thickness 14.9% at 44% chord Max camber 5.3% at 44% chord | Remove Airfoil details Airfoil plotter |
(arad6-il) ARA-D 6% AIRFOIL | Aeronautical Research Association/Bocci-Dowty Rotol ARA-D 6% thick propeller airfoil Max thickness 6% at 20% chord Max camber 5% at 45% chord | Remove Airfoil details Airfoil plotter |
(m7-il) NACA M7 AIRFOIL | NACA/Munk M-7 airfoil Max thickness 6.2% at 40% chord Max camber 4.9% at 30% chord | Remove Airfoil details Airfoil plotter |
(s812-nr) NREL's S812 Airfoil | NREL HAWT airfoil S812 primary Max thickness 21% at 39.6% chord Max camber 1.6% at 77% chord | Remove Airfoil details Airfoil plotter |
(apex16-il) Apex 16 (normalized using XFOIL date021206) | Drela Apex 16 low Reynolds number transonic research airfoil Max thickness 12.9% at 38.6% chord Max camber 2.4% at 59.6% chord | Remove Airfoil details Airfoil plotter |
(s6061-il) S6061 9% | Selig S6061 low Reynolds number airfoil Max thickness 9% at 34% chord Max camber 1.5% at 43.6% chord | Remove Airfoil details Airfoil plotter |
(s817-nr) NREL's S817 Airfoil | NREL HAWT airfoil S817 tip 16.0% Dia=30 to 50 m Re=3.0E+6 Clmax(S)=1.10 Clmax(R)=1.08 Restrained max lift coef Max thickness 16% at 51.1% chord Max camber 2.8% at 41.1% chord | Remove Airfoil details Airfoil plotter |
(e67-il) EPPLER 67 AIRFOIL | Eppler E67 low Reynolds number airfoil Max thickness 11.6% at 32.6% chord Max camber 3.7% at 51.6% chord | Remove Airfoil details Airfoil plotter |
(hq3513-il) HQ 3.5/13 AIRFOIL | Quabeck HQ 3.5/13 R/C sailplane airfoil Max thickness 13% at 35% chord Max camber 3.5% at 50% chord | Remove Airfoil details Airfoil plotter |
(marske4-il) MARSKE PIONEER IID TIP AIRFOIL (NACA 431012A*.833 HYBRID) | Marske Pioneer IID tip airfoil (NACA 43012A*.833 hybrid) Max thickness 10.2% at 20% chord Max camber 2.8% at 15% chord | Remove Airfoil details Airfoil plotter |
Drawing Options
Polars for (marske7-il,s813-nr,hq3014-il,s819-nr,s821-nr,s834-nr,s832-nr,arad6-il,m7-il,s812-nr,apex16-il,s6061-il,s817-nr,e67-il,hq3513-il,marske4-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| marske7-il | 50,000 | 9 | 27.4 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| marske7-il | 50,000 | 5 | 24 at α=8.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| marske7-il | 100,000 | 9 | 43.2 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| marske7-il | 100,000 | 5 | 43.2 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| marske7-il | 200,000 | 9 | 72 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| marske7-il | 200,000 | 5 | 67.9 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| marske7-il | 500,000 | 9 | 103.7 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| marske7-il | 500,000 | 5 | 90.8 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| marske7-il | 1,000,000 | 9 | 120.8 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| marske7-il | 1,000,000 | 5 | 96.1 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s813-nr | 50,000 | 9 | 23.5 at α=10° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s813-nr | 50,000 | 5 | 20.4 at α=10° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s813-nr | 100,000 | 9 | 35.2 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s813-nr | 100,000 | 5 | 34.4 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s813-nr | 200,000 | 9 | 64.8 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s813-nr | 200,000 | 5 | 65.3 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s813-nr | 500,000 | 9 | 104.6 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s813-nr | 500,000 | 5 | 96.3 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s813-nr | 1,000,000 | 9 | 130.8 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s813-nr | 1,000,000 | 5 | 115.3 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hq3014-il | 50,000 | 9 | 30.1 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hq3014-il | 50,000 | 5 | 33 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hq3014-il | 100,000 | 9 | 54.2 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hq3014-il | 100,000 | 5 | 53.4 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hq3014-il | 200,000 | 9 | 77.5 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hq3014-il | 200,000 | 5 | 70.9 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hq3014-il | 500,000 | 9 | 99.8 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hq3014-il | 500,000 | 5 | 85.4 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hq3014-il | 1,000,000 | 9 | 113.7 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hq3014-il | 1,000,000 | 5 | 96.9 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s819-nr | 50,000 | 9 | 7.9 at α=0.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s819-nr | 50,000 | 5 | 22.6 at α=9.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s819-nr | 100,000 | 9 | 38.4 at α=10.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s819-nr | 100,000 | 5 | 40.4 at α=8.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s819-nr | 200,000 | 9 | 55.6 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s819-nr | 200,000 | 5 | 54.8 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s819-nr | 500,000 | 9 | 77.6 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s819-nr | 500,000 | 5 | 72.5 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s819-nr | 1,000,000 | 9 | 93.4 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s819-nr | 1,000,000 | 5 | 84.1 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s821-nr | 50,000 | 9 | 4.8 at α=11.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s821-nr | 50,000 | 5 | 19.4 at α=9.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s821-nr | 100,000 | 9 | 35.6 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s821-nr | 100,000 | 5 | 37.4 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s821-nr | 200,000 | 9 | 52.8 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s821-nr | 200,000 | 5 | 51.1 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s821-nr | 500,000 | 9 | 72.8 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s821-nr | 500,000 | 5 | 66 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s821-nr | 1,000,000 | 9 | 87.5 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s821-nr | 1,000,000 | 5 | 75.6 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s834-nr | 50,000 | 9 | 29.8 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s834-nr | 50,000 | 5 | 26.6 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s834-nr | 100,000 | 9 | 47.4 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s834-nr | 100,000 | 5 | 44.7 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s834-nr | 200,000 | 9 | 70.6 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s834-nr | 200,000 | 5 | 55.5 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s834-nr | 500,000 | 9 | 81.2 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s834-nr | 500,000 | 5 | 74.4 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s834-nr | 1,000,000 | 9 | 102.7 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s834-nr | 1,000,000 | 5 | 83.5 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s832-nr | 50,000 | 9 | 19.8 at α=13.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s832-nr | 50,000 | 5 | 16 at α=13.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s832-nr | 100,000 | 9 | 26.4 at α=12.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s832-nr | 100,000 | 5 | 25.2 at α=11.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s832-nr | 200,000 | 9 | 54.7 at α=9.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s832-nr | 200,000 | 5 | 67.2 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s832-nr | 500,000 | 9 | 126 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s832-nr | 500,000 | 5 | 118.9 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s832-nr | 1,000,000 | 9 | 163.3 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s832-nr | 1,000,000 | 5 | 151.2 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| arad6-il | 50,000 | 9 | 46 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| arad6-il | 50,000 | 5 | 45.8 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| arad6-il | 100,000 | 9 | 68.9 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| arad6-il | 100,000 | 5 | 66.6 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| arad6-il | 200,000 | 9 | 93 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| arad6-il | 200,000 | 5 | 86 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| arad6-il | 500,000 | 9 | 122.5 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| arad6-il | 500,000 | 5 | 105.6 at α=1.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| arad6-il | 1,000,000 | 9 | 139.7 at α=2° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| arad6-il | 1,000,000 | 5 | 106 at α=2.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| m7-il | 50,000 | 9 | 34.2 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| m7-il | 50,000 | 5 | 36 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| m7-il | 100,000 | 9 | 50.3 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| m7-il | 100,000 | 5 | 54.1 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| m7-il | 200,000 | 9 | 63.5 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| m7-il | 200,000 | 5 | 68.2 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| m7-il | 500,000 | 9 | 73.1 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| m7-il | 500,000 | 5 | 75.1 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| m7-il | 1,000,000 | 9 | 73 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| m7-il | 1,000,000 | 5 | 84 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s812-nr | 50,000 | 9 | 17.4 at α=13.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s812-nr | 50,000 | 5 | 14.2 at α=11.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s812-nr | 100,000 | 9 | 23.9 at α=11° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s812-nr | 100,000 | 5 | 25.8 at α=10° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s812-nr | 200,000 | 9 | 56.2 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s812-nr | 200,000 | 5 | 59.6 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s812-nr | 500,000 | 9 | 92.4 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s812-nr | 500,000 | 5 | 87.4 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s812-nr | 1,000,000 | 9 | 116.5 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s812-nr | 1,000,000 | 5 | 105.2 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| apex16-il | 50,000 | 9 | 34 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| apex16-il | 50,000 | 5 | 32.6 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| apex16-il | 100,000 | 9 | 56.1 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| apex16-il | 100,000 | 5 | 54.4 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| apex16-il | 200,000 | 9 | 81.4 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| apex16-il | 200,000 | 5 | 76.8 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| apex16-il | 500,000 | 9 | 112.6 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| apex16-il | 500,000 | 5 | 92.3 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| apex16-il | 1,000,000 | 9 | 123.6 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| apex16-il | 1,000,000 | 5 | 99.4 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s6061-il | 50,000 | 9 | 34.1 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s6061-il | 50,000 | 5 | 35.9 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s6061-il | 100,000 | 9 | 51.2 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s6061-il | 100,000 | 5 | 50.1 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s6061-il | 200,000 | 9 | 68.2 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s6061-il | 200,000 | 5 | 63.3 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s6061-il | 500,000 | 9 | 88.8 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s6061-il | 500,000 | 5 | 77.3 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s6061-il | 1,000,000 | 9 | 102 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s6061-il | 1,000,000 | 5 | 81.7 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s817-nr | 50,000 | 9 | 21.5 at α=11° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s817-nr | 50,000 | 5 | 17.9 at α=10.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s817-nr | 100,000 | 9 | 25.9 at α=9.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s817-nr | 100,000 | 5 | 26.6 at α=9.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s817-nr | 200,000 | 9 | 45.3 at α=8.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s817-nr | 200,000 | 5 | 53 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s817-nr | 500,000 | 9 | 105.3 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s817-nr | 500,000 | 5 | 101.1 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s817-nr | 1,000,000 | 9 | 137.3 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s817-nr | 1,000,000 | 5 | 126 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e67-il | 50,000 | 9 | 37.4 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e67-il | 50,000 | 5 | 36.9 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e67-il | 100,000 | 9 | 60.9 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e67-il | 100,000 | 5 | 60.3 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e67-il | 200,000 | 9 | 86.8 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e67-il | 200,000 | 5 | 82.6 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e67-il | 500,000 | 9 | 121.3 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e67-il | 500,000 | 5 | 107.5 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e67-il | 1,000,000 | 9 | 144.7 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e67-il | 1,000,000 | 5 | 117.9 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hq3513-il | 50,000 | 9 | 30.2 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hq3513-il | 50,000 | 5 | 35.3 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hq3513-il | 100,000 | 9 | 56.9 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hq3513-il | 100,000 | 5 | 56 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hq3513-il | 200,000 | 9 | 81.6 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hq3513-il | 200,000 | 5 | 75.3 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hq3513-il | 500,000 | 9 | 105.6 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hq3513-il | 500,000 | 5 | 88.7 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hq3513-il | 1,000,000 | 9 | 119.4 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hq3513-il | 1,000,000 | 5 | 101.5 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| marske4-il | 50,000 | 9 | 17 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| marske4-il | 50,000 | 5 | 22.3 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| marske4-il | 100,000 | 9 | 24.8 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| marske4-il | 100,000 | 5 | 34.1 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| marske4-il | 200,000 | 9 | 39.5 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| marske4-il | 200,000 | 5 | 50.4 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| marske4-il | 500,000 | 9 | 73.9 at α=11.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| marske4-il | 500,000 | 5 | 78.9 at α=9.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| marske4-il | 1,000,000 | 9 | 100.6 at α=10.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| marske4-il | 1,000,000 | 5 | 98.6 at α=9.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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