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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(ua79sf18-il) UNIVERSITY OF ALBERTA UA 79-SF-187 AIRFOIL | University of Alberta/Marsden UA 79-SF-187 FLAPPED sailplane airfoil Max thickness 18.8% at 42.8% chord Max camber 3.7% at 63.4% chord | Remove Airfoil details Airfoil plotter |
(fx05h126-il) WORTMANN FX 05-H-126 AIRFOIL | Wortmann FX 05-H-126 rotorcraft airfoil Max thickness 12.6% at 37.1% chord Max camber 4.4% at 37.1% chord | Remove Airfoil details Airfoil plotter |
(v43012-il) BOEING VERTOL V43012-1.58 AIRFOIL | Boeing-Vertol V43012-1.58 rotorcraft airfoil Max thickness 12% at 32% chord Max camber 3.7% at 15% chord | Remove Airfoil details Airfoil plotter |
(naca23021-il) NACA 23021 | NACA 23021 airfoil Max thickness 21% at 30% chord Max camber 1.9% at 10% chord | Remove Airfoil details Airfoil plotter |
(boe106-il) BOEING 106 AIRFOIL | Boeing 106 airfoil Max thickness 13.1% at 30% chord Max camber 3.3% at 40% chord | Remove Airfoil details Airfoil plotter |
(daytonwright6-il) Dayton-Wright 6 | Dayton-Wright 6 airfoil Max thickness 13.6% at 30% chord Max camber 4.9% at 40% chord | Remove Airfoil details Airfoil plotter |
(fx049915-il) WORTMANN FX 049-915 AIRFOIL | Wortmann FX 049-915 airfoil Max thickness 14.7% at 37.1% chord Max camber 5.8% at 37.1% chord | Remove Airfoil details Airfoil plotter |
(v23010-il) BOEING-VERTOL V23010-1.58 AIRFOIL | Boeing-Vertol V23010-1.58 rotorcraft airfoil Max thickness 10.2% at 30% chord Max camber 1.8% at 15% chord | Remove Airfoil details Airfoil plotter |
(v43015-il) BOEING VERTOL V43015-2.48 AIRFOIL | Boeing-Vertol V43015-2.48 rotorcraft airfoil Max thickness 15% at 30% chord Max camber 3.7% at 15% chord | Remove Airfoil details Airfoil plotter |
(ua2-180sm-il) UA(2)-180 smoothed | UA(2)-180 (smoothed) airfoil for ultralight category aircraft Max thickness 18.2% at 34.1% chord Max camber 6.5% at 39.3% chord | Remove Airfoil details Airfoil plotter |
(usa31-il) USA 31 AIRFOIL | USA-31 airfoil Max thickness 14.8% at 19.7% chord Max camber 9.3% at 39.7% chord | Remove Airfoil details Airfoil plotter |
(isa571-il) I.S.A. 571 | I.S.A. 571 airfoil Max thickness 7.4% at 30% chord Max camber 3.6% at 30% chord | Remove Airfoil details Airfoil plotter |
(naca23012-il) NACA 23012 12% | NACA 23012 airfoil Max thickness 12% at 29.8% chord Max camber 1.8% at 12.7% chord | Remove Airfoil details Airfoil plotter |
(defcnd3-il) DEFIANT CANARD BL145 AIRFOIL | Rutan DEFIANT canard BL145 airfoil Max thickness 11.5% at 28.6% chord Max camber 2.4% at 28.6% chord | Remove Airfoil details Airfoil plotter |
(wb140-il) WB-140/35/FB 14% | Woody Blanchard WB140/35/FB R/C sailplane airfoil Max thickness 13.9% at 30% chord Max camber 3.7% at 45% chord | Remove Airfoil details Airfoil plotter |
(defcnd1-il) DEFIANT CANARD BL20 AIRFOIL | Rutan DEFIANT canard BL20 airfoil Max thickness 20.9% at 28.6% chord Max camber 4.5% at 36.1% 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 |
(ua79sfm-il) UNIVERSITY OF ALBERTA UA 79-SF-187 AIRFOIL MAIN ELEMENT | University of Alberta/Marsden UA 79-SF-187 sailplane airfoil MAIN ELEMENT Max thickness 18.8% at 42.8% chord Max camber 3% at 66.9% chord | Remove Airfoil details Airfoil plotter |
(clarky-il) CLARK Y AIRFOIL | CLARK Y airfoil Max thickness 11.7% at 28% chord Max camber 3.4% at 42% chord | Remove Airfoil details Airfoil plotter |
(isa962-il) I.S.A. 962 | I.S.A. 962 airfoil Max thickness 9.6% at 20% chord Max camber 4.6% at 40% 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 |
(gm15sm-il) GM15 (smoothed) | Gilbert Morris GM15 F1C class free flight flapper airfoil Max thickness 6.7% at 20.5% chord Max camber 4.8% at 49.3% chord | Remove Airfoil details Airfoil plotter |
(boe103-il) BOEING 103 AIRFOIL | Boeing 103 airfoil Max thickness 12.7% at 30% chord Max camber 3.6% at 40% chord | Remove Airfoil details Airfoil plotter |
(geminism-il) GEMINI (smoothed) | GEMINI R/C sailplane airfoil (smoothed) Max thickness 15.4% at 34.2% chord Max camber 2.2% at 37.9% chord | Remove Airfoil details Airfoil plotter |
(raf25-il) RAF 25 AIRFOIL | RAF-25 airfoil Max thickness 6.5% at 29.9% chord Max camber 1% at 49.9% chord | Remove Airfoil details Airfoil plotter |
(fx05188-il) WORTMANN FX 05-188 AIRFOIL | Wortmann FX 05-188 airfoil Max thickness 18.8% at 37.1% chord Max camber 2.6% at 50% chord | Remove Airfoil details Airfoil plotter |
(m25-il) NACA M25 AIRFOIL | NACA/Munk M-25 airfoil Max thickness 6.3% at 30% chord Max camber 8.2% at 30% chord | Remove Airfoil details Airfoil plotter |
(naca23018-il) NACA 23018 | NACA 23018 airfoil Max thickness 18% at 30% chord Max camber 1.8% at 15% chord | Remove Airfoil details Airfoil plotter |
(ua79sff-il) UNIVERSITY OF ALBERTA UA 79-SF-187 AIRFOIL MAIN ELEMENT | University of Alberta/Marsden UA 79-SF-187 sailplane airfoil FLAP Max thickness 8.7% at 73.1% chord Max camber 3.4% at 78.1% chord | Remove Airfoil details Airfoil plotter |
(n6409-il) NACA6409 9% | NACA 6409 Max thickness 9% at 29.3% chord Max camber 6% at 39.6% chord | Remove Airfoil details Airfoil plotter |
(naca23024-il) NACA 23024 | NACA 23024 airfoil Max thickness 24% at 30.3% chord Max camber 2.9% at 1.3% chord | Remove Airfoil details Airfoil plotter |
(n63012a-il) NACA 63012A AIRFOIL | NACA 63-012A airfoil Max thickness 12% at 35% chord Max camber 0% at 0% chord | Remove Airfoil details Airfoil plotter |
(usa29-il) USA 29 AIRFOIL | USA-29 airfoil Max thickness 13.2% at 29.7% chord Max camber 5.5% at 39.7% chord | Remove Airfoil details Airfoil plotter |
(vr11x-il) BOEING-VERTOL VR-11X AIRFOIL | Boeing-Vertol/NASA/Dadone VR-11X transonic rotorcraft airfoil Max thickness 11% at 40% chord Max camber 2.4% at 25% chord | Remove Airfoil details Airfoil plotter |
(oaf128-il) OAF128 AIRFOIL | ONERA/Aerospatiale OAF128 Fenestron airfoil Max thickness 12.8% at 23.2% chord Max camber 1% at 43.7% chord | Remove Airfoil details Airfoil plotter |
(uag8814320-il) UAG 88-143/20 | UAG 88-143/20 airfoil Max thickness 14.3% at 43.5% chord Max camber 6.2% at 46.7% chord | Remove Airfoil details Airfoil plotter |
(pt40-il) PT40 | Great Plane PT-40 trainer airfoil Max thickness 11.6% at 27.1% chord Max camber 2.9% at 41.6% chord | Remove Airfoil details Airfoil plotter |
(ua2-180-il) UA(2)-180 (University of Alberta/Marsden) | UA(2)-180 airfoil for ultralight category aircraft Max thickness 18.1% at 31.5% chord Max camber 7% at 36.6% chord | Remove Airfoil details Airfoil plotter |
(kc135b-il) KC-135 BL124.32 AIRFOIL | Boeing KC-135 transonic airfoils Max thickness 13% at 40% chord Max camber 1.4% at 20% chord | Remove Airfoil details Airfoil plotter |
(s1046-il) S1046 17% (Danny Howell) | Selig S1046 airfoil Max thickness 17% at 30.8% chord Max camber 0% at 0% chord | Remove Airfoil details Airfoil plotter |
(kc135a-il) KC-135 BL52.44 AIRFOIL | Boeing KC-135 transonic airfoils Max thickness 15.5% at 35% chord Max camber 1.3% at 20% chord | Remove Airfoil details Airfoil plotter |
(rae104-il) RAE 104 AIRFOIL | RAE 104 airfoil Max thickness 10% at 42% chord Max camber 0% at 0% chord | Remove Airfoil details Airfoil plotter |
(n64008a-il) NACA 64-008A AIRFOIL | NACA 64-008A airfoil Max thickness 8% at 40% chord Max camber 0% at 0% chord | Remove Airfoil details Airfoil plotter |
Drawing Options
Polars for (ua79sf18-il,fx05h126-il,v43012-il,naca23021-il,boe106-il,daytonwright6-il,fx049915-il,v23010-il,v43015-il,ua2-180sm-il,usa31-il,isa571-il,naca23012-il,defcnd3-il,wb140-il,defcnd1-il,wb13535sm-il,ua79sfm-il,clarky-il,isa962-il,e1200-il,gm15sm-il,boe103-il,geminism-il,raf25-il,fx05188-il,m25-il,naca23018-il,ua79sff-il,n6409-il,naca23024-il,n63012a-il,usa29-il,vr11x-il,oaf128-il,uag8814320-il,pt40-il,ua2-180-il,kc135b-il,s1046-il,kc135a-il,rae104-il,n64008a-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| ua79sf18-il | 50,000 | 9 | 15 at α=13° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ua79sf18-il | 50,000 | 5 | 15.2 at α=11.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ua79sf18-il | 100,000 | 9 | 24.8 at α=10.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ua79sf18-il | 100,000 | 5 | 23.1 at α=9.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ua79sf18-il | 200,000 | 9 | 37.2 at α=8.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ua79sf18-il | 200,000 | 5 | 35 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ua79sf18-il | 500,000 | 9 | 65 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ua79sf18-il | 500,000 | 5 | 75.9 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ua79sf18-il | 1,000,000 | 9 | 133.3 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ua79sf18-il | 1,000,000 | 5 | 114.1 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx05h126-il | 50,000 | 9 | 19.1 at α=13.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx05h126-il | 50,000 | 5 | 14.5 at α=12.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx05h126-il | 100,000 | 9 | 25.1 at α=11.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx05h126-il | 100,000 | 5 | 24.3 at α=11° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx05h126-il | 200,000 | 9 | 66.3 at α=9.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx05h126-il | 200,000 | 5 | 70.8 at α=8.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx05h126-il | 500,000 | 9 | 121.3 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx05h126-il | 500,000 | 5 | 116.3 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx05h126-il | 1,000,000 | 9 | 158.3 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx05h126-il | 1,000,000 | 5 | 145.9 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| v43012-il | 50,000 | 9 | 24 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| v43012-il | 50,000 | 5 | 28.2 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| v43012-il | 100,000 | 9 | 36.3 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| v43012-il | 100,000 | 5 | 40.6 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| v43012-il | 200,000 | 9 | 50.5 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| v43012-il | 200,000 | 5 | 55.9 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| v43012-il | 500,000 | 9 | 77.7 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| v43012-il | 500,000 | 5 | 81.1 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| v43012-il | 1,000,000 | 9 | 102.9 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| v43012-il | 1,000,000 | 5 | 101.3 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca23021-il | 50,000 | 9 | 18.6 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca23021-il | 50,000 | 5 | 24.8 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca23021-il | 100,000 | 9 | 37 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca23021-il | 100,000 | 5 | 35.7 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca23021-il | 200,000 | 9 | 49.1 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca23021-il | 200,000 | 5 | 42.7 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca23021-il | 500,000 | 9 | 56.4 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca23021-il | 500,000 | 5 | 50.5 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca23021-il | 1,000,000 | 9 | 64.3 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca23021-il | 1,000,000 | 5 | 55.8 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| boe106-il | 50,000 | 9 | 29.7 at α=10.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| boe106-il | 50,000 | 5 | 32.5 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| boe106-il | 100,000 | 9 | 51.6 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| boe106-il | 100,000 | 5 | 52.8 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| boe106-il | 200,000 | 9 | 72.1 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| boe106-il | 200,000 | 5 | 70.2 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| boe106-il | 500,000 | 9 | 98.8 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| boe106-il | 500,000 | 5 | 92 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| boe106-il | 1,000,000 | 9 | 118.8 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| boe106-il | 1,000,000 | 5 | 108.2 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| daytonwright6-il | 50,000 | 9 | 11 at α=1° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| daytonwright6-il | 50,000 | 5 | 31.1 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| daytonwright6-il | 100,000 | 9 | 45.6 at α=2° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| daytonwright6-il | 100,000 | 5 | 49.7 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| daytonwright6-il | 200,000 | 9 | 66.8 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| daytonwright6-il | 200,000 | 5 | 66.4 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| daytonwright6-il | 500,000 | 9 | 92.6 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| daytonwright6-il | 500,000 | 5 | 89.6 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| daytonwright6-il | 1,000,000 | 9 | 115.8 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| daytonwright6-il | 1,000,000 | 5 | 111.2 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx049915-il | 50,000 | 9 | 4.9 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx049915-il | 50,000 | 5 | 10.4 at α=0.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx049915-il | 100,000 | 9 | 6.2 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx049915-il | 100,000 | 5 | 24.1 at α=1.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx049915-il | 200,000 | 9 | 25.4 at α=1.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx049915-il | 200,000 | 5 | 49.2 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx049915-il | 500,000 | 9 | 113.5 at α=10.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx049915-il | 500,000 | 5 | 114.6 at α=9.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx049915-il | 1,000,000 | 9 | 155 at α=9.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx049915-il | 1,000,000 | 5 | 152.6 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| v23010-il | 50,000 | 9 | 23.8 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| v23010-il | 50,000 | 5 | 27.9 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| v23010-il | 100,000 | 9 | 35.1 at α=10.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| v23010-il | 100,000 | 5 | 41.2 at α=9.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| v23010-il | 200,000 | 9 | 54.2 at α=9.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| v23010-il | 200,000 | 5 | 57.7 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| v23010-il | 500,000 | 9 | 79.9 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| v23010-il | 500,000 | 5 | 78 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| v23010-il | 1,000,000 | 9 | 97.6 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| v23010-il | 1,000,000 | 5 | 94.1 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| v43015-il | 50,000 | 9 | 23.5 at α=1.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| v43015-il | 50,000 | 5 | 27.1 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| v43015-il | 100,000 | 9 | 36.3 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| v43015-il | 100,000 | 5 | 39.8 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| v43015-il | 200,000 | 9 | 51.4 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| v43015-il | 200,000 | 5 | 53.5 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| v43015-il | 500,000 | 9 | 74.6 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| v43015-il | 500,000 | 5 | 76.7 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| v43015-il | 1,000,000 | 9 | 98.2 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| v43015-il | 1,000,000 | 5 | 95 at α=9.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ua2-180sm-il | 50,000 | 9 | 3.9 at α=11.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ua2-180sm-il | 50,000 | 5 | 6.5 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ua2-180sm-il | 100,000 | 9 | 4.9 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ua2-180sm-il | 100,000 | 5 | 23.7 at α=2.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ua2-180sm-il | 200,000 | 9 | 27.9 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ua2-180sm-il | 200,000 | 5 | 55.9 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ua2-180sm-il | 500,000 | 9 | 102.9 at α=9.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ua2-180sm-il | 500,000 | 5 | 106.8 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ua2-180sm-il | 1,000,000 | 9 | 146.4 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ua2-180sm-il | 1,000,000 | 5 | 145.3 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| usa31-il | 50,000 | 9 | 4.9 at α=8.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| usa31-il | 50,000 | 5 | 14.1 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| usa31-il | 100,000 | 9 | 34.9 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| usa31-il | 100,000 | 5 | 40.8 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| usa31-il | 200,000 | 9 | 62.3 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| usa31-il | 200,000 | 5 | 54.8 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| usa31-il | 500,000 | 9 | 76.8 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| usa31-il | 500,000 | 5 | 69.2 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| usa31-il | 1,000,000 | 9 | 88.2 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| usa31-il | 1,000,000 | 5 | 79.9 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| isa571-il | 50,000 | 9 | 35.4 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| isa571-il | 50,000 | 5 | 39.4 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| isa571-il | 100,000 | 9 | 51.6 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| isa571-il | 100,000 | 5 | 54.3 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| isa571-il | 200,000 | 9 | 69.6 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| isa571-il | 200,000 | 5 | 70.6 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| isa571-il | 500,000 | 9 | 93.6 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| isa571-il | 500,000 | 5 | 89.1 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| isa571-il | 1,000,000 | 9 | 109.4 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| isa571-il | 1,000,000 | 5 | 100.5 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca23012-il | 50,000 | 9 | 24.2 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca23012-il | 50,000 | 5 | 28.3 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca23012-il | 100,000 | 9 | 36.4 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca23012-il | 100,000 | 5 | 40.5 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca23012-il | 200,000 | 9 | 51 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca23012-il | 200,000 | 5 | 55.4 at α=8.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca23012-il | 500,000 | 9 | 77.1 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca23012-il | 500,000 | 5 | 77.2 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca23012-il | 1,000,000 | 9 | 96.8 at α=8.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca23012-il | 1,000,000 | 5 | 93.7 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| defcnd3-il | 50,000 | 9 | 25.6 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| defcnd3-il | 50,000 | 5 | 32.7 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| defcnd3-il | 100,000 | 9 | 44.6 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| defcnd3-il | 100,000 | 5 | 46.8 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| defcnd3-il | 200,000 | 9 | 60.8 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| defcnd3-il | 200,000 | 5 | 61.1 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| defcnd3-il | 500,000 | 9 | 85 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| defcnd3-il | 500,000 | 5 | 81.7 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| defcnd3-il | 1,000,000 | 9 | 103.8 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| defcnd3-il | 1,000,000 | 5 | 97.2 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| wb140-il | 50,000 | 9 | 9.9 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| wb140-il | 50,000 | 5 | 31.9 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| wb140-il | 100,000 | 9 | 53.4 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| wb140-il | 100,000 | 5 | 52.9 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| wb140-il | 200,000 | 9 | 83.9 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| wb140-il | 200,000 | 5 | 62.2 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| wb140-il | 500,000 | 9 | 105.9 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| wb140-il | 500,000 | 5 | 64 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| wb140-il | 1,000,000 | 9 | 109.3 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| wb140-il | 1,000,000 | 5 | 74.9 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| defcnd1-il | 50,000 | 9 | 3 at α=10.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| defcnd1-il | 50,000 | 5 | 6.1 at α=2.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| defcnd1-il | 100,000 | 9 | 4.6 at α=2.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| defcnd1-il | 100,000 | 5 | 32.3 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| defcnd1-il | 200,000 | 9 | 52.8 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| defcnd1-il | 200,000 | 5 | 60.1 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| defcnd1-il | 500,000 | 9 | 93.7 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| defcnd1-il | 500,000 | 5 | 92.4 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| defcnd1-il | 1,000,000 | 9 | 124.9 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| defcnd1-il | 1,000,000 | 5 | 116.6 at α=8° | 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 | |
| ua79sfm-il | 50,000 | 9 | 12.2 at α=17.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ua79sfm-il | 50,000 | 5 | 16.3 at α=14.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ua79sfm-il | 100,000 | 9 | 41.3 at α=11.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ua79sfm-il | 100,000 | 5 | 40.2 at α=11° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ua79sfm-il | 200,000 | 9 | 82.6 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ua79sfm-il | 200,000 | 5 | 80 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ua79sfm-il | 500,000 | 9 | 145.9 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ua79sfm-il | 500,000 | 5 | 142.4 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ua79sfm-il | 1,000,000 | 9 | 291 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ua79sfm-il | 1,000,000 | 5 | 241.4 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| clarky-il | 50,000 | 9 | 29.6 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| clarky-il | 50,000 | 5 | 36.5 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| clarky-il | 100,000 | 9 | 53 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| clarky-il | 100,000 | 5 | 54.1 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| clarky-il | 200,000 | 9 | 73.2 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| clarky-il | 200,000 | 5 | 69.7 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| clarky-il | 500,000 | 9 | 98.7 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| clarky-il | 500,000 | 5 | 90.9 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| clarky-il | 1,000,000 | 9 | 114.8 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| clarky-il | 1,000,000 | 5 | 108.5 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| isa962-il | 50,000 | 9 | 36.2 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| isa962-il | 50,000 | 5 | 39.4 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| isa962-il | 100,000 | 9 | 57.5 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| isa962-il | 100,000 | 5 | 56.1 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| isa962-il | 200,000 | 9 | 77.1 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| isa962-il | 200,000 | 5 | 69.8 at α=2° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| isa962-il | 500,000 | 9 | 98.7 at α=1.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| isa962-il | 500,000 | 5 | 88.3 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| isa962-il | 1,000,000 | 9 | 111.8 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| isa962-il | 1,000,000 | 5 | 102.5 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 | |
| gm15sm-il | 50,000 | 9 | 45.2 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| gm15sm-il | 50,000 | 5 | 46.1 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| gm15sm-il | 100,000 | 9 | 66.2 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| gm15sm-il | 100,000 | 5 | 66.9 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| gm15sm-il | 200,000 | 9 | 91.5 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| gm15sm-il | 200,000 | 5 | 86.9 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| gm15sm-il | 500,000 | 9 | 123.6 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| gm15sm-il | 500,000 | 5 | 112.4 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| gm15sm-il | 1,000,000 | 9 | 146.5 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| gm15sm-il | 1,000,000 | 5 | 119.5 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| boe103-il | 50,000 | 9 | 32.6 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| boe103-il | 50,000 | 5 | 35 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| boe103-il | 100,000 | 9 | 53.1 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| boe103-il | 100,000 | 5 | 52.1 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| boe103-il | 200,000 | 9 | 72 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| boe103-il | 200,000 | 5 | 66.6 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| boe103-il | 500,000 | 9 | 94.6 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| boe103-il | 500,000 | 5 | 81.1 at α=2.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| boe103-il | 1,000,000 | 9 | 107.9 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| boe103-il | 1,000,000 | 5 | 89 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| geminism-il | 50,000 | 9 | 8.9 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| geminism-il | 50,000 | 5 | 28.3 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| geminism-il | 100,000 | 9 | 47.3 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| geminism-il | 100,000 | 5 | 48.6 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| geminism-il | 200,000 | 9 | 66.9 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| geminism-il | 200,000 | 5 | 65.4 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| geminism-il | 500,000 | 9 | 92.7 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| geminism-il | 500,000 | 5 | 86.7 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| geminism-il | 1,000,000 | 9 | 110.6 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| geminism-il | 1,000,000 | 5 | 100.1 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| raf25-il | 50,000 | 9 | 28.3 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| raf25-il | 50,000 | 5 | 30.6 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| raf25-il | 100,000 | 9 | 43.3 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| raf25-il | 100,000 | 5 | 40.2 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| raf25-il | 200,000 | 9 | 56.2 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| raf25-il | 200,000 | 5 | 47.8 at α=2.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| raf25-il | 500,000 | 9 | 68.2 at α=2° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| raf25-il | 500,000 | 5 | 55.7 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| raf25-il | 1,000,000 | 9 | 72.2 at α=1.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| raf25-il | 1,000,000 | 5 | 68.1 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx05188-il | 50,000 | 9 | 17.1 at α=14.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx05188-il | 50,000 | 5 | 14.2 at α=13° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx05188-il | 100,000 | 9 | 27.8 at α=11.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx05188-il | 100,000 | 5 | 29.4 at α=9° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx05188-il | 200,000 | 9 | 60.5 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx05188-il | 200,000 | 5 | 64.5 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx05188-il | 500,000 | 9 | 99.5 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx05188-il | 500,000 | 5 | 97.8 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx05188-il | 1,000,000 | 9 | 126.9 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx05188-il | 1,000,000 | 5 | 117.9 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| m25-il | 50,000 | 9 | 6.8 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| m25-il | 50,000 | 5 | 20.5 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| m25-il | 100,000 | 9 | 53.9 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| m25-il | 100,000 | 5 | 54.3 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| m25-il | 200,000 | 9 | 78.4 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| m25-il | 200,000 | 5 | 78.5 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| m25-il | 500,000 | 9 | 102.3 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| m25-il | 500,000 | 5 | 94.5 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| m25-il | 1,000,000 | 9 | 111.9 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| m25-il | 1,000,000 | 5 | 107.8 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca23018-il | 50,000 | 9 | 21.1 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca23018-il | 50,000 | 5 | 26.2 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca23018-il | 100,000 | 9 | 36.1 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca23018-il | 100,000 | 5 | 38.2 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca23018-il | 200,000 | 9 | 50 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca23018-il | 200,000 | 5 | 50.8 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca23018-il | 500,000 | 9 | 71.3 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca23018-il | 500,000 | 5 | 70 at α=9.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca23018-il | 1,000,000 | 9 | 89.9 at α=9.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca23018-il | 1,000,000 | 5 | 84.6 at α=9° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ua79sff-il | 50,000 | 9 | 3.4 at α=19.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ua79sff-il | 50,000 | 5 | 3.5 at α=19.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ua79sff-il | 100,000 | 9 | 3.6 at α=19.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ua79sff-il | 100,000 | 5 | 4.1 at α=18.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ua79sff-il | 200,000 | 9 | 3.8 at α=19.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ua79sff-il | 200,000 | 5 | 5.1 at α=13.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ua79sff-il | 500,000 | 9 | 6.4 at α=13.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ua79sff-il | 500,000 | 5 | 25.9 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ua79sff-il | 1,000,000 | 9 | 60.5 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ua79sff-il | 1,000,000 | 5 | 62 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n6409-il | 50,000 | 9 | 27.1 at α=10.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n6409-il | 50,000 | 5 | 36 at α=9° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n6409-il | 100,000 | 9 | 61.6 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n6409-il | 100,000 | 5 | 63.7 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n6409-il | 200,000 | 9 | 87.1 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n6409-il | 200,000 | 5 | 87.4 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n6409-il | 500,000 | 9 | 122.4 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n6409-il | 500,000 | 5 | 118.6 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n6409-il | 1,000,000 | 9 | 151 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n6409-il | 1,000,000 | 5 | 144.3 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca23024-il | 50,000 | 9 | 16.3 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca23024-il | 50,000 | 5 | 19.9 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca23024-il | 100,000 | 9 | 34.2 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca23024-il | 100,000 | 5 | 28.5 at α=9.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca23024-il | 200,000 | 9 | 41.3 at α=9.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca23024-il | 200,000 | 5 | 33.2 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca23024-il | 500,000 | 9 | 44.5 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca23024-il | 500,000 | 5 | 43.4 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca23024-il | 1,000,000 | 9 | 56.9 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca23024-il | 1,000,000 | 5 | 54.4 at α=9.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n63012a-il | 50,000 | 9 | 28.9 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n63012a-il | 50,000 | 5 | 28.1 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n63012a-il | 100,000 | 9 | 41.3 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n63012a-il | 100,000 | 5 | 38.3 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n63012a-il | 200,000 | 9 | 52 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n63012a-il | 200,000 | 5 | 41.9 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n63012a-il | 500,000 | 9 | 58.1 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n63012a-il | 500,000 | 5 | 54.2 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n63012a-il | 1,000,000 | 9 | 64.7 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n63012a-il | 1,000,000 | 5 | 66.6 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| usa29-il | 50,000 | 9 | 6.6 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| usa29-il | 50,000 | 5 | 27.1 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| usa29-il | 100,000 | 9 | 50.4 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| usa29-il | 100,000 | 5 | 52.4 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| usa29-il | 200,000 | 9 | 74.6 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| usa29-il | 200,000 | 5 | 72.6 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| usa29-il | 500,000 | 9 | 90 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| usa29-il | 500,000 | 5 | 80.7 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| usa29-il | 1,000,000 | 9 | 101.1 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| usa29-il | 1,000,000 | 5 | 95.5 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| vr11x-il | 50,000 | 9 | 30.5 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| vr11x-il | 50,000 | 5 | 29.4 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| vr11x-il | 100,000 | 9 | 41 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| vr11x-il | 100,000 | 5 | 39.5 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| vr11x-il | 200,000 | 9 | 55.4 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| vr11x-il | 200,000 | 5 | 51.6 at α=8.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| vr11x-il | 500,000 | 9 | 71.7 at α=9.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| vr11x-il | 500,000 | 5 | 73.2 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| vr11x-il | 1,000,000 | 9 | 92.3 at α=8.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| vr11x-il | 1,000,000 | 5 | 89.6 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| oaf128-il | 50,000 | 9 | 24.7 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| oaf128-il | 50,000 | 5 | 31.1 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| oaf128-il | 100,000 | 9 | 41.4 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| oaf128-il | 100,000 | 5 | 43.5 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| oaf128-il | 200,000 | 9 | 56.5 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| oaf128-il | 200,000 | 5 | 55.5 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| oaf128-il | 500,000 | 9 | 74.1 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| oaf128-il | 500,000 | 5 | 71 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| oaf128-il | 1,000,000 | 9 | 85.4 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| oaf128-il | 1,000,000 | 5 | 85.2 at α=9° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| uag8814320-il | 50,000 | 9 | 5.5 at α=10.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| uag8814320-il | 50,000 | 5 | 15.3 at α=13.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| uag8814320-il | 100,000 | 9 | 32 at α=11.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| uag8814320-il | 100,000 | 5 | 30.3 at α=11° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| uag8814320-il | 200,000 | 9 | 55.1 at α=9.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| uag8814320-il | 200,000 | 5 | 53.2 at α=8.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| uag8814320-il | 500,000 | 9 | 127 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| uag8814320-il | 500,000 | 5 | 123.9 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| uag8814320-il | 1,000,000 | 9 | 185.1 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| uag8814320-il | 1,000,000 | 5 | 169.3 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| pt40-il | 50,000 | 9 | 32.1 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| pt40-il | 50,000 | 5 | 33.4 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| pt40-il | 100,000 | 9 | 48.8 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| pt40-il | 100,000 | 5 | 46.3 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| pt40-il | 200,000 | 9 | 64.3 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| pt40-il | 200,000 | 5 | 57.5 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| pt40-il | 500,000 | 9 | 78.8 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| pt40-il | 500,000 | 5 | 76.1 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| pt40-il | 1,000,000 | 9 | 95 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| pt40-il | 1,000,000 | 5 | 89.2 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ua2-180-il | 50,000 | 9 | 3.9 at α=11.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ua2-180-il | 50,000 | 5 | 6.6 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ua2-180-il | 100,000 | 9 | 5 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ua2-180-il | 100,000 | 5 | 23.8 at α=2.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ua2-180-il | 200,000 | 9 | 30.2 at α=2.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ua2-180-il | 200,000 | 5 | 55.8 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ua2-180-il | 500,000 | 9 | 103.9 at α=9.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ua2-180-il | 500,000 | 5 | 107 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ua2-180-il | 1,000,000 | 9 | 146.2 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ua2-180-il | 1,000,000 | 5 | 139.6 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| kc135b-il | 50,000 | 9 | 31.1 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| kc135b-il | 50,000 | 5 | 31.8 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| kc135b-il | 100,000 | 9 | 50.3 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| kc135b-il | 100,000 | 5 | 49.3 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| kc135b-il | 200,000 | 9 | 70.7 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| kc135b-il | 200,000 | 5 | 62.8 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| kc135b-il | 500,000 | 9 | 89.2 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| kc135b-il | 500,000 | 5 | 71.2 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| kc135b-il | 1,000,000 | 9 | 98.2 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| kc135b-il | 1,000,000 | 5 | 79.8 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s1046-il | 50,000 | 9 | 16.2 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s1046-il | 50,000 | 5 | 25.3 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s1046-il | 100,000 | 9 | 37.2 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s1046-il | 100,000 | 5 | 40.5 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s1046-il | 200,000 | 9 | 55 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s1046-il | 200,000 | 5 | 54.6 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s1046-il | 500,000 | 9 | 77 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s1046-il | 500,000 | 5 | 70.4 at α=9° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s1046-il | 1,000,000 | 9 | 90.9 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s1046-il | 1,000,000 | 5 | 80.9 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| kc135a-il | 50,000 | 9 | 24.9 at α=10.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| kc135a-il | 50,000 | 5 | 27.7 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| kc135a-il | 100,000 | 9 | 47.3 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| kc135a-il | 100,000 | 5 | 47.5 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| kc135a-il | 200,000 | 9 | 68.9 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| kc135a-il | 200,000 | 5 | 62.1 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| kc135a-il | 500,000 | 9 | 88.7 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| kc135a-il | 500,000 | 5 | 73.2 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| kc135a-il | 1,000,000 | 9 | 97.8 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| kc135a-il | 1,000,000 | 5 | 82.5 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rae104-il | 50,000 | 9 | 24.6 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rae104-il | 50,000 | 5 | 26.2 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rae104-il | 100,000 | 9 | 39.8 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rae104-il | 100,000 | 5 | 33.4 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rae104-il | 200,000 | 9 | 44.8 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rae104-il | 200,000 | 5 | 36.7 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rae104-il | 500,000 | 9 | 52.1 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rae104-il | 500,000 | 5 | 49.7 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rae104-il | 1,000,000 | 9 | 58.1 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rae104-il | 1,000,000 | 5 | 61.9 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n64008a-il | 50,000 | 9 | 19.1 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n64008a-il | 50,000 | 5 | 23.3 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n64008a-il | 100,000 | 9 | 32.5 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n64008a-il | 100,000 | 5 | 30.1 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n64008a-il | 200,000 | 9 | 41 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n64008a-il | 200,000 | 5 | 35 at α=2.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n64008a-il | 500,000 | 9 | 46.5 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n64008a-il | 500,000 | 5 | 44.5 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n64008a-il | 1,000,000 | 9 | 49.9 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n64008a-il | 1,000,000 | 5 | 59.4 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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