RAE(NPL) 5213 AIRFOIL (rae5213-il)
RAE(NPL) 5213 AIRFOIL - RAE(NPL) 5213 transonic airfoil
| Details | Dat file | Parser | |
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(rae5213-il) RAE(NPL) 5213 AIRFOIL RAE(NPL) 5213 transonic airfoil Max thickness 10% at 35.5% chord. Max camber 1.4% at 69.1% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
RAE(NPL) 5213 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 0.04029
0.08427 0.04444
0.11349 0.04828
0.14645 0.05170
0.18280 0.05476
0.22221 0.05719
0.26430 0.05904
0.30866 0.06021
0.35486 0.06061
0.40245 0.06017
0.45099 0.05892
0.50000 0.05688
0.54901 0.05394
0.59755 0.05017
0.64514 0.04574
0.69134 0.04087
0.73570 0.03586
0.77779 0.03082
0.81720 0.02581
0.85355 0.02094
0.88651 0.01641
0.91573 0.01236
0.94096 0.00870
0.96194 0.00562
0.97847 0.00302
0.99039 0.00133
0.99759 0.00034
1.00000 0.00000
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(NPL) 5213 AIRFOIL (rae5213-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| rae5213-il | 50,000 | 9 | 29.6 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rae5213-il | 50,000 | 5 | 29.2 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rae5213-il | 100,000 | 9 | 42.7 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rae5213-il | 100,000 | 5 | 35.9 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rae5213-il | 200,000 | 9 | 49.6 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rae5213-il | 200,000 | 5 | 48.7 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rae5213-il | 500,000 | 9 | 65.9 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rae5213-il | 500,000 | 5 | 68.3 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rae5213-il | 1,000,000 | 9 | 83.2 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rae5213-il | 1,000,000 | 5 | 80.6 at α=9.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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