KC-135 BL52.44 AIRFOIL (kc135a-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: KC-135 BL52.44 AIRFOIL (kc135a-il) Reynolds number: 1,000,000 Max Cl/Cd: 82.52 at α=8.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-kc135a-il-1000000-n5.txt Download as CSV file: xf-kc135a-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: KC-135 BL52.44 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
------ -------- --------- --------- -------- -------- --------
-19.000 -1.0177 0.09739 0.09455 -0.0347 1.0000 0.0100
-18.750 -1.0437 0.08883 0.08582 -0.0395 1.0000 0.0100
-18.500 -1.0694 0.08084 0.07767 -0.0438 1.0000 0.0100
-18.250 -1.0761 0.07616 0.07288 -0.0461 1.0000 0.0100
-18.000 -1.0948 0.06992 0.06649 -0.0491 1.0000 0.0100
-17.750 -1.1101 0.06451 0.06094 -0.0515 1.0000 0.0101
-17.500 -1.1210 0.05991 0.05622 -0.0532 1.0000 0.0102
-17.250 -1.1259 0.05626 0.05246 -0.0545 1.0000 0.0102
-17.000 -1.1322 0.05263 0.04872 -0.0555 1.0000 0.0102
-16.750 -1.1380 0.04917 0.04515 -0.0564 1.0000 0.0103
-16.500 -1.1386 0.04642 0.04231 -0.0568 1.0000 0.0103
-16.250 -1.1385 0.04383 0.03964 -0.0572 1.0000 0.0104
-16.000 -1.1371 0.04142 0.03713 -0.0573 1.0000 0.0104
-15.750 -1.1349 0.03914 0.03478 -0.0573 1.0000 0.0105
-15.500 -1.1305 0.03713 0.03270 -0.0573 1.0000 0.0106
-15.250 -1.1232 0.03544 0.03095 -0.0571 1.0000 0.0107
-15.000 -1.1190 0.03349 0.02890 -0.0567 1.0000 0.0107
-14.750 -1.1118 0.03187 0.02721 -0.0563 1.0000 0.0108
-14.500 -1.1036 0.03037 0.02564 -0.0558 1.0000 0.0108
-14.250 -1.0950 0.02897 0.02417 -0.0551 1.0000 0.0109
-14.000 -1.0837 0.02783 0.02299 -0.0544 1.0000 0.0111
-13.750 -1.0753 0.02651 0.02159 -0.0535 1.0000 0.0112
-13.500 -1.0650 0.02539 0.02042 -0.0524 1.0000 0.0112
-13.250 -1.0535 0.02443 0.01941 -0.0514 1.0000 0.0114
-13.000 -1.0434 0.02342 0.01833 -0.0500 1.0000 0.0114
-12.750 -1.0327 0.02251 0.01737 -0.0485 1.0000 0.0116
-12.500 -1.0231 0.02160 0.01639 -0.0467 1.0000 0.0116
-12.250 -1.0123 0.02084 0.01558 -0.0449 1.0000 0.0117
-12.000 -1.0022 0.02012 0.01481 -0.0427 1.0000 0.0118
-11.750 -0.9924 0.01947 0.01411 -0.0403 1.0000 0.0119
-11.500 -0.9819 0.01884 0.01343 -0.0379 0.9917 0.0120
-11.250 -0.9446 0.01803 0.01257 -0.0409 0.9726 0.0121
-11.000 -0.8876 0.01709 0.01155 -0.0481 0.9519 0.0123
-10.750 -0.8318 0.01633 0.01063 -0.0549 0.9077 0.0124
-10.500 -0.8206 0.01590 0.00997 -0.0522 0.8499 0.0126
-10.250 -0.8112 0.01557 0.00947 -0.0490 0.8118 0.0128
-10.000 -0.7999 0.01525 0.00903 -0.0461 0.7872 0.0130
-9.750 -0.7869 0.01496 0.00865 -0.0435 0.7695 0.0132
-9.500 -0.7704 0.01465 0.00826 -0.0416 0.7556 0.0134
-9.250 -0.7524 0.01433 0.00788 -0.0399 0.7436 0.0136
-9.000 -0.7335 0.01402 0.00751 -0.0384 0.7333 0.0140
-8.750 -0.7136 0.01373 0.00716 -0.0371 0.7238 0.0142
-8.500 -0.6933 0.01344 0.00681 -0.0358 0.7160 0.0145
-8.250 -0.6721 0.01316 0.00648 -0.0347 0.7084 0.0149
-8.000 -0.6508 0.01289 0.00615 -0.0335 0.7014 0.0152
-7.750 -0.6290 0.01260 0.00585 -0.0325 0.6951 0.0159
-7.500 -0.6066 0.01235 0.00557 -0.0316 0.6884 0.0165
-7.250 -0.5837 0.01212 0.00530 -0.0307 0.6825 0.0172
-7.000 -0.5603 0.01189 0.00504 -0.0299 0.6765 0.0179
-6.750 -0.5369 0.01167 0.00478 -0.0291 0.6707 0.0188
-6.500 -0.5130 0.01147 0.00456 -0.0284 0.6657 0.0197
-6.250 -0.4884 0.01127 0.00435 -0.0278 0.6610 0.0209
-6.000 -0.4638 0.01108 0.00414 -0.0273 0.6559 0.0221
-5.750 -0.4393 0.01090 0.00394 -0.0267 0.6509 0.0235
-5.500 -0.4141 0.01073 0.00375 -0.0262 0.6466 0.0247
-5.250 -0.3886 0.01057 0.00357 -0.0257 0.6418 0.0260
-5.000 -0.3635 0.01040 0.00340 -0.0252 0.6365 0.0277
-4.750 -0.3380 0.01027 0.00323 -0.0248 0.6312 0.0292
-4.500 -0.3120 0.01012 0.00307 -0.0244 0.6265 0.0308
-4.250 -0.2862 0.00997 0.00292 -0.0240 0.6214 0.0330
-4.000 -0.2603 0.00985 0.00278 -0.0237 0.6164 0.0353
-3.750 -0.2343 0.00970 0.00265 -0.0233 0.6120 0.0392
-3.500 -0.2080 0.00957 0.00253 -0.0230 0.6071 0.0438
-3.000 -0.1559 0.00931 0.00228 -0.0223 0.5972 0.0573
-2.750 -0.1301 0.00913 0.00216 -0.0219 0.5921 0.0728
-2.500 -0.1059 0.00884 0.00201 -0.0213 0.5868 0.1182
-2.250 -0.0974 0.00733 0.00149 -0.0182 0.5822 0.3921
-2.000 -0.0733 0.00704 0.00141 -0.0176 0.5782 0.4516
-1.750 -0.0471 0.00692 0.00137 -0.0172 0.5735 0.4821
-1.500 -0.0204 0.00685 0.00135 -0.0170 0.5684 0.5073
-1.250 0.0066 0.00682 0.00133 -0.0168 0.5632 0.5240
-1.000 0.0342 0.00680 0.00132 -0.0167 0.5576 0.5342
-0.750 0.0615 0.00679 0.00132 -0.0165 0.5520 0.5463
-0.250 0.1169 0.00679 0.00132 -0.0164 0.5427 0.5641
0.000 0.1448 0.00680 0.00132 -0.0164 0.5377 0.5687
0.250 0.1725 0.00685 0.00132 -0.0163 0.5310 0.5722
0.500 0.2003 0.00687 0.00132 -0.0163 0.5213 0.5757
0.750 0.2274 0.00691 0.00133 -0.0161 0.5121 0.5797
1.000 0.2552 0.00693 0.00135 -0.0161 0.5052 0.5836
1.500 0.3108 0.00701 0.00140 -0.0161 0.4932 0.5907
1.750 0.3383 0.00704 0.00143 -0.0160 0.4871 0.5947
2.000 0.3655 0.00708 0.00147 -0.0159 0.4810 0.5991
2.250 0.3932 0.00711 0.00150 -0.0159 0.4739 0.6033
2.500 0.4204 0.00718 0.00155 -0.0158 0.4666 0.6072
2.750 0.4479 0.00723 0.00160 -0.0157 0.4583 0.6110
3.000 0.4745 0.00729 0.00166 -0.0155 0.4487 0.6159
3.250 0.5013 0.00736 0.00172 -0.0153 0.4366 0.6211
3.500 0.5278 0.00747 0.00180 -0.0151 0.4216 0.6257
3.750 0.5529 0.00762 0.00189 -0.0147 0.4000 0.6306
4.000 0.5770 0.00784 0.00202 -0.0140 0.3727 0.6363
4.250 0.6005 0.00810 0.00218 -0.0133 0.3442 0.6423
4.500 0.6235 0.00837 0.00236 -0.0126 0.3166 0.6487
4.750 0.6468 0.00862 0.00254 -0.0118 0.2932 0.6562
5.250 0.6929 0.00910 0.00292 -0.0103 0.2516 0.6724
5.500 0.7161 0.00932 0.00310 -0.0096 0.2360 0.6822
5.750 0.7393 0.00950 0.00329 -0.0088 0.2237 0.6944
6.000 0.7619 0.00970 0.00349 -0.0079 0.2115 0.7075
6.250 0.7844 0.00988 0.00369 -0.0071 0.1998 0.7224
6.500 0.8055 0.01009 0.00391 -0.0059 0.1856 0.7414
6.750 0.8246 0.01035 0.00416 -0.0045 0.1684 0.7655
7.000 0.8432 0.01057 0.00441 -0.0029 0.1539 0.7945
7.250 0.8612 0.01074 0.00466 -0.0011 0.1422 0.8307
7.500 0.8794 0.01088 0.00492 0.0007 0.1338 0.8743
7.750 0.9051 0.01111 0.00525 0.0008 0.1234 0.9248
8.000 0.9541 0.01160 0.00572 -0.0045 0.1094 0.9563
8.250 0.9985 0.01210 0.00617 -0.0087 0.0972 0.9704
8.500 1.0340 0.01257 0.00659 -0.0111 0.0868 0.9800
8.750 1.0631 0.01301 0.00700 -0.0120 0.0779 0.9887
9.000 1.0866 0.01348 0.00743 -0.0118 0.0694 0.9985
9.250 1.1061 0.01397 0.00787 -0.0108 0.0610 1.0000
9.500 1.1124 0.01438 0.00825 -0.0070 0.0544 1.0000
9.750 1.1179 0.01484 0.00869 -0.0032 0.0474 1.0000
10.000 1.1254 0.01537 0.00918 0.0000 0.0411 1.0000
10.250 1.1347 0.01592 0.00973 0.0027 0.0366 1.0000
10.500 1.1452 0.01651 0.01031 0.0051 0.0329 1.0000
10.750 1.1562 0.01714 0.01095 0.0072 0.0298 1.0000
11.000 1.1674 0.01782 0.01164 0.0091 0.0276 1.0000
11.250 1.1792 0.01854 0.01238 0.0107 0.0257 1.0000
11.500 1.1916 0.01928 0.01315 0.0121 0.0244 1.0000
11.750 1.2031 0.02014 0.01403 0.0135 0.0232 1.0000
12.000 1.2149 0.02104 0.01496 0.0147 0.0219 1.0000
12.250 1.2275 0.02194 0.01590 0.0157 0.0213 1.0000
12.500 1.2395 0.02293 0.01692 0.0166 0.0206 1.0000
12.750 1.2498 0.02408 0.01810 0.0175 0.0196 1.0000
13.000 1.2604 0.02526 0.01932 0.0183 0.0190 1.0000
13.250 1.2713 0.02646 0.02056 0.0190 0.0185 1.0000
13.500 1.2822 0.02768 0.02183 0.0196 0.0180 1.0000
13.750 1.2921 0.02900 0.02321 0.0201 0.0175 1.0000
14.000 1.3011 0.03044 0.02469 0.0207 0.0171 1.0000
14.250 1.3095 0.03194 0.02624 0.0211 0.0168 1.0000
14.500 1.3162 0.03361 0.02795 0.0216 0.0161 1.0000
14.750 1.3217 0.03542 0.02981 0.0220 0.0156 1.0000
15.000 1.3294 0.03707 0.03152 0.0223 0.0154 1.0000
15.250 1.3356 0.03886 0.03338 0.0226 0.0151 1.0000
15.500 1.3413 0.04075 0.03534 0.0228 0.0147 1.0000
15.750 1.3465 0.04275 0.03739 0.0228 0.0144 1.0000
16.000 1.3504 0.04492 0.03962 0.0229 0.0141 1.0000
16.250 1.3533 0.04721 0.04198 0.0228 0.0137 1.0000
16.500 1.3558 0.04964 0.04446 0.0227 0.0135 1.0000
16.750 1.3568 0.05230 0.04718 0.0224 0.0132 1.0000
17.000 1.3559 0.05520 0.05016 0.0220 0.0129 1.0000
17.250 1.3573 0.05791 0.05294 0.0215 0.0127 1.0000
17.500 1.3579 0.06076 0.05588 0.0210 0.0125 1.0000
17.750 1.3583 0.06369 0.05888 0.0204 0.0122 1.0000
18.000 1.3563 0.06695 0.06223 0.0196 0.0121 1.0000
18.250 1.3542 0.07027 0.06562 0.0188 0.0118 1.0000
18.500 1.3496 0.07399 0.06943 0.0177 0.0116 1.0000
18.750 1.3441 0.07791 0.07344 0.0165 0.0114 1.0000
19.000 1.3378 0.08199 0.07760 0.0153 0.0113 1.0000
19.250 1.3300 0.08634 0.08203 0.0138 0.0111 1.0000
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