B-29 ROOT AIRFOIL (b29root-il)
B-29 ROOT AIRFOIL - Boeing B-29 root airfoil
| Details | Dat file | Parser | |
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(b29root-il) B-29 ROOT AIRFOIL Boeing B-29 root airfoil Max thickness 22% at 30.2% chord. Max camber 1.7% at 30.2% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
B-29 ROOT AIRFOIL
19.0 21.0
0.0000000 0.0000000
0.0082707 0.0233088
0.0132000 0.0298517
0.0255597 0.0425630
0.0503554 0.0603942
0.0751941 0.0739301
0.1000570 0.0850687
0.1498328 0.1023515
0.1996558 0.1149395
0.2495240 0.1230325
0.2994312 0.1272298
0.3993490 0.1253360
0.4993711 0.1130538
0.5994664 0.0934796
0.6996058 0.0695104
0.7997553 0.0445423
0.8998927 0.0207728
0.9499514 0.0098870
1.0000000 0.0000000
0.0000000 0.0000000
0.0061140 -.0208973
0.0062188 -.0210669
0.0087532 -.0247377
0.0138088 -.0307807
0.0264052 -.0416431
0.0515127 -.0548774
0.0765762 -.0637165
0.1016176 -.0703581
0.1516652 -.0801452
0.2016828 -.0869356
0.2516733 -.0910290
0.3016387 -.0926252
0.4015163 -.0905235
0.5013438 -.0834273
0.6011363 -.0728351
0.7008976 -.0591463
0.8006328 -.0428603
0.9003380 -.0235778
0.9501740 -.0122883
1.0000000 0.0000000
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Polars for B-29 ROOT AIRFOIL (b29root-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| b29root-il | 50,000 | 9 | 2.4 at α=10.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| b29root-il | 50,000 | 5 | 8.5 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| b29root-il | 100,000 | 9 | 13.8 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| b29root-il | 100,000 | 5 | 34.6 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| b29root-il | 200,000 | 9 | 58.2 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| b29root-il | 200,000 | 5 | 52.8 at α=9.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| b29root-il | 500,000 | 9 | 77.9 at α=10.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| b29root-il | 500,000 | 5 | 68.8 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| b29root-il | 1,000,000 | 9 | 90.5 at α=9.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| b29root-il | 1,000,000 | 5 | 83.2 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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