B-29 ROOT AIRFOIL (b29root-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: B-29 ROOT AIRFOIL (b29root-il) Reynolds number: 500,000 Max Cl/Cd: 77.89 at α=10.75° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-b29root-il-500000.txt Download as CSV file: xf-b29root-il-500000.csv |
XFOIL Version 6.96
Calculated polar for: B-29 ROOT AIRFOIL
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.500 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -1.0866 0.07735 0.07245 -0.0655 1.0000 0.0543
-19.500 -1.0845 0.07457 0.06962 -0.0666 1.0000 0.0549
-19.250 -1.0824 0.07183 0.06682 -0.0676 1.0000 0.0555
-19.000 -1.0811 0.06901 0.06392 -0.0687 1.0000 0.0562
-18.750 -1.0801 0.06620 0.06102 -0.0696 1.0000 0.0568
-18.500 -1.0779 0.06358 0.05830 -0.0705 1.0000 0.0573
-18.250 -1.0772 0.06075 0.05535 -0.0714 1.0000 0.0579
-18.000 -1.0705 0.05890 0.05347 -0.0715 1.0000 0.0587
-17.750 -1.0628 0.05715 0.05174 -0.0716 1.0000 0.0595
-17.500 -1.0565 0.05515 0.04974 -0.0721 1.0000 0.0603
-17.250 -1.0505 0.05313 0.04768 -0.0725 1.0000 0.0610
-17.000 -1.0446 0.05110 0.04561 -0.0729 1.0000 0.0619
-16.750 -1.0384 0.04916 0.04360 -0.0731 1.0000 0.0627
-16.500 -1.0323 0.04723 0.04160 -0.0733 1.0000 0.0634
-16.250 -1.0254 0.04545 0.03972 -0.0733 1.0000 0.0640
-16.000 -1.0174 0.04381 0.03802 -0.0732 1.0000 0.0646
-15.750 -1.0077 0.04249 0.03674 -0.0726 1.0000 0.0656
-15.500 -0.9993 0.04098 0.03523 -0.0722 1.0000 0.0663
-15.250 -0.9905 0.03950 0.03374 -0.0720 1.0000 0.0671
-15.000 -0.9817 0.03807 0.03227 -0.0716 1.0000 0.0679
-14.750 -0.9724 0.03670 0.03087 -0.0712 1.0000 0.0688
-14.500 -0.9626 0.03540 0.02952 -0.0707 1.0000 0.0696
-14.250 -0.9528 0.03414 0.02822 -0.0701 1.0000 0.0704
-14.000 -0.9424 0.03297 0.02698 -0.0695 1.0000 0.0711
-13.750 -0.9353 0.03162 0.02566 -0.0684 1.0000 0.0722
-13.500 -0.9221 0.03007 0.02414 -0.0681 0.9738 0.0731
-13.250 -0.8719 0.02858 0.02260 -0.0755 0.9438 0.0751
-13.000 -0.8104 0.02718 0.02111 -0.0846 0.9247 0.0772
-12.750 -0.7502 0.02584 0.01961 -0.0936 0.8985 0.0794
-12.500 -0.7182 0.02461 0.01824 -0.0973 0.8657 0.0813
-12.250 -0.7018 0.02382 0.01732 -0.0971 0.8409 0.0829
-12.000 -0.6891 0.02311 0.01649 -0.0960 0.8229 0.0843
-11.750 -0.6763 0.02248 0.01573 -0.0946 0.8086 0.0860
-11.500 -0.6658 0.02179 0.01494 -0.0929 0.7958 0.0874
-11.250 -0.6597 0.02093 0.01404 -0.0907 0.7848 0.0892
-11.000 -0.6492 0.02030 0.01336 -0.0889 0.7751 0.0914
-10.750 -0.6369 0.01976 0.01275 -0.0871 0.7667 0.0936
-10.500 -0.6227 0.01931 0.01223 -0.0855 0.7580 0.0957
-10.250 -0.6162 0.01861 0.01148 -0.0829 0.7501 0.0984
-10.000 -0.6052 0.01807 0.01093 -0.0807 0.7429 0.1013
-9.750 -0.5912 0.01766 0.01047 -0.0789 0.7357 0.1046
-9.500 -0.5813 0.01714 0.00990 -0.0764 0.7290 0.1081
-9.250 -0.5695 0.01667 0.00943 -0.0742 0.7226 0.1120
-9.000 -0.5542 0.01633 0.00905 -0.0724 0.7161 0.1164
-8.750 -0.5443 0.01584 0.00856 -0.0697 0.7098 0.1217
-8.500 -0.5295 0.01552 0.00820 -0.0678 0.7042 0.1273
-8.250 -0.5175 0.01508 0.00780 -0.0653 0.6984 0.1336
-8.000 -0.5023 0.01476 0.00745 -0.0633 0.6926 0.1410
-7.750 -0.4906 0.01436 0.00706 -0.0607 0.6869 0.1497
-7.500 -0.4769 0.01399 0.00673 -0.0584 0.6816 0.1603
-7.250 -0.4641 0.01358 0.00639 -0.0559 0.6764 0.1740
-7.000 -0.4526 0.01315 0.00603 -0.0532 0.6711 0.1934
-6.750 -0.4420 0.01271 0.00568 -0.0503 0.6659 0.2202
-6.500 -0.4318 0.01226 0.00539 -0.0472 0.6608 0.2533
-6.250 -0.4191 0.01189 0.00515 -0.0445 0.6558 0.2844
-6.000 -0.4046 0.01161 0.00495 -0.0421 0.6507 0.3083
-5.750 -0.3888 0.01139 0.00476 -0.0398 0.6458 0.3283
-5.500 -0.3716 0.01122 0.00462 -0.0378 0.6411 0.3466
-5.250 -0.3531 0.01106 0.00449 -0.0360 0.6363 0.3620
-5.000 -0.3362 0.01089 0.00437 -0.0338 0.6312 0.3764
-4.750 -0.3180 0.01079 0.00426 -0.0319 0.6264 0.3894
-4.250 -0.2806 0.01062 0.00412 -0.0283 0.6171 0.4150
-4.000 -0.2613 0.01054 0.00405 -0.0265 0.6124 0.4266
-3.750 -0.2427 0.01048 0.00399 -0.0246 0.6079 0.4392
-3.500 -0.2243 0.01043 0.00393 -0.0227 0.6031 0.4517
-3.250 -0.2038 0.01037 0.00390 -0.0211 0.5987 0.4649
-3.000 -0.1839 0.01027 0.00385 -0.0195 0.5939 0.4781
-2.750 -0.1627 0.01020 0.00379 -0.0181 0.5894 0.4898
-2.500 -0.1409 0.01017 0.00373 -0.0169 0.5850 0.5024
-2.250 -0.1200 0.01011 0.00371 -0.0154 0.5808 0.5156
-2.000 -0.0990 0.01003 0.00369 -0.0140 0.5765 0.5299
-1.750 -0.0777 0.00998 0.00365 -0.0126 0.5719 0.5450
-1.500 -0.0575 0.00990 0.00362 -0.0110 0.5674 0.5615
-1.250 -0.0371 0.00989 0.00361 -0.0094 0.5628 0.5797
-1.000 -0.0166 0.00980 0.00362 -0.0079 0.5591 0.5968
-0.750 0.0052 0.00975 0.00362 -0.0066 0.5548 0.6118
-0.500 0.0271 0.00972 0.00360 -0.0053 0.5507 0.6269
-0.250 0.0492 0.00969 0.00360 -0.0041 0.5466 0.6419
0.000 0.0718 0.00970 0.00362 -0.0030 0.5423 0.6565
0.250 0.0937 0.00967 0.00364 -0.0017 0.5384 0.6715
0.500 0.1159 0.00962 0.00366 -0.0004 0.5341 0.6868
0.750 0.1385 0.00960 0.00368 0.0007 0.5302 0.7019
1.000 0.1614 0.00964 0.00370 0.0017 0.5262 0.7172
1.250 0.1841 0.00967 0.00376 0.0029 0.5225 0.7322
1.500 0.2074 0.00964 0.00382 0.0039 0.5186 0.7466
1.750 0.2306 0.00963 0.00386 0.0049 0.5145 0.7609
2.000 0.2530 0.00966 0.00390 0.0061 0.5106 0.7760
2.250 0.2789 0.00973 0.00398 0.0065 0.5067 0.7903
2.500 0.3042 0.00977 0.00408 0.0070 0.5031 0.8037
2.750 0.3269 0.00979 0.00416 0.0081 0.4994 0.8180
3.000 0.3538 0.00984 0.00426 0.0084 0.4954 0.8314
3.250 0.3818 0.00992 0.00437 0.0084 0.4917 0.8438
3.500 0.4065 0.01005 0.00447 0.0090 0.4879 0.8573
3.750 0.4401 0.01020 0.00467 0.0078 0.4841 0.8675
4.000 0.4659 0.01029 0.00481 0.0082 0.4806 0.8790
4.250 0.4990 0.01044 0.00500 0.0071 0.4768 0.8879
4.500 0.5265 0.01059 0.00514 0.0072 0.4733 0.8977
4.750 0.5646 0.01085 0.00537 0.0050 0.4692 0.9035
5.000 0.5848 0.01101 0.00555 0.0065 0.4659 0.9141
5.250 0.6252 0.01124 0.00582 0.0038 0.4623 0.9174
5.500 0.6638 0.01147 0.00607 0.0015 0.4586 0.9210
5.750 0.6952 0.01169 0.00628 0.0007 0.4551 0.9266
6.000 0.7227 0.01193 0.00648 0.0007 0.4514 0.9328
6.250 0.7644 0.01223 0.00679 -0.0024 0.4476 0.9342
6.500 0.8026 0.01248 0.00709 -0.0047 0.4441 0.9361
6.750 0.8391 0.01274 0.00738 -0.0066 0.4405 0.9384
7.000 0.8714 0.01300 0.00764 -0.0077 0.4369 0.9424
7.250 0.8930 0.01325 0.00783 -0.0066 0.4325 0.9493
7.500 0.9307 0.01351 0.00815 -0.0089 0.4277 0.9509
7.750 0.9665 0.01374 0.00843 -0.0108 0.4228 0.9532
8.000 0.9984 0.01397 0.00864 -0.0119 0.4170 0.9567
8.250 1.0153 0.01423 0.00889 -0.0100 0.4108 0.9646
8.500 1.0485 0.01437 0.00909 -0.0116 0.4031 0.9671
8.750 1.0801 0.01462 0.00929 -0.0129 0.3970 0.9702
9.000 1.1070 0.01485 0.00957 -0.0132 0.3923 0.9751
9.250 1.1316 0.01505 0.00983 -0.0131 0.3872 0.9798
9.500 1.1648 0.01526 0.01004 -0.0149 0.3817 0.9821
9.750 1.1943 0.01554 0.01032 -0.0160 0.3759 0.9854
10.000 1.2213 0.01578 0.01063 -0.0167 0.3700 0.9895
10.250 1.2474 0.01611 0.01096 -0.0173 0.3636 0.9930
10.500 1.2773 0.01641 0.01130 -0.0189 0.3573 0.9960
10.750 1.3062 0.01677 0.01170 -0.0203 0.3493 0.9991
11.000 1.3080 0.01735 0.01225 -0.0169 0.3433 1.0000
11.250 1.3069 0.01781 0.01278 -0.0128 0.3379 1.0000
11.500 1.3020 0.01847 0.01345 -0.0084 0.3315 1.0000
11.750 1.2956 0.01929 0.01426 -0.0039 0.3253 1.0000
12.000 1.2949 0.02003 0.01505 -0.0004 0.3180 1.0000
12.250 1.2878 0.02113 0.01612 0.0037 0.3105 1.0000
12.500 1.2864 0.02212 0.01713 0.0069 0.3016 1.0000
12.750 1.2787 0.02350 0.01849 0.0105 0.2928 1.0000
13.000 1.2754 0.02482 0.01981 0.0135 0.2823 1.0000
13.250 1.2684 0.02643 0.02141 0.0165 0.2714 1.0000
13.500 1.2581 0.02838 0.02332 0.0196 0.2600 1.0000
13.750 1.2479 0.03049 0.02540 0.0223 0.2467 1.0000
14.000 1.2376 0.03277 0.02764 0.0247 0.2325 1.0000
14.250 1.2220 0.03560 0.03041 0.0272 0.2164 1.0000
14.500 1.2071 0.03855 0.03330 0.0293 0.2015 1.0000
14.750 1.1877 0.04205 0.03673 0.0312 0.1856 1.0000
15.000 1.1761 0.04504 0.03968 0.0326 0.1738 1.0000
15.250 1.1639 0.04821 0.04281 0.0339 0.1621 1.0000
15.500 1.1538 0.05130 0.04589 0.0349 0.1523 1.0000
15.750 1.1432 0.05454 0.04910 0.0358 0.1437 1.0000
16.000 1.1349 0.05764 0.05218 0.0364 0.1345 1.0000
16.250 1.1300 0.06048 0.05501 0.0370 0.1266 1.0000
16.500 1.1220 0.06371 0.05823 0.0374 0.1198 1.0000
16.750 1.1185 0.06653 0.06104 0.0377 0.1133 1.0000
17.000 1.1135 0.06955 0.06406 0.0379 0.1080 1.0000
17.250 1.1104 0.07243 0.06694 0.0380 0.1030 1.0000
17.500 1.1061 0.07548 0.07000 0.0380 0.0989 1.0000
17.750 1.1065 0.07806 0.07260 0.0380 0.0951 1.0000
18.000 1.1024 0.08117 0.07571 0.0379 0.0918 1.0000
18.250 1.1033 0.08372 0.07828 0.0378 0.0888 1.0000
18.500 1.1032 0.08646 0.08106 0.0375 0.0860 1.0000
18.750 1.1021 0.08933 0.08393 0.0373 0.0835 1.0000
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