RAE 5215 AIRFOIL (rae5215-il)
RAE 5215 AIRFOIL - RAE 5215 transonic airfoil
| Details | Dat file | Parser | |
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(rae5215-il) RAE 5215 AIRFOIL RAE 5215 transonic airfoil Max thickness 9.7% at 35.5% chord. Max camber 1.5% at 69.1% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
RAE 5215 AIRFOIL
42. 42.
0.00000 0.00000
0.00050 0.00522
0.00100 0.00732
0.00160 0.00925
0.00241 0.01128
0.00350 0.01343
0.00500 0.01580
0.00650 0.01778
0.00800 0.01940
0.00961 0.02090
0.01500 0.02480
0.02153 0.02841
0.03000 0.03216
0.03806 0.03496
0.05904 0.04033
0.08427 0.04421
0.11349 0.04719
0.14645 0.04995
0.18280 0.05231
0.22221 0.05427
0.26430 0.05581
0.30866 0.05697
0.35486 0.05763
0.40245 0.05779
0.45099 0.05735
0.50000 0.05637
0.54901 0.05462
0.59755 0.05208
0.64514 0.04876
0.69134 0.04455
0.73570 0.03976
0.77779 0.03472
0.81720 0.02971
0.85355 0.02484
0.88651 0.02031
0.91573 0.01626
0.94096 0.01260
0.96194 0.00950
0.97847 0.00706
0.99039 0.00525
0.99759 0.00416
1.00000 0.00380
0.00000 0.00000
0.00050 -0.00410
0.00100 -0.00545
0.00160 -0.00665
0.00241 -0.00785
0.00350 -0.00900
0.00500 -0.01030
0.00650 -0.01139
0.00800 -0.01228
0.00961 -0.01316
0.01500 -0.01533
0.02153 -0.01727
0.03000 -0.01947
0.03806 -0.02118
0.05904 -0.02459
0.08427 -0.02786
0.11349 -0.03074
0.14645 -0.03332
0.18280 -0.03556
0.22221 -0.03731
0.26430 -0.03856
0.30866 -0.03915
0.35486 -0.03889
0.40245 -0.03773
0.45099 -0.03560
0.50000 -0.03232
0.54901 -0.02788
0.59755 -0.02267
0.64514 -0.01716
0.69134 -0.01199
0.73570 -0.00768
0.77779 -0.00424
0.81720 -0.00175
0.85355 -0.00010
0.88651 0.00085
0.91573 0.00130
0.94096 0.00126
0.96194 0.00098
0.97847 0.00062
0.99039 0.00029
0.99759 0.00006
1.00000 0.00000
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Polars for RAE 5215 AIRFOIL (rae5215-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| rae5215-il | 50,000 | 9 | 28.5 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rae5215-il | 50,000 | 5 | 26.7 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rae5215-il | 100,000 | 9 | 38 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rae5215-il | 100,000 | 5 | 35.3 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rae5215-il | 200,000 | 9 | 43.8 at α=2° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rae5215-il | 200,000 | 5 | 49.8 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rae5215-il | 500,000 | 9 | 67.4 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rae5215-il | 500,000 | 5 | 68.6 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rae5215-il | 1,000,000 | 9 | 83.2 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rae5215-il | 1,000,000 | 5 | 81.1 at α=9.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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