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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(rae5215-il) RAE 5215 AIRFOIL | RAE 5215 transonic airfoil Max thickness 9.7% at 35.5% chord Max camber 1.5% at 69.1% chord | Remove Airfoil details Airfoil plotter |
(rae5213-il) RAE(NPL) 5213 AIRFOIL | RAE(NPL) 5213 transonic airfoil Max thickness 10% at 35.5% chord Max camber 1.4% at 69.1% chord | Remove Airfoil details Airfoil plotter |
(rae5212-il) RAE(NPL) 5212 AIRFOIL | RAE(NPL) 5212 transonic airfoil Max thickness 11.9% at 35.5% chord Max camber 1.8% at 69.1% chord | Remove Airfoil details Airfoil plotter |
(rae69ck-il) RAE6-9CK AIRFOIL | RAE6-9CK transonic airfoil Max thickness 12.1% at 37.9% chord Max camber 1.3% at 75.7% chord | Remove Airfoil details Airfoil plotter |
(rae5214-il) RAE 5214 AIRFOIL | RAE 5214 transonic airfoil Max thickness 9.7% at 35.5% chord Max camber 1.4% at 69.1% chord | Remove Airfoil details Airfoil plotter |
(cast102-il) CAST 10-2/DOA 2 AIRFOIL | CAST 10-2/DOA 2 transonic airfoil Max thickness 12.2% at 45.4% chord Max camber 1.5% at 69.4% chord | Remove Airfoil details Airfoil plotter |
(hobiesm-il) HOBIESMO1.DAT | Hobie Hawk airfoil (Hobie Hawk R/C sailplane) Max thickness 8.6% at 25% chord Max camber 3.8% at 45% chord | Remove Airfoil details Airfoil plotter |
(rae2822-il) RAE 2822 AIRFOIL | RAE 2822 transonic airfoil Max thickness 12.1% at 37.9% chord Max camber 1.3% at 75.7% chord | Remove Airfoil details Airfoil plotter |
(b29root-il) B-29 ROOT AIRFOIL | Boeing B-29 root airfoil Max thickness 22% at 30.2% chord Max camber 1.7% at 30.2% chord | Remove Airfoil details Airfoil plotter |
(lrn1007-il) lrn1007 | LRN(1)-1007 low Reynolds number airfoil Max thickness 7.3% at 39.8% chord Max camber 5.9% at 44.6% chord | Remove Airfoil details Airfoil plotter |
(l188tip-il) LOCKHEED L-188 TIP AIRFOIL | Lockheed L-188/P-3 tip airfoil NACA 0012 -1.10 40/1.051 Cli=.4 a=.8 Max thickness 12% at 41.3% chord Max camber 2.7% at 51.7% chord | Remove Airfoil details Airfoil plotter |
(lrn1015-il) NASA LRN 1015 (NASA TM 102840) | LRN 1015 airfoil used on the Northrop Grumman RQ-4 Global Hawk airfoil Max thickness 15.2% at 40% chord Max camber 4.9% at 44% chord | Remove Airfoil details Airfoil plotter |
(lnv109a-il) LNV109A | Douglas/Liebeck LNV109A high lift airfoil Max thickness 13% at 23.5% chord Max camber 6% at 31.5% chord | Remove Airfoil details Airfoil plotter |
(la2573a-il) LA2573A | Liebeck LA2573A airfoil Max thickness 13.7% at 28.8% chord Max camber 3.2% at 26.1% chord | Remove Airfoil details Airfoil plotter |
(pmc19sm-il) PMC19 Smoothed | PMC19 Max thickness 9.2% at 34.2% chord Max camber 2.1% at 17.5% chord | Remove Airfoil details Airfoil plotter |
Drawing Options
Polars for (rae5215-il,rae5213-il,rae5212-il,rae69ck-il,rae5214-il,cast102-il,hobiesm-il,rae2822-il,b29root-il,lrn1007-il,l188tip-il,lrn1015-il,lnv109a-il,la2573a-il,pmc19sm-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| rae5215-il | 50,000 | 9 | 28.5 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rae5215-il | 50,000 | 5 | 26.7 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rae5215-il | 100,000 | 9 | 38 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rae5215-il | 100,000 | 5 | 35.3 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rae5215-il | 200,000 | 9 | 43.8 at α=2° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rae5215-il | 200,000 | 5 | 49.8 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rae5215-il | 500,000 | 9 | 67.4 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rae5215-il | 500,000 | 5 | 68.6 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rae5215-il | 1,000,000 | 9 | 83.2 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rae5215-il | 1,000,000 | 5 | 81.1 at α=9.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rae5213-il | 50,000 | 9 | 29.6 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rae5213-il | 50,000 | 5 | 29.2 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rae5213-il | 100,000 | 9 | 42.7 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rae5213-il | 100,000 | 5 | 35.9 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rae5213-il | 200,000 | 9 | 49.6 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rae5213-il | 200,000 | 5 | 48.7 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rae5213-il | 500,000 | 9 | 65.9 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rae5213-il | 500,000 | 5 | 68.3 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rae5213-il | 1,000,000 | 9 | 83.2 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rae5213-il | 1,000,000 | 5 | 80.6 at α=9.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rae5212-il | 50,000 | 9 | 31.2 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rae5212-il | 50,000 | 5 | 30.4 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rae5212-il | 100,000 | 9 | 47.7 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rae5212-il | 100,000 | 5 | 40.2 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rae5212-il | 200,000 | 9 | 57.8 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rae5212-il | 200,000 | 5 | 48.2 at α=2.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rae5212-il | 500,000 | 9 | 69.8 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rae5212-il | 500,000 | 5 | 63.3 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rae5212-il | 1,000,000 | 9 | 76.4 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rae5212-il | 1,000,000 | 5 | 80.3 at α=10.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rae69ck-il | 50,000 | 9 | 25.4 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rae69ck-il | 50,000 | 5 | 27 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rae69ck-il | 100,000 | 9 | 37.2 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rae69ck-il | 100,000 | 5 | 37.5 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rae69ck-il | 200,000 | 9 | 53.6 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rae69ck-il | 200,000 | 5 | 49.1 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rae69ck-il | 500,000 | 9 | 70.6 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rae69ck-il | 500,000 | 5 | 57.4 at α=2.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rae69ck-il | 1,000,000 | 9 | 79 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rae69ck-il | 1,000,000 | 5 | 69.4 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rae5214-il | 50,000 | 9 | 29.2 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rae5214-il | 50,000 | 5 | 27.5 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rae5214-il | 100,000 | 9 | 40.3 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rae5214-il | 100,000 | 5 | 35.7 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rae5214-il | 200,000 | 9 | 46.4 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rae5214-il | 200,000 | 5 | 49.1 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rae5214-il | 500,000 | 9 | 66.6 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rae5214-il | 500,000 | 5 | 68.4 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rae5214-il | 1,000,000 | 9 | 83.3 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rae5214-il | 1,000,000 | 5 | 80.7 at α=9.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| cast102-il | 50,000 | 9 | 32.8 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| cast102-il | 50,000 | 5 | 30.3 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| cast102-il | 100,000 | 9 | 45.8 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| cast102-il | 100,000 | 5 | 43 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| cast102-il | 200,000 | 9 | 64 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| cast102-il | 200,000 | 5 | 55.6 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| cast102-il | 500,000 | 9 | 85.5 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| cast102-il | 500,000 | 5 | 66.8 at α=2° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| cast102-il | 1,000,000 | 9 | 93.9 at α=2.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| cast102-il | 1,000,000 | 5 | 75.6 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hobiesm-il | 50,000 | 9 | 41.7 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hobiesm-il | 50,000 | 5 | 41.5 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hobiesm-il | 100,000 | 9 | 60.9 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hobiesm-il | 100,000 | 5 | 60.4 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hobiesm-il | 200,000 | 9 | 81.5 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hobiesm-il | 200,000 | 5 | 79 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hobiesm-il | 500,000 | 9 | 110 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hobiesm-il | 500,000 | 5 | 101.9 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hobiesm-il | 1,000,000 | 9 | 130.7 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hobiesm-il | 1,000,000 | 5 | 118.2 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rae2822-il | 50,000 | 9 | 25.4 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rae2822-il | 50,000 | 5 | 27 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rae2822-il | 100,000 | 9 | 37.2 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rae2822-il | 100,000 | 5 | 37.5 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rae2822-il | 200,000 | 9 | 53.6 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rae2822-il | 200,000 | 5 | 49.1 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rae2822-il | 500,000 | 9 | 70.6 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rae2822-il | 500,000 | 5 | 57.4 at α=2.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rae2822-il | 1,000,000 | 9 | 79 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rae2822-il | 1,000,000 | 5 | 69.4 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| b29root-il | 50,000 | 9 | 2.4 at α=10.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| b29root-il | 50,000 | 5 | 8.5 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| b29root-il | 100,000 | 9 | 13.8 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| b29root-il | 100,000 | 5 | 34.6 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| b29root-il | 200,000 | 9 | 58.2 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| b29root-il | 200,000 | 5 | 52.8 at α=9.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| b29root-il | 500,000 | 9 | 77.9 at α=10.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| b29root-il | 500,000 | 5 | 68.8 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| b29root-il | 1,000,000 | 9 | 90.5 at α=9.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| b29root-il | 1,000,000 | 5 | 83.2 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| lrn1007-il | 50,000 | 9 | 30.6 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| lrn1007-il | 50,000 | 5 | 35.7 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| lrn1007-il | 100,000 | 9 | 51.3 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| lrn1007-il | 100,000 | 5 | 55.3 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| lrn1007-il | 200,000 | 9 | 81.7 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| lrn1007-il | 200,000 | 5 | 98.7 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| lrn1007-il | 500,000 | 9 | 125.3 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| lrn1007-il | 500,000 | 5 | 150.8 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| lrn1007-il | 1,000,000 | 9 | 127.3 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| l188tip-il | 50,000 | 9 | 35.1 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| l188tip-il | 50,000 | 5 | 33.4 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| l188tip-il | 100,000 | 9 | 55.4 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| l188tip-il | 100,000 | 5 | 53.2 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| l188tip-il | 200,000 | 9 | 79.3 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| l188tip-il | 200,000 | 5 | 72.9 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| l188tip-il | 500,000 | 9 | 109 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| l188tip-il | 500,000 | 5 | 91.9 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| l188tip-il | 1,000,000 | 9 | 127 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| l188tip-il | 1,000,000 | 5 | 93.6 at α=2.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| lrn1015-il | 50,000 | 9 | 21.9 at α=12.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| lrn1015-il | 50,000 | 5 | 20.2 at α=11° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| lrn1015-il | 100,000 | 9 | 39.8 at α=9.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| lrn1015-il | 100,000 | 5 | 34 at α=9° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| lrn1015-il | 200,000 | 9 | 70.8 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| lrn1015-il | 200,000 | 5 | 72.6 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| lrn1015-il | 500,000 | 9 | 127.7 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| lrn1015-il | 500,000 | 5 | 112.9 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| lrn1015-il | 1,000,000 | 9 | 154.8 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| lrn1015-il | 1,000,000 | 5 | 134.4 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| lnv109a-il | 50,000 | 9 | 5.5 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| lnv109a-il | 50,000 | 5 | 9.8 at α=2.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| lnv109a-il | 100,000 | 9 | 7 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| lnv109a-il | 100,000 | 5 | 23.3 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| lnv109a-il | 200,000 | 9 | 25.5 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| lnv109a-il | 200,000 | 5 | 58.3 at α=9.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| lnv109a-il | 500,000 | 9 | 111.2 at α=11.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| lnv109a-il | 500,000 | 5 | 113.7 at α=10° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| lnv109a-il | 1,000,000 | 9 | 151.5 at α=10° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| lnv109a-il | 1,000,000 | 5 | 149.6 at α=9° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| la2573a-il | 50,000 | 9 | 6.9 at α=-0.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| la2573a-il | 50,000 | 5 | 13.4 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| la2573a-il | 100,000 | 9 | 15.7 at α=14.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| la2573a-il | 100,000 | 5 | 27.9 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| la2573a-il | 200,000 | 9 | 62.3 at α=11.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| la2573a-il | 200,000 | 5 | 64.9 at α=9.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| la2573a-il | 500,000 | 9 | 102.6 at α=9.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| la2573a-il | 500,000 | 5 | 95.3 at α=8.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| la2573a-il | 1,000,000 | 9 | 125.8 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| la2573a-il | 1,000,000 | 5 | 110.9 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| pmc19sm-il | 50,000 | 9 | 28 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| pmc19sm-il | 50,000 | 5 | 32.3 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| pmc19sm-il | 100,000 | 9 | 44.6 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| pmc19sm-il | 100,000 | 5 | 45 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| pmc19sm-il | 200,000 | 9 | 58.9 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| pmc19sm-il | 200,000 | 5 | 57.9 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| pmc19sm-il | 500,000 | 9 | 79 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| pmc19sm-il | 500,000 | 5 | 74 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| pmc19sm-il | 1,000,000 | 9 | 93.8 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| pmc19sm-il | 1,000,000 | 5 | 82.2 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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