AH 93-W-215 (ah93w215-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: AH 93-W-215 (ah93w215-il) Reynolds number: 1,000,000 Max Cl/Cd: 111.44 at α=9.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-ah93w215-il-1000000.txt Download as CSV file: xf-ah93w215-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: AH 93-W-215
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 1.000 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -1.0856 0.08056 0.07668 -0.0672 1.0000 0.0337
-19.500 -1.0923 0.07642 0.07246 -0.0691 1.0000 0.0339
-19.250 -1.1018 0.07202 0.06797 -0.0710 1.0000 0.0343
-19.000 -1.1162 0.06714 0.06302 -0.0730 1.0000 0.0348
-18.750 -1.1251 0.06303 0.05884 -0.0746 1.0000 0.0352
-18.500 -1.1318 0.05928 0.05503 -0.0759 1.0000 0.0355
-18.250 -1.1347 0.05609 0.05178 -0.0770 1.0000 0.0360
-18.000 -1.1379 0.05294 0.04857 -0.0779 1.0000 0.0365
-17.750 -1.1364 0.05038 0.04595 -0.0785 1.0000 0.0370
-17.500 -1.1362 0.04777 0.04328 -0.0790 1.0000 0.0374
-17.250 -1.1328 0.04556 0.04101 -0.0793 1.0000 0.0379
-17.000 -1.1293 0.04340 0.03878 -0.0795 1.0000 0.0383
-16.750 -1.1298 0.04094 0.03626 -0.0796 1.0000 0.0389
-16.500 -1.1320 0.03845 0.03373 -0.0796 1.0000 0.0395
-16.250 -1.1311 0.03633 0.03157 -0.0793 1.0000 0.0400
-16.000 -1.0973 0.03436 0.02958 -0.0846 0.9978 0.0411
-15.750 -1.0670 0.03256 0.02773 -0.0886 0.9924 0.0421
-15.500 -1.0458 0.03088 0.02599 -0.0903 0.9362 0.0429
-15.250 -0.9299 0.02829 0.02292 -0.1123 0.8204 0.0455
-15.000 -0.9146 0.02728 0.02166 -0.1129 0.7718 0.0463
-14.750 -0.8979 0.02636 0.02060 -0.1133 0.7497 0.0474
-14.500 -0.8812 0.02544 0.01956 -0.1136 0.7347 0.0482
-14.250 -0.8670 0.02432 0.01836 -0.1138 0.7232 0.0491
-14.000 -0.8533 0.02317 0.01715 -0.1140 0.7131 0.0505
-13.750 -0.8360 0.02227 0.01620 -0.1143 0.7047 0.0516
-13.500 -0.8162 0.02152 0.01539 -0.1147 0.6975 0.0528
-13.250 -0.7926 0.02091 0.01468 -0.1156 0.6904 0.0539
-13.000 -0.7739 0.01999 0.01373 -0.1161 0.6853 0.0554
-12.750 -0.7535 0.01921 0.01293 -0.1166 0.6803 0.0569
-12.500 -0.7319 0.01863 0.01230 -0.1169 0.6752 0.0585
-12.250 -0.7089 0.01816 0.01176 -0.1172 0.6696 0.0600
-12.000 -0.6913 0.01750 0.01108 -0.1169 0.6658 0.0616
-11.750 -0.6737 0.01690 0.01048 -0.1163 0.6619 0.0636
-11.500 -0.6543 0.01642 0.00997 -0.1158 0.6576 0.0654
-11.250 -0.6334 0.01605 0.00954 -0.1154 0.6535 0.0669
-11.000 -0.6160 0.01554 0.00900 -0.1146 0.6488 0.0693
-10.750 -0.5986 0.01510 0.00855 -0.1135 0.6461 0.0713
-10.500 -0.5798 0.01475 0.00819 -0.1125 0.6434 0.0736
-10.250 -0.5624 0.01438 0.00780 -0.1112 0.6403 0.0757
-10.000 -0.5468 0.01399 0.00740 -0.1096 0.6370 0.0783
-9.750 -0.5298 0.01368 0.00707 -0.1081 0.6334 0.0810
-9.500 -0.5119 0.01344 0.00677 -0.1066 0.6295 0.0834
-9.250 -0.4977 0.01310 0.00645 -0.1045 0.6267 0.0869
-9.000 -0.4818 0.01283 0.00618 -0.1024 0.6246 0.0898
-8.750 -0.4655 0.01260 0.00594 -0.1004 0.6223 0.0929
-8.500 -0.4526 0.01235 0.00571 -0.0977 0.6197 0.0966
-8.250 -0.4377 0.01219 0.00554 -0.0953 0.6169 0.0999
-8.000 -0.4199 0.01202 0.00534 -0.0935 0.6140 0.1037
-7.750 -0.4017 0.01182 0.00515 -0.0917 0.6107 0.1087
-7.500 -0.3800 0.01170 0.00500 -0.0906 0.6074 0.1128
-7.250 -0.3610 0.01146 0.00481 -0.0890 0.6058 0.1187
-7.000 -0.3393 0.01130 0.00465 -0.0879 0.6038 0.1240
-6.750 -0.3190 0.01108 0.00448 -0.0865 0.6015 0.1311
-6.500 -0.2967 0.01093 0.00433 -0.0855 0.5989 0.1370
-6.250 -0.2757 0.01074 0.00416 -0.0842 0.5963 0.1453
-6.000 -0.2530 0.01060 0.00402 -0.0832 0.5937 0.1528
-5.750 -0.2309 0.01044 0.00389 -0.0821 0.5908 0.1621
-5.500 -0.2073 0.01032 0.00377 -0.0814 0.5877 0.1715
-5.250 -0.1841 0.01016 0.00365 -0.0804 0.5861 0.1815
-5.000 -0.1618 0.00995 0.00351 -0.0794 0.5840 0.1949
-4.750 -0.1390 0.00977 0.00339 -0.0784 0.5818 0.2092
-4.500 -0.1160 0.00959 0.00326 -0.0775 0.5796 0.2246
-4.250 -0.0931 0.00941 0.00314 -0.0765 0.5772 0.2425
-4.000 -0.0707 0.00922 0.00302 -0.0755 0.5746 0.2644
-3.750 -0.0485 0.00903 0.00291 -0.0744 0.5716 0.2919
-3.500 -0.0257 0.00885 0.00282 -0.0735 0.5686 0.3241
-3.250 -0.0038 0.00860 0.00272 -0.0724 0.5672 0.3570
-3.000 0.0187 0.00840 0.00264 -0.0713 0.5651 0.3891
-2.750 0.0423 0.00824 0.00258 -0.0704 0.5629 0.4168
-2.500 0.0666 0.00813 0.00253 -0.0697 0.5605 0.4397
-2.250 0.0913 0.00804 0.00249 -0.0690 0.5581 0.4601
-2.000 0.1161 0.00798 0.00246 -0.0683 0.5555 0.4773
-1.750 0.1414 0.00796 0.00245 -0.0677 0.5524 0.4926
-1.500 0.1679 0.00796 0.00246 -0.0674 0.5495 0.5059
-1.250 0.1934 0.00791 0.00244 -0.0668 0.5477 0.5190
-1.000 0.2189 0.00786 0.00243 -0.0663 0.5454 0.5296
-0.750 0.2450 0.00783 0.00242 -0.0658 0.5429 0.5400
-0.500 0.2704 0.00780 0.00241 -0.0652 0.5404 0.5501
-0.250 0.2961 0.00780 0.00240 -0.0647 0.5375 0.5597
0.000 0.3215 0.00782 0.00241 -0.0641 0.5344 0.5680
0.250 0.3478 0.00786 0.00245 -0.0638 0.5313 0.5771
0.500 0.3736 0.00783 0.00245 -0.0633 0.5293 0.5855
0.750 0.3986 0.00780 0.00246 -0.0626 0.5268 0.5946
1.000 0.4245 0.00780 0.00247 -0.0621 0.5240 0.6034
1.250 0.4487 0.00778 0.00249 -0.0613 0.5210 0.6133
1.500 0.4734 0.00781 0.00251 -0.0606 0.5179 0.6233
1.750 0.4973 0.00785 0.00256 -0.0598 0.5141 0.6348
2.000 0.5225 0.00786 0.00259 -0.0591 0.5117 0.6443
2.250 0.5465 0.00783 0.00262 -0.0583 0.5090 0.6537
2.500 0.5709 0.00783 0.00265 -0.0575 0.5058 0.6623
2.750 0.5942 0.00784 0.00267 -0.0565 0.5025 0.6707
3.000 0.6154 0.00787 0.00271 -0.0551 0.4989 0.6798
3.250 0.6382 0.00794 0.00276 -0.0540 0.4951 0.6880
3.500 0.6601 0.00791 0.00281 -0.0527 0.4924 0.6979
3.750 0.6829 0.00792 0.00284 -0.0517 0.4889 0.7072
4.000 0.7042 0.00793 0.00290 -0.0503 0.4853 0.7173
4.250 0.7248 0.00800 0.00297 -0.0488 0.4812 0.7277
4.500 0.7457 0.00807 0.00307 -0.0473 0.4773 0.7381
4.750 0.7688 0.00810 0.00314 -0.0463 0.4738 0.7485
5.000 0.7904 0.00814 0.00323 -0.0450 0.4695 0.7591
5.250 0.8108 0.00823 0.00332 -0.0435 0.4651 0.7698
5.500 0.8288 0.00834 0.00345 -0.0416 0.4603 0.7810
5.750 0.8514 0.00840 0.00355 -0.0405 0.4567 0.7911
6.000 0.8719 0.00846 0.00367 -0.0390 0.4521 0.8018
6.500 0.9089 0.00870 0.00394 -0.0354 0.4418 0.8233
6.750 0.9305 0.00879 0.00406 -0.0342 0.4373 0.8332
7.000 0.9493 0.00891 0.00422 -0.0325 0.4316 0.8441
7.250 0.9650 0.00910 0.00440 -0.0302 0.4257 0.8547
7.500 0.9866 0.00919 0.00455 -0.0291 0.4212 0.8659
7.750 1.0063 0.00934 0.00473 -0.0277 0.4151 0.8766
8.250 1.0493 0.00969 0.00516 -0.0258 0.4036 0.9006
8.500 1.0764 0.00992 0.00540 -0.0262 0.3965 0.9123
8.750 1.1087 0.01019 0.00569 -0.0277 0.3893 0.9238
9.000 1.1518 0.01046 0.00599 -0.0316 0.3812 0.9326
9.250 1.1954 0.01084 0.00636 -0.0357 0.3723 0.9412
9.500 1.2426 0.01115 0.00669 -0.0404 0.3644 0.9482
9.750 1.2842 0.01157 0.00710 -0.0442 0.3558 0.9576
10.250 1.3480 0.01255 0.00807 -0.0477 0.3380 1.0000
10.500 1.3635 0.01303 0.00854 -0.0462 0.3300 1.0000
10.750 1.3752 0.01368 0.00916 -0.0443 0.3222 1.0000
11.000 1.3895 0.01428 0.00976 -0.0429 0.3141 1.0000
11.250 1.3983 0.01517 0.01062 -0.0409 0.3055 1.0000
11.500 1.4096 0.01602 0.01147 -0.0394 0.2967 1.0000
11.750 1.4172 0.01715 0.01259 -0.0378 0.2890 1.0000
12.000 1.4277 0.01821 0.01365 -0.0366 0.2810 1.0000
12.250 1.4326 0.01969 0.01512 -0.0351 0.2728 1.0000
12.500 1.4421 0.02095 0.01639 -0.0341 0.2654 1.0000
12.750 1.4443 0.02274 0.01817 -0.0327 0.2574 1.0000
13.000 1.4516 0.02421 0.01964 -0.0317 0.2495 1.0000
13.250 1.4514 0.02623 0.02165 -0.0303 0.2418 1.0000
13.500 1.4570 0.02785 0.02329 -0.0293 0.2340 1.0000
13.750 1.4538 0.03011 0.02553 -0.0279 0.2260 1.0000
14.000 1.4577 0.03187 0.02730 -0.0269 0.2180 1.0000
14.250 1.4547 0.03420 0.02961 -0.0256 0.2103 1.0000
14.500 1.4574 0.03614 0.03156 -0.0247 0.2034 1.0000
14.750 1.4535 0.03865 0.03405 -0.0236 0.1957 1.0000
15.000 1.4577 0.04054 0.03596 -0.0229 0.1890 1.0000
15.500 1.4562 0.04528 0.04068 -0.0214 0.1740 1.0000
15.750 1.4517 0.04807 0.04346 -0.0206 0.1668 1.0000
16.000 1.4545 0.05020 0.04560 -0.0201 0.1599 1.0000
16.250 1.4499 0.05309 0.04847 -0.0195 0.1532 1.0000
16.500 1.4519 0.05537 0.05075 -0.0192 0.1462 1.0000
16.750 1.4475 0.05834 0.05373 -0.0187 0.1401 1.0000
17.000 1.4503 0.06062 0.05601 -0.0185 0.1342 1.0000
17.250 1.4441 0.06383 0.05921 -0.0182 0.1269 1.0000
17.500 1.4460 0.06626 0.06165 -0.0180 0.1218 1.0000
17.750 1.4404 0.06952 0.06491 -0.0179 0.1158 1.0000
18.000 1.4423 0.07201 0.06742 -0.0179 0.1112 1.0000
18.500 1.4371 0.07806 0.07349 -0.0180 0.1011 1.0000
18.750 1.4310 0.08155 0.07698 -0.0182 0.0961 1.0000
19.000 1.4313 0.08433 0.07979 -0.0185 0.0919 1.0000
19.250 1.4253 0.08788 0.08334 -0.0188 0.0872 1.0000
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