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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(n12-il) N-12 | N-12 airfoil Max thickness 10.5% at 30% chord Max camber 0.2% at 15% chord | Remove Airfoil details Airfoil plotter |
(ht08-il) HT08 | Drela HT08 airfoil Max thickness 5% at 20.2% chord Max camber 0% at 0% chord | Remove Airfoil details Airfoil plotter |
(e1200-il) EPPLER 1200 AIRFOIL | Eppler E1200 general aviation airfoil Max thickness 16.9% at 36.1% chord Max camber 3.5% at 50.2% chord | Remove Airfoil details Airfoil plotter |
(e184-il) E184 (8.33%) | Eppler E184 low Reynolds number airfoil Max thickness 8.3% at 33.3% chord Max camber 0.8% at 38.3% chord | Remove Airfoil details Airfoil plotter |
(la5055-il) LIEBECK LA5055 AIRFOIL | Liebeck high lift airfoil Max thickness 15.9% at 35% chord Max camber 5.9% at 40% chord | Remove Airfoil details Airfoil plotter |
(wb13535sm-il) WB-135/35 13.5% smoothed | Woody Blanchard WB135/35 R/C sailplane airfoil Max thickness 13.6% at 25% chord Max camber 3.8% at 50% chord | Remove Airfoil details Airfoil plotter |
(ag09-il) AG09 | Drela AG09 airfoil Max thickness 4.9% at 17.4% chord Max camber 1.8% at 34.1% chord | Remove Airfoil details Airfoil plotter |
(e178-il) E178 (8.69%) | Eppler E178 low Reynolds number airfoil Max thickness 8.7% at 29.8% chord Max camber 2.8% at 38.8% chord | Remove Airfoil details Airfoil plotter |
(n24-il) N-24 | N-24 airfoil Max thickness 17% at 30% chord Max camber 5.4% at 40% chord | Remove Airfoil details Airfoil plotter |
(hq158-il) HQ 1.5/8 AIRFOIL | Quabeck HQ 1.5/8 R/C sailplane airfoil Max thickness 8% at 32.5% chord Max camber 1.5% at 50% chord | Remove Airfoil details Airfoil plotter |
(n13-il) N-13 | N-13 airfoil Max thickness 11.8% at 30% chord Max camber 0.1% at 95% chord | Remove Airfoil details Airfoil plotter |
(hq1012-il) HQ 1.0/12 AIRFOIL | Quabeck HQ 1.0/12 R/C sailplane airfoil Max thickness 12% at 35% chord Max camber 1% at 50% chord | Remove Airfoil details Airfoil plotter |
(s102b-il) SOMERS S102 AIRFOIL (BLUNT) | Dan Somers airfoil for the Toyota general aviation airplane Max thickness 15% at 40% chord Max camber 2% at 68.7% chord | Remove Airfoil details Airfoil plotter |
(k2-il) GRUMMAN K-2 AIRFOIL | Grumman K-2 transonic airfoil (GAC .80-.53-10.3) Max thickness 10.3% at 38.9% chord Max camber 1.3% at 88.3% chord | Remove Airfoil details Airfoil plotter |
(ht12-il) HT12 | Drela HT12 airfoil Max thickness 5% at 18.6% chord Max camber 0% at 0% chord | Remove Airfoil details Airfoil plotter |
(tsagi8-il) TSAGI 8% AIRFOIL | TSAGI 8% airfoil Max thickness 8% at 30% chord Max camber 1.3% at 30% chord | Remove Airfoil details Airfoil plotter |
Drawing Options
Polars for (n12-il,ht08-il,e1200-il,e184-il,la5055-il,wb13535sm-il,ag09-il,e178-il,n24-il,hq158-il,n13-il,hq1012-il,s102b-il,k2-il,ht12-il,tsagi8-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| n12-il | 50,000 | 9 | 28.9 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n12-il | 50,000 | 5 | 27.7 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n12-il | 100,000 | 9 | 39 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n12-il | 100,000 | 5 | 36.1 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n12-il | 200,000 | 9 | 46.4 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n12-il | 200,000 | 5 | 42.9 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n12-il | 500,000 | 9 | 53.3 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n12-il | 500,000 | 5 | 55.5 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n12-il | 1,000,000 | 9 | 64.4 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n12-il | 1,000,000 | 5 | 73.7 at α=9° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ht08-il | 50,000 | 9 | 21.6 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ht08-il | 50,000 | 5 | 20.1 at α=2.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ht08-il | 100,000 | 9 | 28.8 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ht08-il | 100,000 | 5 | 26.1 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ht08-il | 200,000 | 9 | 33.1 at α=2° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ht08-il | 200,000 | 5 | 34.2 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ht08-il | 500,000 | 9 | 44.1 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ht08-il | 500,000 | 5 | 48.9 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ht08-il | 1,000,000 | 9 | 56.7 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ht08-il | 1,000,000 | 5 | 63.5 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e1200-il | 50,000 | 9 | 9.3 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e1200-il | 50,000 | 5 | 23.4 at α=10.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e1200-il | 100,000 | 9 | 46.9 at α=8.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e1200-il | 100,000 | 5 | 39.5 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e1200-il | 200,000 | 9 | 69.5 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e1200-il | 200,000 | 5 | 68.2 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e1200-il | 500,000 | 9 | 107.4 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e1200-il | 500,000 | 5 | 96.1 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e1200-il | 1,000,000 | 9 | 131.8 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e1200-il | 1,000,000 | 5 | 109.4 at α=2.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e184-il | 50,000 | 9 | 30.9 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e184-il | 50,000 | 5 | 31.7 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e184-il | 100,000 | 9 | 44.4 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e184-il | 100,000 | 5 | 43.2 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e184-il | 200,000 | 9 | 58 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e184-il | 200,000 | 5 | 53.5 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e184-il | 500,000 | 9 | 73.9 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e184-il | 500,000 | 5 | 63.9 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e184-il | 1,000,000 | 9 | 82.4 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e184-il | 1,000,000 | 5 | 67 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| la5055-il | 50,000 | 9 | 4.9 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| la5055-il | 50,000 | 5 | 8.7 at α=13.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| la5055-il | 100,000 | 9 | 18.7 at α=15.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| la5055-il | 100,000 | 5 | 15.5 at α=13.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| la5055-il | 200,000 | 9 | 24.7 at α=13.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| la5055-il | 200,000 | 5 | 46.1 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| la5055-il | 500,000 | 9 | 116.3 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| la5055-il | 500,000 | 5 | 104.2 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| la5055-il | 1,000,000 | 9 | 149.6 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| la5055-il | 1,000,000 | 5 | 83.5 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| wb13535sm-il | 50,000 | 9 | 26.6 at α=11.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| wb13535sm-il | 50,000 | 5 | 33.4 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| wb13535sm-il | 100,000 | 9 | 51.8 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| wb13535sm-il | 100,000 | 5 | 51.6 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| wb13535sm-il | 200,000 | 9 | 73.8 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| wb13535sm-il | 200,000 | 5 | 68.8 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| wb13535sm-il | 500,000 | 9 | 101.3 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| wb13535sm-il | 500,000 | 5 | 84.6 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| wb13535sm-il | 1,000,000 | 9 | 108.2 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| wb13535sm-il | 1,000,000 | 5 | 102.4 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ag09-il | 50,000 | 9 | 32.4 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ag09-il | 50,000 | 5 | 32.9 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ag09-il | 100,000 | 9 | 44.3 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ag09-il | 100,000 | 5 | 44.1 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ag09-il | 200,000 | 9 | 56.4 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ag09-il | 200,000 | 5 | 55.6 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ag09-il | 500,000 | 9 | 74.4 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ag09-il | 500,000 | 5 | 70.7 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ag09-il | 1,000,000 | 9 | 87 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ag09-il | 1,000,000 | 5 | 82 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e178-il | 50,000 | 9 | 36.7 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e178-il | 50,000 | 5 | 37.7 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e178-il | 100,000 | 9 | 56.3 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e178-il | 100,000 | 5 | 55.8 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e178-il | 200,000 | 9 | 77.2 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e178-il | 200,000 | 5 | 73.5 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e178-il | 500,000 | 9 | 105 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e178-il | 500,000 | 5 | 95.1 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e178-il | 1,000,000 | 9 | 125.1 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e178-il | 1,000,000 | 5 | 108.8 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n24-il | 50,000 | 9 | 6.5 at α=1° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n24-il | 50,000 | 5 | 24.5 at α=2.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n24-il | 100,000 | 9 | 41.5 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n24-il | 100,000 | 5 | 47 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n24-il | 200,000 | 9 | 65.6 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n24-il | 200,000 | 5 | 64.6 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n24-il | 500,000 | 9 | 91.5 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n24-il | 500,000 | 5 | 84.4 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n24-il | 1,000,000 | 9 | 108.7 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n24-il | 1,000,000 | 5 | 104.1 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hq158-il | 50,000 | 9 | 35.7 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hq158-il | 50,000 | 5 | 35.9 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hq158-il | 100,000 | 9 | 51.9 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hq158-il | 100,000 | 5 | 49 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hq158-il | 200,000 | 9 | 68.3 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hq158-il | 200,000 | 5 | 60.7 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hq158-il | 500,000 | 9 | 86.8 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hq158-il | 500,000 | 5 | 70 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hq158-il | 1,000,000 | 9 | 92 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hq158-il | 1,000,000 | 5 | 77.5 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n13-il | 50,000 | 9 | 29 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n13-il | 50,000 | 5 | 27.7 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n13-il | 100,000 | 9 | 41.3 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n13-il | 100,000 | 5 | 37.2 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n13-il | 200,000 | 9 | 49.4 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n13-il | 200,000 | 5 | 45.8 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n13-il | 500,000 | 9 | 60.2 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n13-il | 500,000 | 5 | 60.8 at α=9° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n13-il | 1,000,000 | 9 | 73.1 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n13-il | 1,000,000 | 5 | 71 at α=8.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hq1012-il | 50,000 | 9 | 31 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hq1012-il | 50,000 | 5 | 32 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hq1012-il | 100,000 | 9 | 47.1 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hq1012-il | 100,000 | 5 | 45.1 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hq1012-il | 200,000 | 9 | 63.9 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hq1012-il | 200,000 | 5 | 54.9 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hq1012-il | 500,000 | 9 | 75.6 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hq1012-il | 500,000 | 5 | 69.6 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hq1012-il | 1,000,000 | 9 | 87.5 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hq1012-il | 1,000,000 | 5 | 80.6 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s102b-il | 50,000 | 9 | 31.1 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s102b-il | 50,000 | 5 | 28.1 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s102b-il | 100,000 | 9 | 42.6 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s102b-il | 100,000 | 5 | 43.8 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s102b-il | 200,000 | 9 | 60.5 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s102b-il | 200,000 | 5 | 57.6 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s102b-il | 500,000 | 9 | 81.9 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s102b-il | 500,000 | 5 | 70.7 at α=2.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s102b-il | 1,000,000 | 9 | 96.4 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s102b-il | 1,000,000 | 5 | 85.3 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| k2-il | 50,000 | 9 | 21.7 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| k2-il | 50,000 | 5 | 21.1 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| k2-il | 100,000 | 9 | 28.9 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| k2-il | 100,000 | 5 | 25.8 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| k2-il | 200,000 | 9 | 29 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| k2-il | 200,000 | 5 | 35.1 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| k2-il | 500,000 | 9 | 44 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| k2-il | 500,000 | 5 | 52.3 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| k2-il | 1,000,000 | 9 | 60.4 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| k2-il | 1,000,000 | 5 | 66.7 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ht12-il | 50,000 | 9 | 21.2 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ht12-il | 50,000 | 5 | 20.3 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ht12-il | 100,000 | 9 | 26.8 at α=2.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ht12-il | 100,000 | 5 | 26.8 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ht12-il | 200,000 | 9 | 32.3 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ht12-il | 200,000 | 5 | 35.1 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ht12-il | 500,000 | 9 | 45.2 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ht12-il | 500,000 | 5 | 50.2 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ht12-il | 1,000,000 | 9 | 58.3 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ht12-il | 1,000,000 | 5 | 64.7 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| tsagi8-il | 50,000 | 9 | 32.8 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| tsagi8-il | 50,000 | 5 | 32.5 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| tsagi8-il | 100,000 | 9 | 45.3 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| tsagi8-il | 100,000 | 5 | 44.4 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| tsagi8-il | 200,000 | 9 | 57.7 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| tsagi8-il | 200,000 | 5 | 55.4 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| tsagi8-il | 500,000 | 9 | 72.2 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| tsagi8-il | 500,000 | 5 | 65.1 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| tsagi8-il | 1,000,000 | 9 | 76.8 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| tsagi8-il | 1,000,000 | 5 | 69.7 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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