20-32C AIRFOIL (2032c-il)
20-32C AIRFOIL - Dillner 20-32-C low Reynolds number airfoil
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(2032c-il) 20-32C AIRFOIL Dillner 20-32-C low Reynolds number airfoil Max thickness 8% at 20% chord. Max camber 6.9% at 40% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
20-32C AIRFOIL
18. 18.
0.000000 0.000000
0.012500 0.019300
0.025000 0.031700
0.050000 0.051300
0.075000 0.066400
0.100000 0.078000
0.150000 0.093400
0.200000 0.101300
0.250000 0.104400
0.300000 0.104800
0.400000 0.100200
0.500000 0.090500
0.600000 0.077100
0.700000 0.061000
0.800000 0.042800
0.900000 0.022900
0.950000 0.012400
1.000000 0.001600
0.000000 0.000000
0.012500 -0.005000
0.025000 -0.004200
0.050000 -0.001000
0.075000 0.002800
0.100000 0.006800
0.150000 0.014500
0.200000 0.021700
0.250000 0.028200
0.300000 0.033300
0.400000 0.038500
0.500000 0.038600
0.600000 0.035000
0.700000 0.028600
0.800000 0.020200
0.900000 0.010000
0.950000 0.004400
1.000000 -0.001600
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Polars for 20-32C AIRFOIL (2032c-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| 2032c-il | 50,000 | 9 | 31.7 at α=2.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| 2032c-il | 50,000 | 5 | 40.8 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| 2032c-il | 100,000 | 9 | 54.9 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| 2032c-il | 100,000 | 5 | 58.2 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| 2032c-il | 200,000 | 9 | 75.3 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| 2032c-il | 200,000 | 5 | 76.6 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| 2032c-il | 500,000 | 9 | 103.7 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| 2032c-il | 500,000 | 5 | 103.6 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| 2032c-il | 1,000,000 | 9 | 126.8 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| 2032c-il | 1,000,000 | 5 | 124.9 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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