BOEING 106 AIRFOIL (boe106-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: BOEING 106 AIRFOIL (boe106-il) Reynolds number: 1,000,000 Max Cl/Cd: 108.22 at α=5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-boe106-il-1000000-n5.txt Download as CSV file: xf-boe106-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: BOEING 106 AIRFOIL
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 1.000 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-16.750 -1.1668 0.04490 0.04179 -0.0766 1.0000 0.0091
-16.500 -1.1863 0.03850 0.03518 -0.0819 1.0000 0.0091
-16.250 -1.1946 0.03475 0.03128 -0.0838 1.0000 0.0092
-16.000 -1.1976 0.03215 0.02855 -0.0841 1.0000 0.0093
-15.750 -1.1971 0.03021 0.02648 -0.0834 1.0000 0.0094
-15.500 -1.1946 0.02861 0.02477 -0.0820 1.0000 0.0095
-15.250 -1.1921 0.02717 0.02323 -0.0800 1.0000 0.0098
-15.000 -1.1863 0.02597 0.02194 -0.0779 1.0000 0.0100
-14.750 -1.1759 0.02489 0.02079 -0.0763 1.0000 0.0103
-14.500 -1.1641 0.02394 0.01977 -0.0746 1.0000 0.0106
-14.250 -1.1526 0.02311 0.01886 -0.0726 1.0000 0.0110
-14.000 -1.1337 0.02225 0.01792 -0.0720 0.9978 0.0113
-13.750 -1.1076 0.02137 0.01695 -0.0727 0.9942 0.0117
-13.500 -1.0823 0.02059 0.01607 -0.0731 0.9892 0.0120
-13.250 -1.0558 0.01975 0.01517 -0.0738 0.9846 0.0125
-13.000 -1.0301 0.01905 0.01442 -0.0741 0.9787 0.0131
-12.750 -1.0029 0.01842 0.01372 -0.0746 0.9730 0.0137
-12.500 -0.9779 0.01784 0.01308 -0.0746 0.9654 0.0142
-12.250 -0.9527 0.01730 0.01247 -0.0745 0.9582 0.0147
-12.000 -0.9292 0.01680 0.01189 -0.0740 0.9493 0.0153
-11.750 -0.9051 0.01637 0.01143 -0.0736 0.9411 0.0160
-11.500 -0.8811 0.01600 0.01100 -0.0730 0.9322 0.0167
-11.250 -0.8567 0.01563 0.01058 -0.0725 0.9242 0.0174
-11.000 -0.8324 0.01527 0.01013 -0.0720 0.9154 0.0180
-10.750 -0.8079 0.01490 0.00968 -0.0715 0.9073 0.0185
-10.500 -0.7832 0.01454 0.00927 -0.0711 0.8988 0.0191
-10.250 -0.7579 0.01425 0.00894 -0.0707 0.8910 0.0197
-10.000 -0.7324 0.01398 0.00861 -0.0703 0.8823 0.0204
-9.750 -0.7068 0.01373 0.00829 -0.0699 0.8727 0.0211
-9.500 -0.6812 0.01348 0.00796 -0.0695 0.8618 0.0217
-9.250 -0.6554 0.01324 0.00763 -0.0692 0.8509 0.0221
-9.000 -0.6299 0.01290 0.00723 -0.0688 0.8423 0.0226
-8.750 -0.6042 0.01260 0.00688 -0.0684 0.8340 0.0233
-8.500 -0.5778 0.01237 0.00661 -0.0682 0.8265 0.0240
-8.250 -0.5513 0.01216 0.00634 -0.0680 0.8187 0.0246
-8.000 -0.5248 0.01193 0.00606 -0.0677 0.8115 0.0252
-7.750 -0.4981 0.01172 0.00580 -0.0675 0.8039 0.0258
-7.500 -0.4713 0.01152 0.00553 -0.0673 0.7969 0.0264
-7.250 -0.4444 0.01132 0.00528 -0.0671 0.7895 0.0267
-7.000 -0.4184 0.01101 0.00491 -0.0668 0.7826 0.0275
-6.750 -0.3917 0.01074 0.00462 -0.0666 0.7753 0.0282
-6.500 -0.3649 0.01055 0.00438 -0.0663 0.7681 0.0289
-6.250 -0.3377 0.01036 0.00416 -0.0662 0.7616 0.0296
-6.000 -0.3107 0.01018 0.00393 -0.0660 0.7542 0.0302
-5.750 -0.2835 0.01000 0.00371 -0.0658 0.7473 0.0308
-5.500 -0.2563 0.00983 0.00350 -0.0657 0.7399 0.0314
-5.250 -0.2290 0.00969 0.00331 -0.0655 0.7332 0.0319
-5.000 -0.2019 0.00951 0.00309 -0.0653 0.7256 0.0327
-4.750 -0.1749 0.00934 0.00289 -0.0651 0.7181 0.0338
-4.500 -0.1475 0.00919 0.00272 -0.0650 0.7103 0.0349
-4.250 -0.1203 0.00907 0.00257 -0.0648 0.7022 0.0360
-4.000 -0.0929 0.00896 0.00242 -0.0646 0.6928 0.0371
-3.750 -0.0657 0.00888 0.00229 -0.0645 0.6810 0.0381
-3.500 -0.0388 0.00879 0.00215 -0.0642 0.6672 0.0400
-3.250 -0.0119 0.00871 0.00203 -0.0640 0.6540 0.0428
-3.000 0.0155 0.00863 0.00193 -0.0638 0.6432 0.0455
-2.750 0.0428 0.00855 0.00182 -0.0636 0.6328 0.0496
-2.500 0.0699 0.00848 0.00173 -0.0635 0.6213 0.0546
-2.250 0.0969 0.00840 0.00164 -0.0633 0.6097 0.0644
-2.000 0.1236 0.00826 0.00157 -0.0631 0.5992 0.0891
-1.750 0.1506 0.00820 0.00152 -0.0629 0.5884 0.1059
-1.500 0.1776 0.00816 0.00148 -0.0627 0.5767 0.1190
-1.250 0.2048 0.00811 0.00145 -0.0625 0.5656 0.1336
-1.000 0.2318 0.00807 0.00142 -0.0624 0.5557 0.1511
-0.750 0.2587 0.00799 0.00139 -0.0622 0.5463 0.1761
-0.500 0.2850 0.00783 0.00136 -0.0620 0.5381 0.2279
-0.250 0.3107 0.00764 0.00135 -0.0616 0.5291 0.2999
0.000 0.3363 0.00741 0.00135 -0.0613 0.5207 0.3817
0.250 0.3615 0.00722 0.00136 -0.0609 0.5118 0.4605
0.500 0.3859 0.00691 0.00137 -0.0603 0.5042 0.5708
0.750 0.4104 0.00673 0.00142 -0.0597 0.4966 0.6611
1.000 0.4366 0.00666 0.00146 -0.0593 0.4897 0.7060
1.250 0.4630 0.00664 0.00151 -0.0590 0.4819 0.7383
1.500 0.4892 0.00660 0.00156 -0.0586 0.4750 0.7729
1.750 0.5151 0.00659 0.00162 -0.0581 0.4667 0.8080
2.000 0.5409 0.00657 0.00169 -0.0576 0.4587 0.8430
2.250 0.5659 0.00657 0.00179 -0.0568 0.4488 0.8923
2.500 0.5949 0.00665 0.00193 -0.0569 0.4354 0.9424
2.750 0.6293 0.00683 0.00205 -0.0583 0.4197 0.9634
3.000 0.6640 0.00700 0.00217 -0.0598 0.4063 0.9756
3.250 0.6989 0.00718 0.00229 -0.0614 0.3937 0.9846
3.500 0.7350 0.00736 0.00240 -0.0634 0.3808 0.9877
3.750 0.7666 0.00755 0.00251 -0.0644 0.3669 0.9904
4.000 0.7974 0.00772 0.00263 -0.0652 0.3556 0.9932
4.250 0.8298 0.00787 0.00274 -0.0663 0.3456 0.9949
4.500 0.8616 0.00808 0.00289 -0.0674 0.3312 0.9967
4.750 0.8927 0.00831 0.00304 -0.0684 0.3157 0.9986
5.000 0.9231 0.00853 0.00320 -0.0692 0.3027 1.0000
5.250 0.9445 0.00874 0.00335 -0.0680 0.2910 1.0000
5.500 0.9662 0.00894 0.00351 -0.0669 0.2785 1.0000
5.750 0.9876 0.00916 0.00367 -0.0657 0.2653 1.0000
6.000 1.0083 0.00942 0.00387 -0.0644 0.2495 1.0000
6.250 1.0266 0.00982 0.00413 -0.0627 0.2221 1.0000
6.500 1.0408 0.01045 0.00453 -0.0604 0.1807 1.0000
6.750 1.0583 0.01092 0.00488 -0.0586 0.1592 1.0000
7.000 1.0786 0.01126 0.00516 -0.0574 0.1474 1.0000
7.250 1.1000 0.01155 0.00543 -0.0563 0.1385 1.0000
7.500 1.1210 0.01188 0.00572 -0.0552 0.1296 1.0000
7.750 1.1426 0.01219 0.00600 -0.0543 0.1216 1.0000
8.000 1.1639 0.01252 0.00630 -0.0533 0.1135 1.0000
8.250 1.1844 0.01290 0.00663 -0.0522 0.1047 1.0000
8.500 1.2057 0.01322 0.00696 -0.0513 0.0980 1.0000
8.750 1.2252 0.01365 0.00733 -0.0501 0.0890 1.0000
9.000 1.2436 0.01411 0.00774 -0.0488 0.0795 1.0000
9.250 1.2621 0.01450 0.00812 -0.0474 0.0734 1.0000
9.500 1.2791 0.01497 0.00855 -0.0458 0.0676 1.0000
9.750 1.2974 0.01536 0.00896 -0.0445 0.0641 1.0000
10.000 1.3144 0.01585 0.00944 -0.0431 0.0603 1.0000
10.250 1.3314 0.01635 0.00994 -0.0417 0.0566 1.0000
10.500 1.3485 0.01685 0.01045 -0.0404 0.0536 1.0000
10.750 1.3644 0.01743 0.01104 -0.0390 0.0508 1.0000
11.000 1.3803 0.01803 0.01166 -0.0376 0.0482 1.0000
11.250 1.3971 0.01858 0.01224 -0.0365 0.0467 1.0000
11.500 1.4123 0.01926 0.01294 -0.0352 0.0439 1.0000
11.750 1.4253 0.02008 0.01376 -0.0337 0.0408 1.0000
12.000 1.4402 0.02082 0.01453 -0.0326 0.0385 1.0000
12.250 1.4524 0.02174 0.01546 -0.0312 0.0351 1.0000
12.500 1.4647 0.02270 0.01644 -0.0300 0.0322 1.0000
12.750 1.4744 0.02387 0.01760 -0.0286 0.0279 1.0000
13.000 1.4812 0.02529 0.01901 -0.0271 0.0222 1.0000
13.250 1.4854 0.02698 0.02070 -0.0256 0.0170 1.0000
13.500 1.4911 0.02861 0.02235 -0.0243 0.0144 1.0000
13.750 1.4965 0.03031 0.02410 -0.0232 0.0127 1.0000
14.000 1.5036 0.03193 0.02577 -0.0222 0.0118 1.0000
14.250 1.5091 0.03372 0.02761 -0.0213 0.0109 1.0000
14.500 1.5132 0.03568 0.02963 -0.0205 0.0102 1.0000
14.750 1.5187 0.03758 0.03160 -0.0198 0.0098 1.0000
15.000 1.5236 0.03956 0.03366 -0.0192 0.0094 1.0000
15.250 1.5274 0.04172 0.03588 -0.0187 0.0090 1.0000
15.500 1.5301 0.04405 0.03829 -0.0183 0.0087 1.0000
15.750 1.5317 0.04657 0.04087 -0.0180 0.0084 1.0000
16.000 1.5321 0.04928 0.04366 -0.0178 0.0081 1.0000
16.250 1.5313 0.05221 0.04666 -0.0177 0.0078 1.0000
16.500 1.5313 0.05511 0.04964 -0.0178 0.0076 1.0000
16.750 1.5315 0.05806 0.05267 -0.0180 0.0075 1.0000
17.000 1.5305 0.06118 0.05589 -0.0182 0.0073 1.0000
17.250 1.5286 0.06447 0.05927 -0.0186 0.0071 1.0000
17.500 1.5258 0.06794 0.06282 -0.0191 0.0070 1.0000
17.750 1.5221 0.07159 0.06655 -0.0197 0.0068 1.0000
18.000 1.5173 0.07539 0.07044 -0.0204 0.0066 1.0000
18.250 1.5115 0.07938 0.07453 -0.0213 0.0065 1.0000
18.500 1.5049 0.08357 0.07880 -0.0222 0.0063 1.0000
18.750 1.4972 0.08796 0.08328 -0.0234 0.0062 1.0000
19.000 1.4885 0.09255 0.08796 -0.0246 0.0061 1.0000
19.250 1.4788 0.09733 0.09284 -0.0260 0.0060 1.0000
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