PMC19 Smoothed (pmc19sm-il)
PMC19 Smoothed - PMC19
| Details | Dat file | Parser | |
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(pmc19sm-il) PMC19 Smoothed PMC19 Max thickness 9.2% at 34.2% chord. Max camber 2.1% at 17.5% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Selig format |
PMC19 Smoothed
1.00000 0.00095
0.99754 0.00124
0.99070 0.00189
0.98037 0.00258
0.96698 0.00325
0.95044 0.00400
0.93064 0.00497
0.90775 0.00627
0.88202 0.00795
0.85370 0.01006
0.82309 0.01260
0.79048 0.01556
0.75616 0.01891
0.72043 0.02258
0.68359 0.02650
0.64594 0.03058
0.60778 0.03476
0.56937 0.03892
0.53099 0.04301
0.49265 0.04694
0.45435 0.05065
0.41638 0.05406
0.37887 0.05707
0.34204 0.05959
0.30609 0.06151
0.27120 0.06271
0.23760 0.06305
0.20549 0.06237
0.17504 0.06049
0.14648 0.05731
0.11999 0.05288
0.09576 0.04739
0.07395 0.04101
0.05468 0.03407
0.03811 0.02717
0.02433 0.02075
0.01338 0.01476
0.00548 0.00905
0.00098 0.00359
0.00000 -0.00011
0.00098 -0.00343
0.00548 -0.00713
0.01338 -0.00959
0.02433 -0.01089
0.03811 -0.01151
0.05468 -0.01198
0.07395 -0.01249
0.09576 -0.01318
0.11999 -0.01423
0.14648 -0.01580
0.17504 -0.01800
0.20549 -0.02073
0.23760 -0.02375
0.27120 -0.02683
0.30609 -0.02977
0.34204 -0.03235
0.37887 -0.03440
0.41638 -0.03576
0.45435 -0.03632
0.49265 -0.03610
0.53099 -0.03514
0.56937 -0.03355
0.60778 -0.03138
0.64594 -0.02872
0.68359 -0.02570
0.72043 -0.02242
0.75616 -0.01903
0.79048 -0.01567
0.82309 -0.01251
0.85370 -0.00969
0.88202 -0.00729
0.90775 -0.00536
0.93064 -0.00390
0.95044 -0.00297
0.96698 -0.00255
0.98037 -0.00232
0.99070 -0.00192
0.99754 -0.00134
1.00000 -0.00103
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Similar airfoils
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Polars for PMC19 Smoothed (pmc19sm-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| pmc19sm-il | 50,000 | 9 | 28 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| pmc19sm-il | 50,000 | 5 | 32.3 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| pmc19sm-il | 100,000 | 9 | 44.6 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| pmc19sm-il | 100,000 | 5 | 45 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| pmc19sm-il | 200,000 | 9 | 58.9 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| pmc19sm-il | 200,000 | 5 | 57.9 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| pmc19sm-il | 500,000 | 9 | 79 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| pmc19sm-il | 500,000 | 5 | 74 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| pmc19sm-il | 1,000,000 | 9 | 93.8 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| pmc19sm-il | 1,000,000 | 5 | 82.2 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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