NACA M27 AIRFOIL (m27-il)
NACA M27 AIRFOIL - NACA/Munk M-27 airfoil
| Details | Dat file | Parser | |
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(m27-il) NACA M27 AIRFOIL NACA/Munk M-27 airfoil Max thickness 12% at 30.1% chord. Max camber 8.4% at 30.1% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
NACA M27 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0126100 0.0244500
0.0251600 0.0382900
0.0502600 0.0598800
0.0753300 0.0774800
0.1004000 0.0920700
0.1504900 0.1143500
0.2005600 0.1297400
0.3006200 0.1434100
0.4006000 0.1393800
0.5005300 0.1228500
0.6004200 0.0988200
0.7003100 0.0712900
0.8001900 0.0436600
0.9000800 0.0195300
0.9500400 0.0101100
1.0000000 0.0026000
0.0000000 0.0000000
0.0124500 -.0118500
0.0249500 -.0118100
0.0499700 -.0080100
0.0749900 -.0025200
0.1000100 0.0028700
0.1500500 0.0118500
0.2000800 0.0186400
0.3001000 0.0239100
0.4000900 0.0205800
0.5000500 0.0115500
0.6000000 0.0005200
0.6999600 -.0093100
0.7999300 -.0151400
0.8999400 -.0137700
0.9499600 -.0094800
1.0000000 -.0026000
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Polars for NACA M27 AIRFOIL (m27-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| m27-il | 50,000 | 9 | 4.7 at α=9.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| m27-il | 50,000 | 5 | 9.6 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| m27-il | 100,000 | 9 | 9 at α=0.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| m27-il | 100,000 | 5 | 41.3 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| m27-il | 200,000 | 9 | 62.8 at α=10.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| m27-il | 200,000 | 5 | 70.1 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| m27-il | 500,000 | 9 | 105.5 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| m27-il | 500,000 | 5 | 105 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| m27-il | 1,000,000 | 9 | 135.9 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| m27-il | 1,000,000 | 5 | 126.2 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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