BE50 (smoothed) (be50sm-il)
BE50 (smoothed) - Verbitsky BE50 free flight airfoil (original)
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(be50sm-il) BE50 (smoothed) Verbitsky BE50 free flight airfoil (original) Max thickness 7.3% at 23.8% chord. Max camber 4% at 45.4% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Selig format |
BE50 (smoothed)
1.00000 0.00129
0.99754 0.00178
0.99070 0.00314
0.98037 0.00517
0.96698 0.00777
0.95044 0.01091
0.93064 0.01457
0.90775 0.01865
0.88202 0.02305
0.85370 0.02766
0.82309 0.03238
0.79048 0.03710
0.75616 0.04176
0.72043 0.04627
0.68359 0.05058
0.64594 0.05463
0.60778 0.05835
0.56937 0.06171
0.53099 0.06466
0.49265 0.06714
0.45435 0.06911
0.41638 0.07054
0.37887 0.07144
0.34204 0.07186
0.30609 0.07180
0.27120 0.07119
0.23760 0.06993
0.20549 0.06792
0.17504 0.06505
0.14648 0.06128
0.11999 0.05662
0.09576 0.05113
0.07395 0.04491
0.05468 0.03812
0.03811 0.03098
0.02433 0.02374
0.01338 0.01662
0.00548 0.00989
0.00098 0.00382
0.00000 -0.00003
0.00098 -0.00332
0.00548 -0.00695
0.01338 -0.00956
0.02433 -0.01127
0.03811 -0.01224
0.05468 -0.01256
0.07395 -0.01229
0.09576 -0.01152
0.11999 -0.01033
0.14648 -0.00882
0.17504 -0.00709
0.20549 -0.00522
0.23760 -0.00323
0.27120 -0.00115
0.30609 0.00102
0.34204 0.00330
0.37887 0.00563
0.41638 0.00792
0.45435 0.01002
0.49265 0.01177
0.53099 0.01310
0.56937 0.01397
0.60778 0.01440
0.64594 0.01440
0.68359 0.01402
0.72043 0.01331
0.75616 0.01233
0.79048 0.01114
0.82309 0.00980
0.85370 0.00836
0.88202 0.00688
0.90775 0.00540
0.93064 0.00398
0.95044 0.00265
0.96698 0.00146
0.98037 0.00041
0.99070 -0.00046
0.99754 -0.00107
1.00000 -0.00130
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Polars for BE50 (smoothed) (be50sm-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| be50sm-il | 50,000 | 9 | 38.9 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| be50sm-il | 50,000 | 5 | 43 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| be50sm-il | 100,000 | 9 | 60.5 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| be50sm-il | 100,000 | 5 | 59.2 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| be50sm-il | 200,000 | 9 | 81.2 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| be50sm-il | 200,000 | 5 | 74.4 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| be50sm-il | 500,000 | 9 | 104.9 at α=2.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| be50sm-il | 500,000 | 5 | 97.8 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| be50sm-il | 1,000,000 | 9 | 121.5 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| be50sm-il | 1,000,000 | 5 | 115.9 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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