NACA M26 AIRFOIL (m26-il)
NACA M26 AIRFOIL - NACA/Munk M-26 airfoil
| Details | Dat file | Parser | |
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(m26-il) NACA M26 AIRFOIL NACA/Munk M-26 airfoil Max thickness 8.3% at 40% chord. Max camber 8.3% at 30% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
NACA M26 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0125200 0.0177800
0.0250400 0.0288600
0.0500700 0.0483300
0.0750900 0.0627900
0.1001100 0.0757600
0.1501300 0.0962900
0.2001600 0.1102000
0.3001700 0.1232800
0.4001600 0.1214400
0.5001500 0.1043000
0.6001100 0.0820600
0.7000800 0.0576200
0.8000500 0.0338800
0.9000200 0.0140400
0.9500100 0.0070700
1.0000000 0.0024000
0.0000000 0.0000000
0.0124900 -.0080200
0.0249900 -.0057300
0.0500000 0.0011300
0.0750100 0.0084900
0.1000200 0.0155600
0.1500400 0.0269900
0.2000500 0.0350200
0.3000600 0.0417800
0.4000500 0.0384400
0.5000400 0.0284000
0.6000200 0.0153600
0.7000000 0.0027200
0.7999900 -.0064200
0.8999900 -.0092600
0.9499900 -.0069300
1.0000000 -.0024000
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Polars for NACA M26 AIRFOIL (m26-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| m26-il | 50,000 | 9 | 6.1 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| m26-il | 50,000 | 5 | 14 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| m26-il | 100,000 | 9 | 16.6 at α=12° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| m26-il | 100,000 | 5 | 41.4 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| m26-il | 200,000 | 9 | 78.7 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| m26-il | 200,000 | 5 | 78.3 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| m26-il | 500,000 | 9 | 115.7 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| m26-il | 500,000 | 5 | 98.7 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| m26-il | 1,000,000 | 9 | 141.1 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| m26-il | 1,000,000 | 5 | 113.7 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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