LDS-2 AIRFOIL (lds2-il)
LDS-2 AIRFOIL - LDS-2 airfoil
| Details | Dat file | Parser | |
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(lds2-il) LDS-2 AIRFOIL LDS-2 airfoil Max thickness 12% at 34.9% chord. Max camber 2.2% at 45% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
LDS-2 AIRFOIL
29. 29.
0.000000 0.000000
0.002000 0.009474
0.005000 0.014580
0.012500 0.022728
0.025000 0.031500
0.037500 0.037762
0.050000 0.042726
0.075000 0.050484
0.100000 0.056496
0.125000 0.061386
0.150000 0.065400
0.175000 0.068800
0.200000 0.071660
0.250000 0.076000
0.300000 0.078760
0.348800 0.080320
0.399200 0.080180
0.449600 0.078800
0.500000 0.075742
0.550300 0.071270
0.600600 0.065628
0.650800 0.059006
0.700900 0.051586
0.750500 0.043616
0.800800 0.035078
0.850700 0.026352
0.900500 0.017584
0.950200 0.008912
1.000000 0.000000
0.000000 0.000000
0.002000 -0.005484
0.005000 -0.008754
0.012500 -0.013108
0.025000 -0.017282
0.037500 -0.020250
0.050000 -0.022680
0.075000 -0.026610
0.100000 -0.029720
0.125000 -0.032260
0.150000 -0.034368
0.175000 -0.036120
0.200000 -0.037440
0.250000 -0.039360
0.300000 -0.039900
0.348800 -0.039420
0.399200 -0.037900
0.449600 -0.035574
0.500000 -0.032588
0.550300 -0.029338
0.600600 -0.025976
0.650800 -0.022670
0.700900 -0.019420
0.750500 -0.016202
0.800800 -0.012994
0.850700 -0.009776
0.900500 -0.006536
0.950200 -0.003272
1.000000 0.000000
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Polars for LDS-2 AIRFOIL (lds2-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| lds2-il | 50,000 | 9 | 34 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| lds2-il | 50,000 | 5 | 33.3 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| lds2-il | 100,000 | 9 | 52.7 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| lds2-il | 100,000 | 5 | 50.3 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| lds2-il | 200,000 | 9 | 72.7 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| lds2-il | 200,000 | 5 | 66.3 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| lds2-il | 500,000 | 9 | 97.7 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| lds2-il | 500,000 | 5 | 77.6 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| lds2-il | 1,000,000 | 9 | 106.5 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| lds2-il | 1,000,000 | 5 | 85.5 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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