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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(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 |
(v13009-il) BOEING VERTOL V(1.95)3009-1.25 AIRFOIL | Boeing-Vertol V(1.9)3006-1.25 rotorcraft airfoil Max thickness 9% at 30.1% chord Max camber 1.3% at 20.1% 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 |
(clarkw-il) CLARK W AIRFOIL | CLARK W airfoil Max thickness 11.2% at 30% chord Max camber 3.7% at 40% chord | Remove Airfoil details Airfoil plotter |
(rae103-il) RAE 103 AIRFOIL | RAE 103 airfoil Max thickness 10% at 40% chord Max camber 0% at 0% chord | Remove Airfoil details Airfoil plotter |
(rae101-il) RAE 101 AIRFOIL | RAE 101 airfoil Max thickness 10% at 30% chord Max camber 0% at 0% chord | Remove Airfoil details Airfoil plotter |
(waspsm-il) WASP (smoothed) | Mike Fox WASP low Reynolds number airfoil Max thickness 9.4% at 27.1% chord Max camber 3% at 37.9% chord | Remove Airfoil details Airfoil plotter |
(clarkx-il) CLARK X AIRFOIL | CLARK X airfoil Max thickness 11.7% at 30% chord Max camber 3.3% at 40% chord | Remove Airfoil details Airfoil plotter |
(r140sm-il) R140 12.04% (smoothed) | R140 Quickee 500 airfoil (smoothed) Max thickness 12% at 39.3% chord Max camber 0.4% at 39.3% 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 |
(rae102-il) RAE 102 AIRFOIL | RAE 102 airfoil Max thickness 10% at 36% chord Max camber 0% at 0% chord | Remove Airfoil details Airfoil plotter |
(hq1585-il) HQ 1.5/8.5 AIRFOIL | Quabeck HQ 1.5/8.5 R/C sailplane airfoil Max thickness 8.6% at 35% chord Max camber 1.5% at 50% chord | Remove Airfoil details Airfoil plotter |
(cap21c-il) CAP 21 (TraCFoil) | CAP 21 (TraCFoil) airfoil Max thickness 15.6% at 15.7% chord Max camber 0.6% at 23.9% chord | Remove Airfoil details Airfoil plotter |
(hq1012-il) HQ 1.0/12 AIRFOIL | Quabeck HQ 1.0/12 R/C sailplane airfoil Max thickness 12% at 35% chord Max camber 1% at 50% chord | Remove Airfoil details Airfoil plotter |
(hq1510-il) HQ 1.5/10 AIRFOIL | Quabeck HQ 1.5/10 R/C sailplane airfoil Max thickness 10% at 35% chord Max camber 1.5% at 50% chord | Remove Airfoil details Airfoil plotter |
(r1082t-il) RONCZ 1082T VOYAGER TIP OUTER AFT WING AIRFOIL | Roncz 1082T Voyager tip outer aft wing airfoil Max thickness 16% at 40% chord Max camber 3% at 40% chord | Remove Airfoil details Airfoil plotter |
(rae100-il) RAE 100 AIRFOIL | RAE 100 airfoil Max thickness 10% at 26% chord Max camber 0% at 0% chord | Remove Airfoil details Airfoil plotter |
(clarkv-il) CLARK V AIRFOIL | CLARK V airfoil Max thickness 11.6% at 30% chord Max camber 3.4% at 50% chord | Remove Airfoil details Airfoil plotter |
(hq1511-il) HQ 1.5/11 AIRFOIL | Quabeck HQ 1.5/11 R/C sailplane airfoil Max thickness 11% at 33.9% chord Max camber 1.5% at 50% chord | Remove Airfoil details Airfoil plotter |
(hq1010-il) HQ 1.0/10 AIRFOIL | Quabeck HQ 1.0/10 R/C sailplane airfoil Max thickness 10% at 35% chord Max camber 1% at 50% 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 |
(clarkk-il) CLARK K AIRFOIL | CLARK K airfoil Max thickness 11.7% at 29.7% chord Max camber 3.3% at 39.6% chord | Remove Airfoil details Airfoil plotter |
(hq1512-il) HQ 1.5/12 AIRFOIL | Quabeck HQ 1.5/12 R/C sailplane airfoil Max thickness 12% at 35% chord Max camber 1.5% at 50% chord | Remove Airfoil details Airfoil plotter |
(ch10sm-il) CH10 (smoothed) | Chuch Hollinger CH 10-48-13 high lift low Reynolds number airfoil Max thickness 12.8% at 30.6% chord Max camber 10.2% at 49.3% 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 |
(be50sm-il) BE50 (smoothed) | Verbitsky BE50 free flight airfoil (original) Max thickness 7.3% at 23.8% chord Max camber 4% at 45.4% chord | Remove Airfoil details Airfoil plotter |
(la5055-il) LIEBECK LA5055 AIRFOIL | Liebeck high lift airfoil Max thickness 15.9% at 35% chord Max camber 5.9% at 40% chord | Remove Airfoil details Airfoil plotter |
(b29tip-il) B-29 TIP AIRFOIL | Boeing B-29 tip airfoil Max thickness 9% at 30% chord Max camber 2.2% at 30% chord | Remove Airfoil details Airfoil plotter |
(lg10sc-il) LOCKHEED-GEORGIA SUPERCRITICAL AIRFOIL | Lockheed-Georgia/NASA/Blackwell rotorcraft airfoil Max thickness 10% at 32% chord Max camber 1.5% at 16% chord | Remove Airfoil details Airfoil plotter |
(la203a-il) DOUGLAS LA203A AIRFOIL | Douglas/Liebeck LA203A high lift airfoil Max thickness 15.7% at 34.3% chord Max camber 5.5% at 46% chord | Remove Airfoil details Airfoil plotter |
(isa960-il) I.S.A. 960 | I.S.A. 960 airfoil Max thickness 9.5% at 30% chord Max camber 4.5% at 40% 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 |
(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 |
(isa961-il) I.S.A. 961 | I.S.A. 961 airfoil Max thickness 9.3% at 20% chord Max camber 4.6% at 40% chord | Remove Airfoil details Airfoil plotter |
(bacxxx-il) BOEING BACXXX AIRFOIL | Boeing Commercial Airplane Company BACXXX Energy Efficient Transport Program airfoil Max thickness 11.3% at 35% chord Max camber 1.4% at 15% chord | Remove Airfoil details Airfoil plotter |
Drawing Options
Polars for (v43012-il,v13009-il,v43015-il,clarkw-il,rae103-il,rae101-il,waspsm-il,clarkx-il,r140sm-il,rae104-il,rae102-il,hq1585-il,cap21c-il,hq1012-il,hq1510-il,r1082t-il,rae100-il,clarkv-il,hq1511-il,hq1010-il,clarky-il,clarkk-il,hq1512-il,ch10sm-il,isa571-il,be50sm-il,la5055-il,b29tip-il,lg10sc-il,la203a-il,isa960-il,isa962-il,boe103-il,isa961-il,bacxxx-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| 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 | |
| v13009-il | 50,000 | 9 | 26.2 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| v13009-il | 50,000 | 5 | 28.7 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| v13009-il | 100,000 | 9 | 36.6 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| v13009-il | 100,000 | 5 | 39.7 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| v13009-il | 200,000 | 9 | 49.7 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| v13009-il | 200,000 | 5 | 53.7 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| v13009-il | 500,000 | 9 | 72.9 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| v13009-il | 500,000 | 5 | 71.7 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| v13009-il | 1,000,000 | 9 | 88.4 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| v13009-il | 1,000,000 | 5 | 86.4 at α=8° | 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 | |
| clarkw-il | 50,000 | 9 | 32.2 at α=9.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| clarkw-il | 50,000 | 5 | 36.5 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| clarkw-il | 100,000 | 9 | 53.2 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| clarkw-il | 100,000 | 5 | 54.1 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| clarkw-il | 200,000 | 9 | 73.5 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| clarkw-il | 200,000 | 5 | 69.7 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| clarkw-il | 500,000 | 9 | 98.7 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| clarkw-il | 500,000 | 5 | 91.1 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| clarkw-il | 1,000,000 | 9 | 116.1 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| clarkw-il | 1,000,000 | 5 | 107.5 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rae103-il | 50,000 | 9 | 27.8 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rae103-il | 50,000 | 5 | 27.1 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rae103-il | 100,000 | 9 | 40.2 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rae103-il | 100,000 | 5 | 36.5 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rae103-il | 200,000 | 9 | 48.6 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rae103-il | 200,000 | 5 | 39.2 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rae103-il | 500,000 | 9 | 54.8 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rae103-il | 500,000 | 5 | 52.6 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rae103-il | 1,000,000 | 9 | 62.2 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rae103-il | 1,000,000 | 5 | 66 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rae101-il | 50,000 | 9 | 27.9 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rae101-il | 50,000 | 5 | 27.4 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rae101-il | 100,000 | 9 | 39 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rae101-il | 100,000 | 5 | 36.4 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rae101-il | 200,000 | 9 | 49.7 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rae101-il | 200,000 | 5 | 44.2 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rae101-il | 500,000 | 9 | 60.3 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rae101-il | 500,000 | 5 | 56.4 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rae101-il | 1,000,000 | 9 | 67.9 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rae101-il | 1,000,000 | 5 | 70.2 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| waspsm-il | 50,000 | 9 | 31.1 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| waspsm-il | 50,000 | 5 | 37.5 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| waspsm-il | 100,000 | 9 | 51 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| waspsm-il | 100,000 | 5 | 53.2 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| waspsm-il | 200,000 | 9 | 69.7 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| waspsm-il | 200,000 | 5 | 69.1 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| waspsm-il | 500,000 | 9 | 96 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| waspsm-il | 500,000 | 5 | 91 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| waspsm-il | 1,000,000 | 9 | 115.8 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| waspsm-il | 1,000,000 | 5 | 108.1 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| clarkx-il | 50,000 | 9 | 32.9 at α=9.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| clarkx-il | 50,000 | 5 | 36.4 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| clarkx-il | 100,000 | 9 | 54.2 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| clarkx-il | 100,000 | 5 | 55.2 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| clarkx-il | 200,000 | 9 | 76.2 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| clarkx-il | 200,000 | 5 | 72.3 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| clarkx-il | 500,000 | 9 | 103.7 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| clarkx-il | 500,000 | 5 | 92.8 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| clarkx-il | 1,000,000 | 9 | 122.4 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| clarkx-il | 1,000,000 | 5 | 107.9 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| r140sm-il | 50,000 | 9 | 22.8 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| r140sm-il | 50,000 | 5 | 29.4 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| r140sm-il | 100,000 | 9 | 43 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| r140sm-il | 100,000 | 5 | 41.4 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| r140sm-il | 200,000 | 9 | 53.5 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| r140sm-il | 200,000 | 5 | 46.5 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| r140sm-il | 500,000 | 9 | 62 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| r140sm-il | 500,000 | 5 | 53.3 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| r140sm-il | 1,000,000 | 9 | 71.1 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| r140sm-il | 1,000,000 | 5 | 59.8 at α=6.75° | 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 | |
| rae102-il | 50,000 | 9 | 28.4 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rae102-il | 50,000 | 5 | 27.4 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rae102-il | 100,000 | 9 | 39.6 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rae102-il | 100,000 | 5 | 36.7 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rae102-il | 200,000 | 9 | 50.5 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rae102-il | 200,000 | 5 | 41.5 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rae102-il | 500,000 | 9 | 57.2 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rae102-il | 500,000 | 5 | 54.7 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rae102-il | 1,000,000 | 9 | 65.6 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rae102-il | 1,000,000 | 5 | 68.3 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hq1585-il | 50,000 | 9 | 35.6 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hq1585-il | 50,000 | 5 | 35.6 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hq1585-il | 100,000 | 9 | 51.4 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hq1585-il | 100,000 | 5 | 48.4 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hq1585-il | 200,000 | 9 | 67.2 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hq1585-il | 200,000 | 5 | 58.3 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hq1585-il | 500,000 | 9 | 84.7 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hq1585-il | 500,000 | 5 | 67.3 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hq1585-il | 1,000,000 | 9 | 85.3 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hq1585-il | 1,000,000 | 5 | 80.4 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| cap21c-il | 50,000 | 9 | 9.9 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| cap21c-il | 50,000 | 5 | 14.6 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| cap21c-il | 100,000 | 9 | 17.1 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| cap21c-il | 100,000 | 5 | 26 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| cap21c-il | 200,000 | 9 | 38.4 at α=10° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| cap21c-il | 200,000 | 5 | 48.1 at α=11.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| cap21c-il | 500,000 | 9 | 74 at α=10° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| cap21c-il | 500,000 | 5 | 77.6 at α=10.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| cap21c-il | 1,000,000 | 9 | 97.4 at α=9.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| cap21c-il | 1,000,000 | 5 | 97.4 at α=9.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hq1012-il | 50,000 | 9 | 31 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hq1012-il | 50,000 | 5 | 32 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hq1012-il | 100,000 | 9 | 47.1 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hq1012-il | 100,000 | 5 | 45.1 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hq1012-il | 200,000 | 9 | 63.9 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hq1012-il | 200,000 | 5 | 54.9 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hq1012-il | 500,000 | 9 | 75.6 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hq1012-il | 500,000 | 5 | 69.6 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hq1012-il | 1,000,000 | 9 | 87.5 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hq1012-il | 1,000,000 | 5 | 80.6 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hq1510-il | 50,000 | 9 | 34.3 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hq1510-il | 50,000 | 5 | 35.1 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hq1510-il | 100,000 | 9 | 51.3 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hq1510-il | 100,000 | 5 | 49.2 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hq1510-il | 200,000 | 9 | 68.4 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hq1510-il | 200,000 | 5 | 61.9 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hq1510-il | 500,000 | 9 | 88.4 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hq1510-il | 500,000 | 5 | 73.3 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hq1510-il | 1,000,000 | 9 | 92.1 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hq1510-il | 1,000,000 | 5 | 81 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| r1082t-il | 50,000 | 9 | 21.7 at α=12.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| r1082t-il | 50,000 | 5 | 16.5 at α=12.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| r1082t-il | 100,000 | 9 | 34.3 at α=11.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| r1082t-il | 100,000 | 5 | 38.2 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| r1082t-il | 200,000 | 9 | 73.2 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| r1082t-il | 200,000 | 5 | 69.4 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| r1082t-il | 500,000 | 9 | 107.6 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| r1082t-il | 500,000 | 5 | 101.6 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| r1082t-il | 1,000,000 | 9 | 135 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| r1082t-il | 1,000,000 | 5 | 122.4 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rae100-il | 50,000 | 9 | 24.6 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rae100-il | 50,000 | 5 | 26.1 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rae100-il | 100,000 | 9 | 35.3 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rae100-il | 100,000 | 5 | 35.2 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rae100-il | 200,000 | 9 | 46.1 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rae100-il | 200,000 | 5 | 45 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rae100-il | 500,000 | 9 | 60.4 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rae100-il | 500,000 | 5 | 60.9 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rae100-il | 1,000,000 | 9 | 74.1 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rae100-il | 1,000,000 | 5 | 74.8 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| clarkv-il | 50,000 | 9 | 35.5 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| clarkv-il | 50,000 | 5 | 36.4 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| clarkv-il | 100,000 | 9 | 57.6 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| clarkv-il | 100,000 | 5 | 56.3 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| clarkv-il | 200,000 | 9 | 80.9 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| clarkv-il | 200,000 | 5 | 75.2 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| clarkv-il | 500,000 | 9 | 110.4 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| clarkv-il | 500,000 | 5 | 95.6 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| clarkv-il | 1,000,000 | 9 | 129.4 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| clarkv-il | 1,000,000 | 5 | 105.6 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hq1511-il | 50,000 | 9 | 33.2 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hq1511-il | 50,000 | 5 | 34.4 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hq1511-il | 100,000 | 9 | 50.5 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hq1511-il | 100,000 | 5 | 48.4 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hq1511-il | 200,000 | 9 | 67.8 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hq1511-il | 200,000 | 5 | 59.9 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hq1511-il | 500,000 | 9 | 82.2 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hq1511-il | 500,000 | 5 | 74 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hq1511-il | 1,000,000 | 9 | 94.4 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hq1511-il | 1,000,000 | 5 | 82.4 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hq1010-il | 50,000 | 9 | 32.4 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hq1010-il | 50,000 | 5 | 32.9 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hq1010-il | 100,000 | 9 | 47.8 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hq1010-il | 100,000 | 5 | 45.1 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hq1010-il | 200,000 | 9 | 63.1 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hq1010-il | 200,000 | 5 | 55.8 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hq1010-il | 500,000 | 9 | 79.1 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hq1010-il | 500,000 | 5 | 68.2 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hq1010-il | 1,000,000 | 9 | 85.9 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hq1010-il | 1,000,000 | 5 | 78 at α=6.25° | 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 | |
| clarkk-il | 50,000 | 9 | 32.2 at α=10° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| clarkk-il | 50,000 | 5 | 36.4 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| clarkk-il | 100,000 | 9 | 54.1 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| clarkk-il | 100,000 | 5 | 54.7 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| clarkk-il | 200,000 | 9 | 75.7 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| clarkk-il | 200,000 | 5 | 71.5 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| clarkk-il | 500,000 | 9 | 102.7 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| clarkk-il | 500,000 | 5 | 91.3 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| clarkk-il | 1,000,000 | 9 | 121.4 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| clarkk-il | 1,000,000 | 5 | 104.4 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hq1512-il | 50,000 | 9 | 32.3 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hq1512-il | 50,000 | 5 | 33.6 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hq1512-il | 100,000 | 9 | 49.9 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hq1512-il | 100,000 | 5 | 48.4 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hq1512-il | 200,000 | 9 | 67.7 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hq1512-il | 200,000 | 5 | 60.3 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hq1512-il | 500,000 | 9 | 82.1 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hq1512-il | 500,000 | 5 | 73.2 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hq1512-il | 1,000,000 | 9 | 93.9 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hq1512-il | 1,000,000 | 5 | 81.9 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ch10sm-il | 50,000 | 9 | 6.2 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ch10sm-il | 50,000 | 5 | 12.4 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ch10sm-il | 100,000 | 9 | 10.9 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ch10sm-il | 100,000 | 5 | 38.1 at α=2.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ch10sm-il | 200,000 | 9 | 73.2 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ch10sm-il | 200,000 | 5 | 86.2 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ch10sm-il | 500,000 | 9 | 135.4 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ch10sm-il | 500,000 | 5 | 132.4 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ch10sm-il | 1,000,000 | 9 | 175.2 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ch10sm-il | 1,000,000 | 5 | 164 at α=3.75° | 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 | |
| be50sm-il | 50,000 | 9 | 38.9 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| be50sm-il | 50,000 | 5 | 43 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| be50sm-il | 100,000 | 9 | 60.5 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| be50sm-il | 100,000 | 5 | 59.2 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| be50sm-il | 200,000 | 9 | 81.2 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| be50sm-il | 200,000 | 5 | 74.4 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| be50sm-il | 500,000 | 9 | 104.9 at α=2.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| be50sm-il | 500,000 | 5 | 97.8 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| be50sm-il | 1,000,000 | 9 | 121.5 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| be50sm-il | 1,000,000 | 5 | 115.9 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| la5055-il | 50,000 | 9 | 4.9 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| la5055-il | 50,000 | 5 | 8.7 at α=13.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| la5055-il | 100,000 | 9 | 18.7 at α=15.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| la5055-il | 100,000 | 5 | 15.5 at α=13.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| la5055-il | 200,000 | 9 | 24.7 at α=13.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| la5055-il | 200,000 | 5 | 46.1 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| la5055-il | 500,000 | 9 | 116.3 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| la5055-il | 500,000 | 5 | 104.2 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| la5055-il | 1,000,000 | 9 | 149.6 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| la5055-il | 1,000,000 | 5 | 83.5 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| b29tip-il | 50,000 | 9 | 34.1 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| b29tip-il | 50,000 | 5 | 34.8 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| b29tip-il | 100,000 | 9 | 51.1 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| b29tip-il | 100,000 | 5 | 50.9 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| b29tip-il | 200,000 | 9 | 68.8 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| b29tip-il | 200,000 | 5 | 66.4 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| b29tip-il | 500,000 | 9 | 91.4 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| b29tip-il | 500,000 | 5 | 84.3 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| b29tip-il | 1,000,000 | 9 | 106.1 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| b29tip-il | 1,000,000 | 5 | 90 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| lg10sc-il | 50,000 | 9 | 25.9 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| lg10sc-il | 50,000 | 5 | 27.8 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| lg10sc-il | 100,000 | 9 | 35.1 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| lg10sc-il | 100,000 | 5 | 39.1 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| lg10sc-il | 200,000 | 9 | 48.2 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| lg10sc-il | 200,000 | 5 | 53.3 at α=9° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| lg10sc-il | 500,000 | 9 | 73.5 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| lg10sc-il | 500,000 | 5 | 74.6 at α=8.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| lg10sc-il | 1,000,000 | 9 | 92.8 at α=8.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| lg10sc-il | 1,000,000 | 5 | 90.8 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| la203a-il | 50,000 | 9 | 6 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| la203a-il | 50,000 | 5 | 13.7 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| la203a-il | 100,000 | 9 | 30.6 at α=12.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| la203a-il | 100,000 | 5 | 46.5 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| la203a-il | 200,000 | 9 | 82.4 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| la203a-il | 200,000 | 5 | 85.4 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| la203a-il | 500,000 | 9 | 127.7 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| la203a-il | 500,000 | 5 | 124 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| la203a-il | 1,000,000 | 9 | 160.5 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| la203a-il | 1,000,000 | 5 | 151.5 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| isa960-il | 50,000 | 9 | 39.3 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| isa960-il | 50,000 | 5 | 38 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| isa960-il | 100,000 | 9 | 55.9 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| isa960-il | 100,000 | 5 | 49.8 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| isa960-il | 200,000 | 9 | 64.7 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| isa960-il | 200,000 | 5 | 53.7 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| isa960-il | 500,000 | 9 | 68.2 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| isa960-il | 500,000 | 5 | 72.1 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| isa960-il | 1,000,000 | 9 | 90.5 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| isa960-il | 1,000,000 | 5 | 91.6 at α=6.5° | 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 | |
| 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 | |
| isa961-il | 50,000 | 9 | 34.9 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| isa961-il | 50,000 | 5 | 39.5 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| isa961-il | 100,000 | 9 | 55.5 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| isa961-il | 100,000 | 5 | 53.9 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| isa961-il | 200,000 | 9 | 70.4 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| isa961-il | 200,000 | 5 | 63 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| isa961-il | 500,000 | 9 | 80 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| isa961-il | 500,000 | 5 | 75.5 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| isa961-il | 1,000,000 | 9 | 90.6 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| isa961-il | 1,000,000 | 5 | 88.9 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| bacxxx-il | 50,000 | 9 | 31.2 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| bacxxx-il | 50,000 | 5 | 30.8 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| bacxxx-il | 100,000 | 9 | 44 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| bacxxx-il | 100,000 | 5 | 42.7 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| bacxxx-il | 200,000 | 9 | 58.4 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| bacxxx-il | 200,000 | 5 | 55.2 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| bacxxx-il | 500,000 | 9 | 75.2 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| bacxxx-il | 500,000 | 5 | 72.8 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| bacxxx-il | 1,000,000 | 9 | 90.3 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| bacxxx-il | 1,000,000 | 5 | 86.5 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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