DAVIS BASIC B-24 WING AIRFOIL (davis-corrected-il) Xfoil prediction polar at RE=5,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: DAVIS BASIC B-24 WING AIRFOIL (davis-corrected-il) Reynolds number: 5,000,000 Max Cl/Cd: 157.6 at α=7° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-davis-corrected-il-5000000.txt Download as CSV file: xf-davis-corrected-il-5000000.csv |
XFOIL Version 6.96
Calculated polar for: DAVIS BASIC B-24 WING AIRFOIL
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 5.000 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -1.6205 0.03319 0.02946 -0.0611 1.0000 0.0100
-19.500 -1.6207 0.03081 0.02702 -0.0612 1.0000 0.0102
-19.250 -1.6163 0.02895 0.02511 -0.0611 1.0000 0.0103
-19.000 -1.6107 0.02731 0.02342 -0.0606 1.0000 0.0104
-18.750 -1.6051 0.02575 0.02181 -0.0599 1.0000 0.0105
-18.500 -1.5979 0.02441 0.02043 -0.0591 1.0000 0.0107
-18.250 -1.5880 0.02333 0.01931 -0.0581 1.0000 0.0107
-18.000 -1.5785 0.02228 0.01822 -0.0570 1.0000 0.0109
-17.750 -1.5673 0.02138 0.01730 -0.0557 1.0000 0.0110
-17.500 -1.5554 0.02058 0.01646 -0.0544 1.0000 0.0111
-17.250 -1.5430 0.01984 0.01569 -0.0530 1.0000 0.0112
-17.000 -1.5294 0.01919 0.01501 -0.0516 1.0000 0.0113
-16.750 -1.5159 0.01857 0.01436 -0.0500 1.0000 0.0113
-16.500 -1.5002 0.01809 0.01385 -0.0486 1.0000 0.0114
-16.250 -1.4872 0.01748 0.01321 -0.0467 1.0000 0.0116
-16.000 -1.4733 0.01695 0.01265 -0.0448 1.0000 0.0118
-15.750 -1.4606 0.01639 0.01208 -0.0427 1.0000 0.0123
-15.500 -1.4470 0.01594 0.01161 -0.0405 1.0000 0.0126
-15.250 -1.4334 0.01555 0.01120 -0.0381 1.0000 0.0128
-15.000 -1.4176 0.01516 0.01080 -0.0361 1.0000 0.0131
-14.750 -1.3990 0.01479 0.01041 -0.0346 1.0000 0.0132
-14.500 -1.3798 0.01444 0.01006 -0.0332 1.0000 0.0134
-14.250 -1.3600 0.01412 0.00972 -0.0318 1.0000 0.0136
-14.000 -1.3398 0.01382 0.00940 -0.0305 1.0000 0.0137
-13.500 -1.2741 0.01300 0.00857 -0.0331 0.9796 0.0144
-13.250 -1.2014 0.01237 0.00790 -0.0429 0.9433 0.0154
-13.000 -1.1874 0.01232 0.00762 -0.0402 0.8621 0.0156
-12.750 -1.1680 0.01215 0.00734 -0.0385 0.8248 0.0159
-12.500 -1.1470 0.01199 0.00709 -0.0372 0.7941 0.0163
-12.250 -1.1248 0.01181 0.00684 -0.0361 0.7710 0.0164
-12.000 -1.1023 0.01162 0.00659 -0.0351 0.7485 0.0166
-11.750 -1.0801 0.01137 0.00629 -0.0340 0.7311 0.0175
-11.500 -1.0573 0.01114 0.00602 -0.0331 0.7149 0.0182
-11.250 -1.0337 0.01094 0.00578 -0.0322 0.6996 0.0187
-11.000 -1.0096 0.01076 0.00556 -0.0314 0.6834 0.0192
-10.750 -0.9849 0.01060 0.00536 -0.0308 0.6715 0.0194
-10.500 -0.9606 0.01039 0.00513 -0.0300 0.6604 0.0202
-10.000 -0.9112 0.01000 0.00469 -0.0287 0.6377 0.0219
-9.750 -0.8859 0.00985 0.00451 -0.0281 0.6263 0.0225
-9.500 -0.8602 0.00970 0.00433 -0.0276 0.6171 0.0231
-9.250 -0.8350 0.00951 0.00413 -0.0270 0.6075 0.0246
-9.000 -0.8094 0.00934 0.00395 -0.0264 0.5981 0.0256
-8.750 -0.7832 0.00921 0.00379 -0.0260 0.5892 0.0263
-8.500 -0.7572 0.00906 0.00362 -0.0255 0.5814 0.0276
-8.250 -0.7312 0.00890 0.00345 -0.0250 0.5727 0.0291
-8.000 -0.7047 0.00876 0.00330 -0.0247 0.5658 0.0302
-7.750 -0.6785 0.00863 0.00315 -0.0242 0.5559 0.0321
-7.500 -0.6519 0.00848 0.00300 -0.0239 0.5507 0.0339
-7.250 -0.6250 0.00837 0.00288 -0.0235 0.5432 0.0350
-7.000 -0.5985 0.00823 0.00274 -0.0231 0.5362 0.0377
-6.750 -0.5715 0.00811 0.00261 -0.0228 0.5300 0.0397
-6.500 -0.5447 0.00799 0.00249 -0.0225 0.5214 0.0425
-6.250 -0.5176 0.00787 0.00237 -0.0222 0.5169 0.0452
-6.000 -0.4905 0.00775 0.00226 -0.0219 0.5114 0.0485
-5.750 -0.4634 0.00765 0.00215 -0.0216 0.5034 0.0515
-5.500 -0.4361 0.00753 0.00205 -0.0214 0.4992 0.0557
-5.250 -0.4087 0.00744 0.00195 -0.0211 0.4933 0.0594
-5.000 -0.3817 0.00733 0.00185 -0.0208 0.4857 0.0651
-4.750 -0.3541 0.00722 0.00176 -0.0206 0.4824 0.0710
-4.500 -0.3266 0.00712 0.00168 -0.0204 0.4777 0.0759
-4.250 -0.2994 0.00703 0.00159 -0.0201 0.4707 0.0838
-4.000 -0.2717 0.00693 0.00152 -0.0200 0.4659 0.0911
-3.750 -0.2441 0.00684 0.00145 -0.0198 0.4618 0.0990
-3.500 -0.2168 0.00674 0.00138 -0.0195 0.4565 0.1095
-3.250 -0.1894 0.00665 0.00131 -0.0193 0.4501 0.1212
-3.000 -0.1617 0.00654 0.00125 -0.0191 0.4473 0.1336
-2.750 -0.1341 0.00646 0.00120 -0.0190 0.4426 0.1460
-2.500 -0.1066 0.00638 0.00115 -0.0188 0.4367 0.1603
-2.250 -0.0791 0.00628 0.00110 -0.0186 0.4323 0.1777
-2.000 -0.0514 0.00618 0.00106 -0.0184 0.4296 0.1945
-1.750 -0.0238 0.00609 0.00102 -0.0182 0.4255 0.2137
-1.500 0.0036 0.00603 0.00099 -0.0180 0.4194 0.2316
-1.250 0.0313 0.00595 0.00096 -0.0179 0.4152 0.2517
-1.000 0.0590 0.00586 0.00093 -0.0177 0.4123 0.2746
-0.750 0.0864 0.00577 0.00091 -0.0176 0.4085 0.2989
-0.500 0.1139 0.00571 0.00089 -0.0174 0.4033 0.3225
-0.250 0.1414 0.00564 0.00088 -0.0172 0.3988 0.3476
0.000 0.1691 0.00556 0.00087 -0.0171 0.3963 0.3733
0.250 0.1966 0.00549 0.00087 -0.0169 0.3924 0.4002
0.500 0.2240 0.00544 0.00087 -0.0167 0.3879 0.4269
0.750 0.2514 0.00539 0.00088 -0.0165 0.3826 0.4539
1.000 0.2791 0.00532 0.00088 -0.0164 0.3809 0.4812
1.250 0.3066 0.00525 0.00089 -0.0162 0.3779 0.5115
1.500 0.3340 0.00521 0.00091 -0.0161 0.3736 0.5388
1.750 0.3613 0.00519 0.00094 -0.0159 0.3680 0.5655
2.000 0.3888 0.00514 0.00096 -0.0157 0.3655 0.5935
2.250 0.4163 0.00508 0.00098 -0.0155 0.3633 0.6228
2.500 0.4437 0.00506 0.00101 -0.0154 0.3597 0.6492
2.750 0.4709 0.00505 0.00105 -0.0152 0.3551 0.6748
3.000 0.4979 0.00503 0.00109 -0.0149 0.3500 0.7029
3.250 0.5255 0.00500 0.00112 -0.0148 0.3485 0.7271
3.500 0.5527 0.00497 0.00116 -0.0146 0.3459 0.7518
3.750 0.5797 0.00497 0.00121 -0.0143 0.3421 0.7758
4.000 0.6065 0.00500 0.00127 -0.0140 0.3371 0.7977
4.250 0.6335 0.00500 0.00132 -0.0138 0.3336 0.8194
4.500 0.6605 0.00499 0.00137 -0.0135 0.3317 0.8404
4.750 0.6872 0.00500 0.00143 -0.0132 0.3286 0.8600
5.000 0.7133 0.00505 0.00150 -0.0128 0.3220 0.8788
5.250 0.7396 0.00511 0.00158 -0.0124 0.3135 0.8957
5.500 0.7650 0.00523 0.00168 -0.0119 0.3012 0.9119
5.750 0.7911 0.00532 0.00177 -0.0115 0.2934 0.9271
6.000 0.8175 0.00541 0.00187 -0.0112 0.2855 0.9413
6.250 0.8453 0.00548 0.00196 -0.0112 0.2807 0.9534
6.500 0.8740 0.00563 0.00209 -0.0114 0.2710 0.9631
6.750 0.9036 0.00577 0.00220 -0.0119 0.2634 0.9711
7.000 0.9377 0.00595 0.00235 -0.0134 0.2534 0.9754
7.250 0.9691 0.00619 0.00252 -0.0143 0.2399 0.9798
7.500 0.9991 0.00644 0.00270 -0.0150 0.2255 0.9832
7.750 1.0322 0.00680 0.00296 -0.0165 0.2046 0.9844
8.000 1.0616 0.00732 0.00331 -0.0173 0.1755 0.9861
8.250 1.0876 0.00797 0.00376 -0.0175 0.1398 0.9885
8.500 1.1133 0.00852 0.00417 -0.0176 0.1143 0.9912
8.750 1.1372 0.00902 0.00455 -0.0173 0.0953 0.9936
9.000 1.1670 0.00946 0.00490 -0.0182 0.0796 0.9947
9.250 1.1969 0.00985 0.00522 -0.0191 0.0692 0.9958
9.500 1.2266 0.01023 0.00554 -0.0200 0.0605 0.9969
9.750 1.2559 0.01061 0.00587 -0.0208 0.0531 0.9979
10.000 1.2853 0.01097 0.00619 -0.0216 0.0474 0.9987
10.250 1.3143 0.01136 0.00653 -0.0224 0.0421 0.9994
10.500 1.3433 0.01173 0.00687 -0.0232 0.0384 0.9999
10.750 1.3628 0.01203 0.00715 -0.0219 0.0359 1.0000
11.000 1.3762 0.01234 0.00746 -0.0195 0.0336 1.0000
11.250 1.3899 0.01265 0.00776 -0.0171 0.0316 1.0000
11.500 1.4038 0.01298 0.00809 -0.0148 0.0301 1.0000
11.750 1.4109 0.01335 0.00846 -0.0112 0.0281 1.0000
12.000 1.4195 0.01367 0.00879 -0.0079 0.0270 1.0000
12.250 1.4304 0.01409 0.00921 -0.0054 0.0257 1.0000
12.500 1.4414 0.01461 0.00973 -0.0031 0.0240 1.0000
12.750 1.4551 0.01510 0.01024 -0.0015 0.0233 1.0000
13.000 1.4673 0.01573 0.01088 0.0001 0.0222 1.0000
13.250 1.4789 0.01647 0.01163 0.0016 0.0212 1.0000
13.500 1.4910 0.01727 0.01244 0.0029 0.0202 1.0000
13.750 1.5033 0.01813 0.01333 0.0038 0.0197 1.0000
14.000 1.5147 0.01912 0.01434 0.0047 0.0191 1.0000
14.250 1.5239 0.02036 0.01560 0.0056 0.0181 1.0000
14.500 1.5331 0.02168 0.01694 0.0062 0.0172 1.0000
14.750 1.5434 0.02298 0.01827 0.0067 0.0169 1.0000
15.000 1.5523 0.02445 0.01977 0.0071 0.0165 1.0000
15.250 1.5591 0.02613 0.02149 0.0074 0.0160 1.0000
15.500 1.5638 0.02805 0.02343 0.0077 0.0153 1.0000
15.750 1.5677 0.03008 0.02550 0.0080 0.0146 1.0000
16.000 1.5728 0.03201 0.02747 0.0082 0.0145 1.0000
16.250 1.5767 0.03408 0.02958 0.0083 0.0142 1.0000
16.500 1.5792 0.03630 0.03184 0.0084 0.0140 1.0000
16.750 1.5788 0.03881 0.03439 0.0085 0.0135 1.0000
17.000 1.5779 0.04144 0.03707 0.0085 0.0133 1.0000
17.250 1.5751 0.04433 0.04000 0.0084 0.0127 1.0000
17.500 1.5748 0.04700 0.04272 0.0082 0.0127 1.0000
17.750 1.5706 0.05017 0.04593 0.0079 0.0121 1.0000
18.000 1.5690 0.05310 0.04892 0.0075 0.0121 1.0000
18.250 1.5679 0.05598 0.05185 0.0071 0.0119 1.0000
18.500 1.5680 0.05875 0.05466 0.0067 0.0118 1.0000
18.750 1.5641 0.06206 0.05803 0.0061 0.0116 1.0000
19.000 1.5602 0.06536 0.06137 0.0055 0.0115 1.0000
19.250 1.5577 0.06851 0.06456 0.0049 0.0112 1.0000
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