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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(fx76120-il) WORTMANN FX 76-120 | Wortmann FX 76-120 symmetrical airfoil Max thickness 12.1% at 27.9% chord Max camber 0% at 0% chord | Remove Airfoil details Airfoil plotter |
(npl9510-il) NPL 9510 AIRFOIL | NPL 9510 transonic airfoil Max thickness 11.1% at 32% chord Max camber 1.6% at 80% chord | Remove Airfoil details Airfoil plotter |
(fx69274-il) WORTMANN FX 69-274 | Wortmann FX 69-274 airfoil Max thickness 27.4% at 33.9% chord Max camber 3.2% at 37.1% chord | Remove Airfoil details Airfoil plotter |
(drgnfly-il) DRAGONFLY CANARD | Dragonfly Canard airfoil Max thickness 19.3% at 37.6% chord Max camber 6.6% at 40.9% chord | Remove Airfoil details Airfoil plotter |
(ah95160-il) AH 95-160 | Althaus AH 95-160 airfoil Max thickness 16% at 38.9% chord Max camber 5.6% at 44.6% chord | Remove Airfoil details Airfoil plotter |
(fx61163-il) FX 61-163 AIRFOIL | Wortmann FX 61-163 airfoil Max thickness 16.4% at 37.1% chord Max camber 2.6% at 33.9% chord | Remove Airfoil details Airfoil plotter |
(amsoil1-il) RUTAN CANARD AIRFOIL | Rutan AMSOIL racer canard airfoil Max thickness 11.6% at 39% chord Max camber 2.1% at 42% chord | Remove Airfoil details Airfoil plotter |
(nacam18-il) NACA M18 | NACA M18 airfoil Max thickness 12% at 30% chord Max camber 4.1% at 30% chord | Remove Airfoil details Airfoil plotter |
(amsoil2-il) RUTAN WING AIRFOIL | Rutan AMSOIL racer wing airfoil Max thickness 11.8% at 39% chord Max camber 1% at 48% chord | Remove Airfoil details Airfoil plotter |
(ah83159-il) AH 83-159 | Althaus AH 83-159 airfoil Max thickness 15.9% at 40.2% chord Max camber 3.8% at 40.2% chord | Remove Airfoil details Airfoil plotter |
(fx75193-il) WORTMANN FX 75-193 | Wortmann FX 75-193 airfoil Max thickness 19.3% at 40.2% chord Max camber 3.7% at 69.1% chord | Remove Airfoil details Airfoil plotter |
(raf32md-il) RAF 32 MOD AIRFOIL | RAF-32 MOD airfoil Max thickness 10.2% at 30% chord Max camber 4% at 50% chord | Remove Airfoil details Airfoil plotter |
(ah93157-il) AH 93-157 | Althaus AH 93-157 airfoil Max thickness 15.7% at 39.6% chord Max camber 3.5% at 41.7% chord | Remove Airfoil details Airfoil plotter |
(fx71120-il) WORTMANN FX 71-120 AIRFOIL | Wortmann FX 71-120 airfoil Max thickness 12% at 25% chord Max camber 0% at 0% chord | Remove Airfoil details Airfoil plotter |
(raf30md-il) RAF 30 MOD AIRFOIL | RAF-30 MOD airfoil Max thickness 7.6% at 30% chord Max camber 0% at 0% chord | Remove Airfoil details Airfoil plotter |
(fx66h60-il) FX 66-H-60 | Wortmann FX 66-H-60 airfoil Max thickness 6% at 22.2% chord Max camber 1.7% at 17% chord | Remove Airfoil details Airfoil plotter |
(nn7mk20-il) NN7 MK20 | NN7 MK20 airfoil Max thickness 16.9% at 37.1% chord Max camber 3% at 59.8% chord | Remove Airfoil details Airfoil plotter |
(nacam12-il) NACA M12 | NACA M12 airfoil Max thickness 11.9% at 30% chord Max camber 2% at 30% chord | Remove Airfoil details Airfoil plotter |
(npl9626-il) NPL 9626 AIRFOIL | NPL 9626 rotorcraft airfoil Max thickness 12.1% at 30.9% chord Max camber 0.7% at 30.9% chord | Remove Airfoil details Airfoil plotter |
(marske5-il) MARSKE MONARCH AIRFOIL (NACA 43012A) | Marske Monarch airfoil (NACA 43012A) Max thickness 12.2% at 20% chord Max camber 3.4% at 15% chord | Remove Airfoil details Airfoil plotter |
(goe547-il) GOE 547 AIRFOIL | Gottingen 547 airfoil Max thickness 10.5% at 29.7% chord Max camber 4% at 49.7% chord | Remove Airfoil details Airfoil plotter |
(goe515-il) GOE 515 AIRFOIL | Gottingen 515 airfoil Max thickness 8.5% at 30% chord Max camber 2.8% at 40% chord | Remove Airfoil details Airfoil plotter |
(usnps4-il) USNPS4 (smoothed) | Jacobs USNPS4 (smoothed) 17.5 kW wind turbine airfoil Max thickness 11.9% at 34.2% chord Max camber 5% at 34.2% chord | Remove Airfoil details Airfoil plotter |
(goe235-il) GOE 235 (SCHTTE-LANZ) AIRFOIL | Gottingen 235 (SCHATTE-LANZ) airfoil Max thickness 6.5% at 19.9% chord Max camber 3.5% at 39.9% chord | Remove Airfoil details Airfoil plotter |
(goe528-il) GOE 528 AIRFOIL | Gottingen 528 airfoil Max thickness 12.5% at 29.8% chord Max camber 6.2% at 39.8% chord | Remove Airfoil details Airfoil plotter |
(goe284-il) GOE 284 AIRFOIL | Gottingen 284 airfoil Max thickness 17.7% at 29.3% chord Max camber 5.1% at 39.3% chord | Remove Airfoil details Airfoil plotter |
(goe176-il) GOE 176 (ALBATROS 7020) AIRFOIL | Gottingen 176 (Albatros 7020) airfoil Max thickness 10.3% at 19.8% chord Max camber 5.6% at 39.8% chord | Remove Airfoil details Airfoil plotter |
(rc08b3-il) NASA/LANGLEY RC-08(B)3 AIRFOIL | NASA/Langley RC-08(B)3 rotorcraft airfoil Max thickness 8% at 37.8% chord Max camber 1.1% at 34.1% chord | Remove Airfoil details Airfoil plotter |
(goe488-il) GOE 488 AIRFOIL | Gottingen 488 airfoil Max thickness 6.8% at 19.9% chord Max camber 3% at 39.9% 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 |
(goe420-il) GOE 420 AIRFOIL | Gottingen 420 airfoil Max thickness 18.8% at 30% chord Max camber 4.3% at 50% chord | Remove Airfoil details Airfoil plotter |
(goe400-il) GOE 400 AIRFOIL | Gottingen 400 airfoil Max thickness 6.1% at 20% chord Max camber 4.9% at 40% chord | Remove Airfoil details Airfoil plotter |
(goe269-il) GOE 269 AIRFOIL | Gottingen 269 airfoil Max thickness 6.6% at 29.9% chord Max camber 5% at 39.9% 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 |
(clarkz-il) CLARK Z AIRFOIL | CLARK Z airfoil Max thickness 11.8% at 30% chord Max camber 4% at 40% chord | Remove Airfoil details Airfoil plotter |
(goe426-il) GOE 426 AIRFOIL | Gottingen 426 airfoil Max thickness 13.6% at 30% chord Max camber 4.6% at 40% chord | Remove Airfoil details Airfoil plotter |
Drawing Options
Polars for (fx76120-il,npl9510-il,fx69274-il,drgnfly-il,ah95160-il,fx61163-il,amsoil1-il,nacam18-il,amsoil2-il,ah83159-il,fx75193-il,raf32md-il,ah93157-il,fx71120-il,raf30md-il,fx66h60-il,nn7mk20-il,nacam12-il,npl9626-il,marske5-il,goe547-il,goe515-il,usnps4-il,goe235-il,goe528-il,goe284-il,goe176-il,rc08b3-il,goe488-il,goe386-il,goe420-il,goe400-il,goe269-il,goe279-il,clarkz-il,goe426-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| fx76120-il | 50,000 | 9 | 25 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx76120-il | 50,000 | 5 | 26.7 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx76120-il | 100,000 | 9 | 35.9 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx76120-il | 100,000 | 5 | 37.8 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx76120-il | 200,000 | 9 | 49.3 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx76120-il | 200,000 | 5 | 49.4 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx76120-il | 500,000 | 9 | 67.9 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx76120-il | 500,000 | 5 | 64.2 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx76120-il | 1,000,000 | 9 | 78.9 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx76120-il | 1,000,000 | 5 | 76.8 at α=9.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| npl9510-il | 50,000 | 9 | 15.5 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| npl9510-il | 50,000 | 5 | 17 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| npl9510-il | 100,000 | 9 | 18.4 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| npl9510-il | 100,000 | 5 | 23.3 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| npl9510-il | 200,000 | 9 | 25.4 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| npl9510-il | 200,000 | 5 | 32.4 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| npl9510-il | 500,000 | 9 | 40.3 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| npl9510-il | 500,000 | 5 | 49.8 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| npl9510-il | 1,000,000 | 9 | 57.2 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| npl9510-il | 1,000,000 | 5 | 67.8 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx69274-il | 50,000 | 9 | 1.6 at α=10° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx69274-il | 100,000 | 9 | 1.7 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx69274-il | 200,000 | 9 | 36 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx69274-il | 500,000 | 9 | 65.4 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx69274-il | 1,000,000 | 9 | 81.3 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| drgnfly-il | 50,000 | 9 | 3.9 at α=12.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| drgnfly-il | 50,000 | 5 | 5.8 at α=14.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| drgnfly-il | 100,000 | 9 | 4.7 at α=13.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| drgnfly-il | 100,000 | 5 | 8.4 at α=9.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| drgnfly-il | 200,000 | 9 | 8.8 at α=13.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| drgnfly-il | 200,000 | 5 | 45.8 at α=2.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| drgnfly-il | 500,000 | 9 | 87.8 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| drgnfly-il | 500,000 | 5 | 104.7 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| drgnfly-il | 1,000,000 | 9 | 144.6 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| drgnfly-il | 1,000,000 | 5 | 149.1 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah95160-il | 50,000 | 9 | 5.7 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah95160-il | 50,000 | 5 | 12.8 at α=14.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah95160-il | 100,000 | 9 | 23.9 at α=13.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah95160-il | 100,000 | 5 | 24.8 at α=1.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah95160-il | 200,000 | 9 | 65.4 at α=10° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah95160-il | 200,000 | 5 | 73.7 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah95160-il | 500,000 | 9 | 130.3 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah95160-il | 500,000 | 5 | 128.1 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah95160-il | 1,000,000 | 9 | 173.1 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah95160-il | 1,000,000 | 5 | 163.2 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx61163-il | 50,000 | 9 | 6.1 at α=0.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx61163-il | 50,000 | 5 | 19.4 at α=11.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx61163-il | 100,000 | 9 | 47.7 at α=10.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx61163-il | 100,000 | 5 | 50 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx61163-il | 200,000 | 9 | 70.9 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx61163-il | 200,000 | 5 | 72.7 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx61163-il | 500,000 | 9 | 103.1 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx61163-il | 500,000 | 5 | 98.8 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx61163-il | 1,000,000 | 5 | 115.7 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx61163-il | 1,000,000 | 0 | 127.4 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| amsoil1-il | 50,000 | 9 | 33 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| amsoil1-il | 50,000 | 5 | 31.9 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| amsoil1-il | 100,000 | 9 | 48.6 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| amsoil1-il | 100,000 | 5 | 46.8 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| amsoil1-il | 200,000 | 9 | 67.5 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| amsoil1-il | 200,000 | 5 | 59.9 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| amsoil1-il | 500,000 | 9 | 86.2 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| amsoil1-il | 500,000 | 5 | 68.1 at α=2.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| amsoil1-il | 1,000,000 | 9 | 93 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| amsoil1-il | 1,000,000 | 5 | 81.1 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| nacam18-il | 50,000 | 9 | 10.2 at α=1.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| nacam18-il | 50,000 | 5 | 26.2 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| nacam18-il | 100,000 | 9 | 47.9 at α=10.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| nacam18-il | 100,000 | 5 | 50.8 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| nacam18-il | 200,000 | 9 | 71.7 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| nacam18-il | 200,000 | 5 | 72.3 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| nacam18-il | 500,000 | 9 | 102.6 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| nacam18-il | 500,000 | 5 | 99.2 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| nacam18-il | 1,000,000 | 9 | 125.1 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| nacam18-il | 1,000,000 | 5 | 114 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| amsoil2-il | 50,000 | 9 | 25.9 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| amsoil2-il | 50,000 | 5 | 25.3 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| amsoil2-il | 100,000 | 9 | 38.7 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| amsoil2-il | 100,000 | 5 | 35.4 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| amsoil2-il | 200,000 | 9 | 48.9 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| amsoil2-il | 200,000 | 5 | 42.8 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| amsoil2-il | 500,000 | 9 | 56.9 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| amsoil2-il | 500,000 | 5 | 61.7 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| amsoil2-il | 1,000,000 | 9 | 74.9 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| amsoil2-il | 1,000,000 | 5 | 77.4 at α=9° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah83159-il | 50,000 | 9 | 17.1 at α=13.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah83159-il | 50,000 | 5 | 15.5 at α=13° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah83159-il | 100,000 | 9 | 31.4 at α=11.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah83159-il | 100,000 | 5 | 29 at α=11° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah83159-il | 200,000 | 9 | 64.5 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah83159-il | 200,000 | 5 | 63.5 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah83159-il | 500,000 | 9 | 106.2 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah83159-il | 500,000 | 5 | 105.5 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah83159-il | 1,000,000 | 9 | 136.8 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah83159-il | 1,000,000 | 5 | 133.8 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx75193-il | 50,000 | 9 | 4.2 at α=12.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx75193-il | 50,000 | 5 | 11.7 at α=14.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx75193-il | 100,000 | 9 | 23.4 at α=12.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx75193-il | 100,000 | 5 | 22.9 at α=11.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx75193-il | 200,000 | 9 | 43.4 at α=10° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx75193-il | 200,000 | 5 | 44.1 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx75193-il | 500,000 | 9 | 91.7 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx75193-il | 500,000 | 5 | 93.5 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx75193-il | 1,000,000 | 9 | 122.7 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx75193-il | 1,000,000 | 5 | 120.1 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| raf32md-il | 50,000 | 9 | 38 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| raf32md-il | 50,000 | 5 | 37.5 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| raf32md-il | 100,000 | 9 | 62.1 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| raf32md-il | 100,000 | 5 | 61.3 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| raf32md-il | 200,000 | 9 | 87.2 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| raf32md-il | 200,000 | 5 | 83.8 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| raf32md-il | 500,000 | 9 | 120.8 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| raf32md-il | 500,000 | 5 | 110.5 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| raf32md-il | 1,000,000 | 9 | 144.4 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| raf32md-il | 1,000,000 | 5 | 124.3 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah93157-il | 50,000 | 9 | 4.7 at α=11° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah93157-il | 50,000 | 5 | 14.4 at α=12.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah93157-il | 100,000 | 9 | 40 at α=10.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah93157-il | 100,000 | 5 | 37.5 at α=9.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah93157-il | 200,000 | 9 | 74.9 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah93157-il | 200,000 | 5 | 66.2 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah93157-il | 500,000 | 9 | 100.4 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah93157-il | 500,000 | 5 | 92 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah93157-il | 1,000,000 | 9 | 120.6 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah93157-il | 1,000,000 | 5 | 112.2 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx71120-il | 50,000 | 9 | 20.3 at α=2.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx71120-il | 50,000 | 5 | 21.2 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx71120-il | 100,000 | 9 | 26.3 at α=2° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx71120-il | 100,000 | 5 | 29.1 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx71120-il | 200,000 | 9 | 34.5 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx71120-il | 200,000 | 5 | 38.9 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx71120-il | 500,000 | 9 | 50.3 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx71120-il | 500,000 | 5 | 56.3 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx71120-il | 1,000,000 | 9 | 64.4 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx71120-il | 1,000,000 | 5 | 71.8 at α=8.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| raf30md-il | 50,000 | 9 | 26.4 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| raf30md-il | 50,000 | 5 | 25.1 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| raf30md-il | 100,000 | 9 | 35.2 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| raf30md-il | 100,000 | 5 | 31 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| raf30md-il | 200,000 | 9 | 42.7 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| raf30md-il | 200,000 | 5 | 36.3 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| raf30md-il | 500,000 | 9 | 47.9 at α=2.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| raf30md-il | 500,000 | 5 | 52.3 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| raf30md-il | 1,000,000 | 9 | 59.9 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| raf30md-il | 1,000,000 | 5 | 65.4 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx66h60-il | 50,000 | 9 | 28.6 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx66h60-il | 50,000 | 5 | 29.9 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx66h60-il | 100,000 | 9 | 37.9 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx66h60-il | 100,000 | 5 | 40.1 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx66h60-il | 200,000 | 9 | 51.3 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx66h60-il | 200,000 | 5 | 51.3 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx66h60-il | 500,000 | 9 | 69.8 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx66h60-il | 500,000 | 5 | 67.8 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx66h60-il | 1,000,000 | 9 | 84.1 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx66h60-il | 1,000,000 | 5 | 76.8 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| nn7mk20-il | 50,000 | 9 | 21 at α=12.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| nn7mk20-il | 50,000 | 5 | 17.2 at α=12° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| nn7mk20-il | 100,000 | 9 | 44.2 at α=10° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| nn7mk20-il | 100,000 | 5 | 43.8 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| nn7mk20-il | 200,000 | 9 | 70.2 at α=8.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| nn7mk20-il | 200,000 | 5 | 69.9 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| nn7mk20-il | 500,000 | 9 | 101.8 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| nn7mk20-il | 500,000 | 5 | 99 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| nn7mk20-il | 1,000,000 | 9 | 127.2 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| nn7mk20-il | 1,000,000 | 5 | 118.1 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| nacam12-il | 50,000 | 9 | 31.8 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| nacam12-il | 50,000 | 5 | 33.6 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| nacam12-il | 100,000 | 9 | 49.4 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| nacam12-il | 100,000 | 5 | 48.8 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| nacam12-il | 200,000 | 9 | 66.3 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| nacam12-il | 200,000 | 5 | 56.6 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| nacam12-il | 500,000 | 9 | 71.5 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| nacam12-il | 500,000 | 5 | 62.7 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| nacam12-il | 1,000,000 | 9 | 78.3 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| nacam12-il | 1,000,000 | 5 | 71.7 at α=9.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| npl9626-il | 50,000 | 9 | 29.8 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| npl9626-il | 50,000 | 5 | 29.6 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| npl9626-il | 100,000 | 9 | 42.1 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| npl9626-il | 100,000 | 5 | 39.9 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| npl9626-il | 200,000 | 9 | 53.3 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| npl9626-il | 200,000 | 5 | 48.5 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| npl9626-il | 500,000 | 9 | 65.3 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| npl9626-il | 500,000 | 5 | 60.4 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| npl9626-il | 1,000,000 | 9 | 73.6 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| npl9626-il | 1,000,000 | 5 | 76.1 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| marske5-il | 50,000 | 9 | 15.7 at α=2° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| marske5-il | 50,000 | 5 | 20.8 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| marske5-il | 100,000 | 9 | 23.3 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| marske5-il | 100,000 | 5 | 31.8 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| marske5-il | 200,000 | 9 | 36.1 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| marske5-il | 200,000 | 5 | 47.7 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| marske5-il | 500,000 | 9 | 65.1 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| marske5-il | 500,000 | 5 | 73.6 at α=10.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| marske5-il | 1,000,000 | 9 | 92.9 at α=12.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| marske5-il | 1,000,000 | 5 | 96.5 at α=12° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe547-il | 50,000 | 9 | 36.9 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe547-il | 50,000 | 5 | 35.2 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe547-il | 100,000 | 9 | 60.4 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe547-il | 100,000 | 5 | 59.5 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe547-il | 200,000 | 9 | 86.9 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe547-il | 200,000 | 5 | 82.4 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe547-il | 500,000 | 9 | 120.6 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe547-il | 500,000 | 5 | 105.8 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe547-il | 1,000,000 | 9 | 143.4 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe547-il | 1,000,000 | 5 | 104.7 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe515-il | 50,000 | 9 | 37.6 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe515-il | 50,000 | 5 | 37.9 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe515-il | 100,000 | 9 | 56.8 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe515-il | 100,000 | 5 | 54.9 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe515-il | 200,000 | 9 | 77.2 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe515-il | 200,000 | 5 | 71 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe515-il | 500,000 | 9 | 103.3 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe515-il | 500,000 | 5 | 88 at α=2.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe515-il | 1,000,000 | 9 | 119 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe515-il | 1,000,000 | 5 | 95.1 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| usnps4-il | 50,000 | 9 | 32.7 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| usnps4-il | 50,000 | 5 | 37.1 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| usnps4-il | 100,000 | 9 | 55.5 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| usnps4-il | 100,000 | 5 | 53.2 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| usnps4-il | 200,000 | 9 | 74.3 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| usnps4-il | 200,000 | 5 | 67.2 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| usnps4-il | 500,000 | 9 | 95.2 at α=1° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| usnps4-il | 500,000 | 5 | 87.2 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| usnps4-il | 1,000,000 | 9 | 110.8 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| usnps4-il | 1,000,000 | 5 | 105.3 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe235-il | 50,000 | 9 | 36.9 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe235-il | 50,000 | 5 | 37.5 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe235-il | 100,000 | 9 | 52.2 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe235-il | 100,000 | 5 | 48 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe235-il | 200,000 | 9 | 60.8 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe235-il | 200,000 | 5 | 57.6 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe235-il | 500,000 | 9 | 73.9 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe235-il | 500,000 | 5 | 68.8 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe235-il | 1,000,000 | 9 | 80.8 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe235-il | 1,000,000 | 5 | 81.6 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe528-il | 50,000 | 9 | 9 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe528-il | 50,000 | 5 | 29.8 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe528-il | 100,000 | 9 | 46.6 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe528-il | 100,000 | 5 | 55.7 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe528-il | 200,000 | 9 | 75.5 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe528-il | 200,000 | 5 | 77.6 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe528-il | 500,000 | 9 | 110.5 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe528-il | 500,000 | 5 | 106.7 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe528-il | 1,000,000 | 9 | 137.7 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe528-il | 1,000,000 | 5 | 128.9 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe284-il | 50,000 | 9 | 4.3 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe284-il | 50,000 | 5 | 18 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe284-il | 100,000 | 9 | 34.1 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe284-il | 100,000 | 5 | 45.2 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe284-il | 200,000 | 9 | 69 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe284-il | 200,000 | 5 | 69.5 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe284-il | 500,000 | 9 | 103.5 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe284-il | 500,000 | 5 | 95 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe284-il | 1,000,000 | 9 | 126.5 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe284-il | 1,000,000 | 5 | 107.1 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe176-il | 50,000 | 9 | 30.3 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe176-il | 50,000 | 5 | 40.2 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe176-il | 100,000 | 9 | 56 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe176-il | 100,000 | 5 | 57.5 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe176-il | 200,000 | 9 | 73.7 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe176-il | 200,000 | 5 | 73.6 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe176-il | 500,000 | 9 | 99.2 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe176-il | 500,000 | 5 | 87 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe176-il | 1,000,000 | 9 | 113.1 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe176-il | 1,000,000 | 5 | 93.5 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rc08b3-il | 50,000 | 9 | 32.2 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rc08b3-il | 50,000 | 5 | 31.2 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rc08b3-il | 100,000 | 9 | 45.5 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rc08b3-il | 100,000 | 5 | 41.5 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rc08b3-il | 200,000 | 9 | 57.7 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rc08b3-il | 200,000 | 5 | 49.3 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rc08b3-il | 500,000 | 9 | 67.8 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rc08b3-il | 500,000 | 5 | 60 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rc08b3-il | 1,000,000 | 9 | 71.5 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rc08b3-il | 1,000,000 | 5 | 73.8 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe488-il | 50,000 | 9 | 37.2 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe488-il | 50,000 | 5 | 37.7 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe488-il | 100,000 | 9 | 55.2 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe488-il | 100,000 | 5 | 51.3 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe488-il | 200,000 | 9 | 74.6 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe488-il | 200,000 | 5 | 64.8 at α=2° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe488-il | 500,000 | 9 | 96.4 at α=1.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe488-il | 500,000 | 5 | 79.7 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe488-il | 1,000,000 | 9 | 101.4 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe488-il | 1,000,000 | 5 | 89.4 at α=3.25° | 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 | |
| goe420-il | 50,000 | 9 | 4 at α=10.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe420-il | 50,000 | 5 | 13.4 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe420-il | 100,000 | 9 | 32.7 at α=11.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe420-il | 100,000 | 5 | 44.5 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe420-il | 200,000 | 9 | 66.7 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe420-il | 200,000 | 5 | 62.7 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe420-il | 500,000 | 9 | 89.9 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe420-il | 500,000 | 5 | 83.5 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe420-il | 1,000,000 | 9 | 111.3 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe420-il | 1,000,000 | 5 | 102.2 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe400-il | 50,000 | 9 | 37.4 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe400-il | 50,000 | 5 | 41.9 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe400-il | 100,000 | 9 | 59.1 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe400-il | 100,000 | 5 | 61.4 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe400-il | 200,000 | 9 | 81 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe400-il | 200,000 | 5 | 79.9 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe400-il | 500,000 | 9 | 109.8 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe400-il | 500,000 | 5 | 88.8 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe400-il | 1,000,000 | 9 | 126 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe400-il | 1,000,000 | 5 | 101.4 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe269-il | 50,000 | 9 | 36.1 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe269-il | 50,000 | 5 | 43.2 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe269-il | 100,000 | 9 | 59.1 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe269-il | 100,000 | 5 | 61.5 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe269-il | 200,000 | 9 | 80.2 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe269-il | 200,000 | 5 | 79.2 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe269-il | 500,000 | 9 | 107.7 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe269-il | 500,000 | 5 | 102.9 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe269-il | 1,000,000 | 9 | 127.9 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe269-il | 1,000,000 | 5 | 115.6 at α=5.25° | 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 | |
| clarkz-il | 50,000 | 9 | 30.4 at α=10° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| clarkz-il | 50,000 | 5 | 36.2 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| clarkz-il | 100,000 | 9 | 54 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| clarkz-il | 100,000 | 5 | 55.4 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| clarkz-il | 200,000 | 9 | 74.8 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| clarkz-il | 200,000 | 5 | 72.2 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| clarkz-il | 500,000 | 9 | 100.9 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| clarkz-il | 500,000 | 5 | 93.5 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| clarkz-il | 1,000,000 | 9 | 120.6 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| clarkz-il | 1,000,000 | 5 | 109.5 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe426-il | 50,000 | 9 | 7.9 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe426-il | 50,000 | 5 | 26.6 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe426-il | 100,000 | 9 | 46.9 at α=11.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe426-il | 100,000 | 5 | 52.1 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe426-il | 200,000 | 9 | 75.9 at α=9.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe426-il | 200,000 | 5 | 77.9 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe426-il | 500,000 | 9 | 112.7 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe426-il | 500,000 | 5 | 110.4 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe426-il | 1,000,000 | 9 | 141.9 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe426-il | 1,000,000 | 5 | 134.3 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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