NACA 64(1)-212 (n64212-il)
NACA 64(1)-212 - NACA 64(1)-212 airfoil
| Details | Dat file | Parser | |
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(n64212-il) NACA 64(1)-212 NACA 64(1)-212 airfoil Max thickness 12% at 40% chord. Max camber 1.1% at 50% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
NACA 64(1)-212
26.0 26.0
0.0000000 0.0000000
0.0041800 0.0102500
0.0065900 0.0124500
0.0114700 0.0159300
0.0238200 0.0221800
0.0486800 0.0312300
0.0736400 0.0381500
0.0986500 0.0438600
0.1487200 0.0529100
0.1988600 0.0596800
0.2490300 0.0647000
0.2992100 0.0681500
0.3494100 0.0700800
0.3996100 0.0705200
0.4498200 0.0689300
0.5000000 0.0658300
0.5501600 0.0615100
0.6002900 0.0561900
0.6503900 0.0500400
0.7004500 0.0432200
0.7504700 0.0359000
0.8004500 0.0282500
0.8503800 0.0205400
0.9002700 0.0130300
0.9501300 0.0060400
1.0000000 0.0000000
0.0000000 0.0000000
0.0058200 -.0092500
0.0084100 -.0110500
0.0135300 -.0137900
0.0261800 -.0184600
0.0513200 -.0249100
0.0763600 -.0296700
0.1013500 -.0335200
0.1512800 -.0394500
0.2011400 -.0437600
0.2509700 -.0468000
0.3007900 -.0487100
0.3505900 -.0494800
0.4003900 -.0491000
0.4501800 -.0470300
0.5000000 -.0437700
0.5498400 -.0396100
0.5997100 -.0347700
0.6496100 -.0294400
0.6995500 -.0237800
0.7495300 -.0180000
0.7995500 -.0123300
0.8496200 -.0070800
0.8997300 -.0026900
0.9498700 0.0002800
1.0000000 0.0000000
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Polars for NACA 64(1)-212 (n64212-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| n64212-il | 50,000 | 9 | 31.1 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n64212-il | 50,000 | 5 | 31.8 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n64212-il | 100,000 | 9 | 48.2 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n64212-il | 100,000 | 5 | 45.9 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n64212-il | 200,000 | 9 | 65.2 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n64212-il | 200,000 | 5 | 55.9 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n64212-il | 500,000 | 9 | 80.3 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n64212-il | 500,000 | 5 | 67.8 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n64212-il | 1,000,000 | 9 | 91.2 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n64212-il | 1,000,000 | 5 | 73.3 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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