NACA 642-015 AIRFOIL (n64015-il)
NACA 642-015 AIRFOIL - NACA 64(2)-015 airfoil
| Details | Dat file | Parser | |
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(n64015-il) NACA 642-015 AIRFOIL NACA 64(2)-015 airfoil Max thickness 15% at 35% chord. Max camber 0% at 0% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
NACA 642-015 AIRFOIL
26. 26.
0.000000 0.000000
0.005000 0.012080
0.007500 0.014560
0.012500 0.018420
0.025000 0.025280
0.050000 0.035040
0.075000 0.042400
0.100000 0.048420
0.150000 0.057850
0.200000 0.064800
0.250000 0.069850
0.300000 0.073190
0.350000 0.074820
0.400000 0.074730
0.450000 0.072240
0.500000 0.068100
0.550000 0.062660
0.600000 0.056200
0.650000 0.048950
0.700000 0.041130
0.750000 0.032960
0.800000 0.024720
0.850000 0.016770
0.900000 0.009500
0.950000 0.003460
1.000000 0.000000
0.000000 0.000000
0.005000 -.012080
0.007500 -.014560
0.012500 -.018420
0.025000 -.025280
0.050000 -.035040
0.075000 -.042400
0.100000 -.048420
0.150000 -.057850
0.200000 -.064800
0.250000 -.069850
0.300000 -.073190
0.350000 -.074820
0.400000 -.074730
0.450000 -.072240
0.500000 -.068100
0.550000 -.062660
0.600000 -.056200
0.650000 -.048950
0.700000 -.041130
0.750000 -.032960
0.800000 -.024720
0.850000 -.016770
0.900000 -.009500
0.950000 -.003460
1.000000 0.000000
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Polars for NACA 642-015 AIRFOIL (n64015-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| n64015-il | 50,000 | 9 | 27.6 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n64015-il | 50,000 | 5 | 27 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n64015-il | 100,000 | 9 | 40.3 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n64015-il | 100,000 | 5 | 35.1 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n64015-il | 200,000 | 9 | 48.9 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n64015-il | 200,000 | 5 | 45 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n64015-il | 500,000 | 9 | 65.2 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n64015-il | 500,000 | 5 | 52.6 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n64015-il | 1,000,000 | 9 | 72.4 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n64015-il | 1,000,000 | 5 | 65 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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