CAST 10-2/DOA 2 AIRFOIL (cast102-il)
CAST 10-2/DOA 2 AIRFOIL - CAST 10-2/DOA 2 transonic airfoil
| Details | Dat file | Parser | |
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(cast102-il) CAST 10-2/DOA 2 AIRFOIL CAST 10-2/DOA 2 transonic airfoil Max thickness 12.2% at 45.4% chord. Max camber 1.5% at 69.4% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
CAST 10-2/DOA 2 AIRFOIL
29. 29.
0.0 0.0
0.0008289 0.0046133
0.0024762 0.0080391
0.0073888 0.0137153
0.0123292 0.0175919
0.0172804 0.0207685
0.0247141 0.0250836
0.0346379 0.0300370
0.0470596 0.0351288
0.0644740 0.0406977
0.0868873 0.0463435
0.1143073 0.0515664
0.1542197 0.0572817
0.2141277 0.0633048
0.2740664 0.0673284
0.3340267 0.0699521
0.3939024 0.0715743
0.4538935 0.0721984
0.5139016 0.0717224
0.5739295 0.0699466
0.6339809 0.0666711
0.6940659 0.0611959
0.7541876 0.0533209
0.8143482 0.0429462
0.8745379 0.0306718
0.9196926 0.0206659
0.9497966 0.0139288
0.9773936 0.0076530
1.0000000 0.0025002
0.0 0.0
0.0011767 -.0049824
0.0027102 -.0071591
0.0077629 -.0105817
0.0127896 -.0123045
0.0178100 -.0136273
0.0253345 -.0152117
0.0353661 -.0172573
0.0479034 -.0196646
0.0654470 -.0224947
0.0879989 -.0258478
0.1155530 -.0293239
0.1556209 -.0337074
0.2157074 -.0392825
0.2757784 -.0438580
0.3358327 -.0473336
0.3957655 -.0494108
0.4557689 -.0495868
0.5157368 -.0474630
0.5756710 -.0431394
0.6355790 -.0371162
0.6954732 -.0301930
0.7553640 -.0230699
0.8152613 -.0163466
0.8751723 -.0105233
0.9201159 -.0068308
0.9500861 -.0048690
0.9775629 -.0033456
1.0000000 -.0024992
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Polars for CAST 10-2/DOA 2 AIRFOIL (cast102-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| cast102-il | 50,000 | 9 | 32.8 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| cast102-il | 50,000 | 5 | 30.3 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| cast102-il | 100,000 | 9 | 45.8 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| cast102-il | 100,000 | 5 | 43 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| cast102-il | 200,000 | 9 | 64 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| cast102-il | 200,000 | 5 | 55.6 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| cast102-il | 500,000 | 9 | 85.5 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| cast102-il | 500,000 | 5 | 66.8 at α=2° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| cast102-il | 1,000,000 | 9 | 93.9 at α=2.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| cast102-il | 1,000,000 | 5 | 75.6 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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