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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(fx67k150-il) FX 67-K-150/17 AIRFOIL | Wortmann FX 67-K-150/17 airfoil Max thickness 15% at 40.2% chord Max camber 4.8% at 43.5% chord | Remove Airfoil details Airfoil plotter |
(fx62k131-il) WORTMANN FX 62-K-131 AIRFOIL | Wortmann FX 62-K-131/17 airfoil Max thickness 13.1% at 40.2% chord Max camber 3.9% at 53.3% chord | Remove Airfoil details Airfoil plotter |
(ah93k130-il) AH 93-K-130/15 | Althaus AH 93-K-130/15 airfoil for use with flaps (K) Max thickness 13.1% at 42% chord Max camber 3.5% at 42% chord | Remove Airfoil details Airfoil plotter |
(fx66s171-il) FX 66-S-171 AIRFOIL | Wortmann FX 66-S-171 airfoil Max thickness 17.1% at 33.9% chord Max camber 3.9% at 43.5% chord | Remove Airfoil details Airfoil plotter |
(goe610b-il) GOE 610 B AIRFOIL | Gottingen 610 B airfoil Max thickness 7.8% at 39.9% chord Max camber 5.3% at 39.9% chord | Remove Airfoil details Airfoil plotter |
(ag45c03-il) AG45c -03f | Drela AG45c -03f airfoil Max thickness 6.9% at 23.5% chord Max camber 2% at 31.7% chord | Remove Airfoil details Airfoil plotter |
(clarkyh-il) CLARK YH AIRFOIL | CLARK YH airfoil Max thickness 11.9% at 30% chord Max camber 2.5% at 30% chord | Remove Airfoil details Airfoil plotter |
(cr001sm-il) cr001sm | Cody Robertson CR 001 R/C hand-launch low Reynolds number airfoil (smoothed) Max thickness 7.3% at 27.1% chord Max camber 4.1% at 45.4% chord | Remove Airfoil details Airfoil plotter |
(ah80140-il) AH 80-140 | Althaus AH 80-140 airfoil Max thickness 14% at 30.9% chord Max camber 4.4% at 33.9% chord | Remove Airfoil details Airfoil plotter |
(clarkys-il) CLARK YS AIRFOIL | CLARK YS airfoil Max thickness 11.7% at 30% chord Max camber 2.4% at 30% chord | Remove Airfoil details Airfoil plotter |
(fx61147-il) FX 61-147 AIRFOIL | Wortmann FX 61-147 airfoil Max thickness 14.8% at 33.9% chord Max camber 3.2% at 33.9% chord | Remove Airfoil details Airfoil plotter |
(fx61168-il) FX 61-168 AIRFOIL | Wortmann FX 61-168 airfoil Max thickness 16.8% at 37.1% chord Max camber 3% at 37.1% chord | Remove Airfoil details Airfoil plotter |
(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 |
(ah93156-il) AH 93-156 | Althaus AH 93-156 airfoil Max thickness 15.7% at 39.5% chord Max camber 3.7% at 41.5% chord | Remove Airfoil details Airfoil plotter |
(nlf0115-il) NLF(1)-0115 | NASA/Langley/Somers-Selig-Maughmer NLF(1)-0115 natural laminar flow airfoil Max thickness 15% at 44.1% chord Max camber 1.8% at 30% chord | Remove Airfoil details Airfoil plotter |
(ag47c03-il) AG47c -03f | Drela AG47c -03f airfoil Max thickness 5.1% at 22.4% chord Max camber 1.3% at 33.4% chord | Remove Airfoil details Airfoil plotter |
Drawing Options
Polars for (fx67k150-il,fx62k131-il,ah93k130-il,fx66s171-il,goe610b-il,ag45c03-il,clarkyh-il,cr001sm-il,ah80140-il,clarkys-il,fx61147-il,fx61168-il,marske7-il,ah93156-il,nlf0115-il,ag47c03-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| fx67k150-il | 50,000 | 9 | 5.8 at α=10° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx67k150-il | 50,000 | 5 | 14.3 at α=12° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx67k150-il | 100,000 | 9 | 25 at α=10.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx67k150-il | 100,000 | 5 | 27.1 at α=10° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx67k150-il | 200,000 | 9 | 61.6 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx67k150-il | 200,000 | 5 | 68.5 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx67k150-il | 500,000 | 9 | 126.3 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx67k150-il | 500,000 | 5 | 118.2 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx67k150-il | 1,000,000 | 9 | 157.2 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx67k150-il | 1,000,000 | 5 | 147.8 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx62k131-il | 50,000 | 5 | 29 at α=9.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx62k131-il | 50,000 | 0 | 30.5 at α=9.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx62k131-il | 100,000 | 5 | 55.1 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx62k131-il | 100,000 | 0 | 56.4 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx62k131-il | 200,000 | 5 | 84.1 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx62k131-il | 200,000 | 0 | 83.7 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx62k131-il | 500,000 | 5 | 125.5 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx62k131-il | 500,000 | 0 | 124 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx62k131-il | 1,000,000 | 5 | 153.3 at α=2.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx62k131-il | 1,000,000 | 0 | 162.4 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah93k130-il | 50,000 | 9 | 25.1 at α=10.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah93k130-il | 50,000 | 5 | 22.6 at α=10.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah93k130-il | 100,000 | 9 | 42.4 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah93k130-il | 100,000 | 5 | 40.7 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah93k130-il | 200,000 | 9 | 75.6 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah93k130-il | 200,000 | 5 | 73.5 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah93k130-il | 500,000 | 9 | 114.8 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah93k130-il | 500,000 | 5 | 104.5 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah93k130-il | 1,000,000 | 9 | 136.6 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah93k130-il | 1,000,000 | 5 | 108.9 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx66s171-il | 50,000 | 9 | 5 at α=9.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx66s171-il | 50,000 | 5 | 12.7 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx66s171-il | 100,000 | 9 | 13.3 at α=1° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx66s171-il | 100,000 | 5 | 39.2 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx66s171-il | 200,000 | 9 | 70.3 at α=10.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx66s171-il | 200,000 | 5 | 72.4 at α=9.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx66s171-il | 500,000 | 9 | 113.9 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx66s171-il | 500,000 | 5 | 113.4 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx66s171-il | 1,000,000 | 9 | 147.6 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx66s171-il | 1,000,000 | 5 | 133.8 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe610b-il | 50,000 | 9 | 37.4 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe610b-il | 50,000 | 5 | 38.8 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe610b-il | 100,000 | 9 | 61.2 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe610b-il | 100,000 | 5 | 62.7 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe610b-il | 200,000 | 9 | 86.5 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe610b-il | 200,000 | 5 | 84 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe610b-il | 500,000 | 9 | 118 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe610b-il | 500,000 | 5 | 95.1 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe610b-il | 1,000,000 | 9 | 132.2 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe610b-il | 1,000,000 | 5 | 99.4 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ag45c03-il | 50,000 | 9 | 29.7 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ag45c03-il | 50,000 | 5 | 34.9 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ag45c03-il | 100,000 | 9 | 46 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ag45c03-il | 100,000 | 5 | 47.9 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ag45c03-il | 200,000 | 9 | 62.4 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ag45c03-il | 200,000 | 5 | 61 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ag45c03-il | 500,000 | 9 | 83 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ag45c03-il | 500,000 | 5 | 78.1 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ag45c03-il | 1,000,000 | 9 | 97.4 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ag45c03-il | 1,000,000 | 5 | 91.2 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| clarkyh-il | 50,000 | 9 | 29.1 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| clarkyh-il | 50,000 | 5 | 33 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| clarkyh-il | 100,000 | 9 | 47.7 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| clarkyh-il | 100,000 | 5 | 49.2 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| clarkyh-il | 200,000 | 9 | 66 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| clarkyh-il | 200,000 | 5 | 62.3 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| clarkyh-il | 500,000 | 9 | 84 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| clarkyh-il | 500,000 | 5 | 77.7 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| clarkyh-il | 1,000,000 | 9 | 97.4 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| clarkyh-il | 1,000,000 | 5 | 89.1 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| cr001sm-il | 50,000 | 9 | 41.2 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| cr001sm-il | 50,000 | 5 | 44.2 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| cr001sm-il | 100,000 | 9 | 64.8 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| cr001sm-il | 100,000 | 5 | 64.3 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| cr001sm-il | 200,000 | 9 | 89.3 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| cr001sm-il | 200,000 | 5 | 83.3 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| cr001sm-il | 500,000 | 9 | 120.2 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| cr001sm-il | 500,000 | 5 | 105.2 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| cr001sm-il | 1,000,000 | 9 | 139.9 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| cr001sm-il | 1,000,000 | 5 | 119.7 at α=2.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah80140-il | 50,000 | 9 | 5.3 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah80140-il | 50,000 | 5 | 14.3 at α=2° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah80140-il | 100,000 | 9 | 22.5 at α=14° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah80140-il | 100,000 | 5 | 35.7 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah80140-il | 200,000 | 9 | 70.9 at α=10.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah80140-il | 200,000 | 5 | 74.2 at α=9.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah80140-il | 500,000 | 9 | 116.4 at α=8.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah80140-il | 500,000 | 5 | 113.2 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah80140-il | 1,000,000 | 9 | 149.2 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah80140-il | 1,000,000 | 5 | 139 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| clarkys-il | 50,000 | 9 | 23.2 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| clarkys-il | 50,000 | 5 | 31.7 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| clarkys-il | 100,000 | 9 | 45.7 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| clarkys-il | 100,000 | 5 | 47 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| clarkys-il | 200,000 | 9 | 62.2 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| clarkys-il | 200,000 | 5 | 58.1 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| clarkys-il | 500,000 | 9 | 76.5 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| clarkys-il | 500,000 | 5 | 68.3 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| clarkys-il | 1,000,000 | 9 | 85.7 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| clarkys-il | 1,000,000 | 5 | 80.2 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx61147-il | 50,000 | 9 | 8.4 at α=1° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx61147-il | 50,000 | 5 | 28.7 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx61147-il | 100,000 | 9 | 50 at α=10.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx61147-il | 100,000 | 5 | 52.3 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx61147-il | 200,000 | 9 | 70.8 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx61147-il | 200,000 | 5 | 71.9 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx61147-il | 500,000 | 9 | 99.2 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx61147-il | 500,000 | 5 | 98.7 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx61147-il | 1,000,000 | 9 | 123.9 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx61147-il | 1,000,000 | 5 | 119.2 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx61168-il | 50,000 | 9 | 5.1 at α=10.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx61168-il | 50,000 | 5 | 15.4 at α=12° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx61168-il | 100,000 | 9 | 44.7 at α=11.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx61168-il | 100,000 | 5 | 48.4 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx61168-il | 200,000 | 9 | 71 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx61168-il | 200,000 | 5 | 73 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx61168-il | 500,000 | 9 | 104.5 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx61168-il | 500,000 | 5 | 101.2 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx61168-il | 1,000,000 | 9 | 129.7 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx61168-il | 1,000,000 | 5 | 120.4 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| 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 | |
| ah93156-il | 50,000 | 9 | 4.8 at α=9.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah93156-il | 50,000 | 5 | 15.6 at α=12° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah93156-il | 100,000 | 9 | 39 at α=11.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah93156-il | 100,000 | 5 | 35.5 at α=10.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah93156-il | 200,000 | 9 | 72.1 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah93156-il | 200,000 | 5 | 64.7 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah93156-il | 500,000 | 9 | 103.1 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah93156-il | 500,000 | 5 | 94.1 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah93156-il | 1,000,000 | 9 | 125 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah93156-il | 1,000,000 | 5 | 114.9 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| nlf0115-il | 50,000 | 9 | 30.7 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| nlf0115-il | 50,000 | 5 | 26.8 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| nlf0115-il | 100,000 | 9 | 45.5 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| nlf0115-il | 100,000 | 5 | 41.4 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| nlf0115-il | 200,000 | 9 | 60.8 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| nlf0115-il | 200,000 | 5 | 56 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| nlf0115-il | 500,000 | 9 | 81.9 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| nlf0115-il | 500,000 | 5 | 69.5 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| nlf0115-il | 1,000,000 | 9 | 94.4 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| nlf0115-il | 1,000,000 | 5 | 76.3 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ag47c03-il | 50,000 | 9 | 30.3 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ag47c03-il | 50,000 | 5 | 30.7 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ag47c03-il | 100,000 | 9 | 42.3 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ag47c03-il | 100,000 | 5 | 39.3 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ag47c03-il | 200,000 | 9 | 53 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ag47c03-il | 200,000 | 5 | 49.3 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ag47c03-il | 500,000 | 9 | 65.2 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ag47c03-il | 500,000 | 5 | 66.6 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ag47c03-il | 1,000,000 | 9 | 80.3 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ag47c03-il | 1,000,000 | 5 | 80.7 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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