AH 94-W-301 (ah94w301-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: AH 94-W-301 (ah94w301-il) Reynolds number: 1,000,000 Max Cl/Cd: 99.02 at α=8.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-ah94w301-il-1000000-n5.txt Download as CSV file: xf-ah94w301-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: AH 94-W-301
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 -1.1258 0.09841 0.09423 -0.0290 1.0000 0.1346
-18.750 -1.1257 0.09550 0.09131 -0.0299 1.0000 0.1376
-18.500 -1.1244 0.09273 0.08853 -0.0307 1.0000 0.1405
-18.250 -1.1230 0.09000 0.08576 -0.0314 1.0000 0.1429
-18.000 -1.1242 0.08702 0.08278 -0.0321 1.0000 0.1461
-17.750 -1.1277 0.08380 0.07955 -0.0328 1.0000 0.1494
-17.500 -1.1266 0.08110 0.07683 -0.0334 1.0000 0.1523
-17.250 -1.1202 0.07901 0.07472 -0.0339 1.0000 0.1547
-17.000 -1.1232 0.07594 0.07164 -0.0344 1.0000 0.1578
-16.750 -1.1209 0.07255 0.06824 -0.0363 0.9973 0.1617
-16.500 -1.0743 0.06874 0.06411 -0.0469 0.8671 0.1664
-16.250 -1.0754 0.06631 0.06141 -0.0468 0.8115 0.1692
-16.000 -1.0769 0.06362 0.05862 -0.0471 0.7861 0.1728
-15.750 -1.0739 0.06134 0.05625 -0.0475 0.7664 0.1762
-15.500 -1.0706 0.05902 0.05385 -0.0479 0.7501 0.1791
-15.250 -1.0654 0.05695 0.05170 -0.0483 0.7356 0.1822
-15.000 -1.0684 0.05411 0.04881 -0.0486 0.7214 0.1862
-14.750 -1.0656 0.05183 0.04648 -0.0489 0.7093 0.1901
-14.500 -1.0574 0.05008 0.04465 -0.0492 0.6962 0.1932
-14.250 -1.0568 0.04760 0.04212 -0.0495 0.6867 0.1965
-14.000 -1.0549 0.04532 0.03981 -0.0497 0.6770 0.2004
-13.750 -1.0516 0.04313 0.03756 -0.0499 0.6685 0.2043
-13.500 -1.0428 0.04146 0.03585 -0.0502 0.6606 0.2075
-13.250 -1.0399 0.03933 0.03367 -0.0503 0.6519 0.2112
-13.000 -1.0392 0.03702 0.03133 -0.0503 0.6444 0.2155
-12.750 -1.0324 0.03525 0.02952 -0.0505 0.6370 0.2194
-12.500 -1.0233 0.03369 0.02790 -0.0506 0.6289 0.2223
-12.250 -1.0209 0.03166 0.02584 -0.0505 0.6221 0.2263
-12.000 -1.0185 0.02969 0.02385 -0.0503 0.6170 0.2305
-11.750 -1.0118 0.02806 0.02219 -0.0502 0.6112 0.2343
-11.500 -1.0003 0.02681 0.02089 -0.0502 0.6050 0.2374
-11.250 -0.9979 0.02490 0.01895 -0.0499 0.5994 0.2417
-11.000 -0.9911 0.02331 0.01734 -0.0497 0.5951 0.2458
-10.750 -0.9799 0.02204 0.01605 -0.0496 0.5896 0.2496
-10.500 -0.9664 0.02095 0.01491 -0.0496 0.5836 0.2526
-10.000 -0.9502 0.01817 0.01209 -0.0487 0.5742 0.2607
-9.750 -0.9438 0.01710 0.01099 -0.0475 0.5704 0.2643
-9.500 -0.9241 0.01633 0.01018 -0.0481 0.5659 0.2675
-9.250 -0.9026 0.01550 0.00931 -0.0492 0.5613 0.2710
-9.000 -0.8781 0.01472 0.00850 -0.0508 0.5563 0.2753
-8.750 -0.8503 0.01421 0.00797 -0.0523 0.5524 0.2795
-8.500 -0.8215 0.01390 0.00763 -0.0534 0.5484 0.2827
-8.250 -0.7925 0.01362 0.00732 -0.0545 0.5439 0.2858
-8.000 -0.7636 0.01327 0.00696 -0.0557 0.5395 0.2901
-7.750 -0.7339 0.01302 0.00669 -0.0568 0.5352 0.2940
-7.500 -0.7035 0.01282 0.00647 -0.0579 0.5317 0.2976
-7.250 -0.6726 0.01266 0.00629 -0.0590 0.5287 0.3004
-7.000 -0.6417 0.01244 0.00607 -0.0602 0.5250 0.3040
-6.750 -0.6107 0.01224 0.00586 -0.0614 0.5209 0.3078
-6.500 -0.5795 0.01209 0.00569 -0.0625 0.5168 0.3116
-6.250 -0.5481 0.01198 0.00555 -0.0636 0.5129 0.3149
-6.000 -0.5164 0.01188 0.00543 -0.0647 0.5101 0.3173
-5.750 -0.4845 0.01171 0.00527 -0.0659 0.5076 0.3210
-5.500 -0.4525 0.01156 0.00512 -0.0671 0.5043 0.3249
-5.250 -0.4205 0.01146 0.00500 -0.0683 0.5007 0.3283
-5.000 -0.3885 0.01138 0.00490 -0.0694 0.4970 0.3313
-4.750 -0.3566 0.01133 0.00482 -0.0704 0.4935 0.3340
-4.500 -0.3245 0.01124 0.00472 -0.0715 0.4901 0.3372
-4.250 -0.2920 0.01113 0.00462 -0.0727 0.4882 0.3406
-4.000 -0.2595 0.01104 0.00453 -0.0739 0.4859 0.3440
-3.750 -0.2271 0.01097 0.00447 -0.0750 0.4831 0.3474
-3.500 -0.1948 0.01093 0.00440 -0.0761 0.4800 0.3501
-3.250 -0.1626 0.01090 0.00435 -0.0771 0.4765 0.3521
-3.000 -0.1303 0.01084 0.00428 -0.0782 0.4729 0.3555
-2.750 -0.0980 0.01079 0.00423 -0.0793 0.4697 0.3590
-2.500 -0.0653 0.01073 0.00418 -0.0804 0.4680 0.3625
-2.250 -0.0328 0.01069 0.00415 -0.0814 0.4658 0.3655
-2.000 -0.0003 0.01067 0.00412 -0.0825 0.4634 0.3680
-1.750 0.0320 0.01066 0.00409 -0.0835 0.4608 0.3699
-1.500 0.0645 0.01061 0.00406 -0.0845 0.4579 0.3737
-1.250 0.0968 0.01059 0.00403 -0.0855 0.4547 0.3773
-1.000 0.1288 0.01060 0.00403 -0.0865 0.4511 0.3804
-0.750 0.1611 0.01059 0.00402 -0.0874 0.4488 0.3833
-0.500 0.1936 0.01058 0.00402 -0.0884 0.4469 0.3859
-0.250 0.2259 0.01059 0.00402 -0.0893 0.4447 0.3882
0.000 0.2583 0.01056 0.00401 -0.0903 0.4422 0.3916
0.250 0.2906 0.01056 0.00402 -0.0912 0.4396 0.3947
0.500 0.3226 0.01057 0.00403 -0.0921 0.4368 0.3978
0.750 0.3544 0.01060 0.00406 -0.0929 0.4337 0.4010
1.000 0.3859 0.01065 0.00409 -0.0937 0.4304 0.4036
1.250 0.4181 0.01067 0.00411 -0.0946 0.4286 0.4055
1.500 0.4502 0.01068 0.00413 -0.0954 0.4267 0.4082
1.750 0.4823 0.01068 0.00416 -0.0963 0.4245 0.4113
2.000 0.5142 0.01070 0.00420 -0.0971 0.4221 0.4144
2.250 0.5458 0.01074 0.00425 -0.0979 0.4194 0.4177
2.500 0.5771 0.01080 0.00430 -0.0985 0.4164 0.4206
2.750 0.6081 0.01088 0.00436 -0.0991 0.4132 0.4230
3.000 0.6393 0.01094 0.00443 -0.0998 0.4108 0.4248
3.250 0.6711 0.01096 0.00448 -0.1005 0.4092 0.4279
3.500 0.7027 0.01099 0.00454 -0.1013 0.4071 0.4312
3.750 0.7340 0.01104 0.00461 -0.1019 0.4046 0.4346
4.000 0.7650 0.01110 0.00469 -0.1025 0.4018 0.4378
4.250 0.7956 0.01118 0.00477 -0.1030 0.3992 0.4405
4.500 0.8259 0.01128 0.00486 -0.1035 0.3966 0.4427
4.750 0.8558 0.01139 0.00496 -0.1039 0.3935 0.4447
5.000 0.8867 0.01144 0.00506 -0.1044 0.3916 0.4484
5.250 0.9176 0.01150 0.00515 -0.1050 0.3895 0.4519
5.500 0.9481 0.01157 0.00525 -0.1054 0.3874 0.4551
5.750 0.9782 0.01165 0.00536 -0.1058 0.3850 0.4579
6.000 1.0078 0.01176 0.00547 -0.1061 0.3823 0.4604
6.250 1.0369 0.01189 0.00560 -0.1063 0.3793 0.4626
6.500 1.0655 0.01203 0.00574 -0.1064 0.3762 0.4650
6.750 1.0946 0.01214 0.00588 -0.1067 0.3739 0.4689
7.000 1.1243 0.01222 0.00601 -0.1070 0.3718 0.4722
7.250 1.1534 0.01233 0.00615 -0.1071 0.3692 0.4752
7.500 1.1818 0.01245 0.00630 -0.1072 0.3661 0.4781
7.750 1.2091 0.01262 0.00646 -0.1071 0.3623 0.4806
8.000 1.2347 0.01283 0.00666 -0.1066 0.3577 0.4829
8.250 1.2623 0.01297 0.00683 -0.1065 0.3544 0.4856
8.500 1.2894 0.01310 0.00700 -0.1064 0.3509 0.4894
8.750 1.3150 0.01328 0.00720 -0.1059 0.3463 0.4928
9.000 1.3368 0.01358 0.00748 -0.1048 0.3396 0.4958
9.250 1.3615 0.01377 0.00769 -0.1042 0.3339 0.4987
9.500 1.3834 0.01403 0.00795 -0.1031 0.3277 0.5013
9.750 1.3988 0.01438 0.00829 -0.1009 0.3220 0.5037
10.000 1.4171 0.01462 0.00856 -0.0991 0.3172 0.5065
10.250 1.4346 0.01502 0.00897 -0.0973 0.3098 0.5103
10.500 1.4506 0.01553 0.00947 -0.0954 0.3025 0.5136
10.750 1.4667 0.01607 0.01000 -0.0936 0.2934 0.5167
11.000 1.4796 0.01675 0.01067 -0.0915 0.2845 0.5196
11.250 1.4897 0.01761 0.01150 -0.0891 0.2740 0.5222
11.500 1.4996 0.01854 0.01242 -0.0869 0.2639 0.5247
11.750 1.5047 0.01983 0.01368 -0.0844 0.2532 0.5269
12.000 1.5064 0.02150 0.01533 -0.0821 0.2408 0.5306
12.250 1.5089 0.02332 0.01715 -0.0802 0.2288 0.5340
12.500 1.5079 0.02556 0.01938 -0.0785 0.2172 0.5370
12.750 1.5024 0.02830 0.02211 -0.0768 0.2052 0.5396
13.000 1.4952 0.03128 0.02508 -0.0752 0.1945 0.5421
13.250 1.4877 0.03438 0.02818 -0.0739 0.1842 0.5443
13.500 1.4775 0.03778 0.03159 -0.0725 0.1750 0.5462
13.750 1.4635 0.04155 0.03536 -0.0712 0.1660 0.5477
14.000 1.4537 0.04504 0.03888 -0.0701 0.1582 0.5503
14.250 1.4406 0.04897 0.04283 -0.0692 0.1502 0.5531
14.500 1.4285 0.05289 0.04679 -0.0684 0.1429 0.5561
14.750 1.4194 0.05660 0.05052 -0.0678 0.1358 0.5591
15.000 1.4091 0.06049 0.05442 -0.0673 0.1294 0.5620
15.250 1.3997 0.06435 0.05831 -0.0669 0.1228 0.5647
15.500 1.3906 0.06825 0.06223 -0.0666 0.1170 0.5670
15.750 1.3844 0.07187 0.06586 -0.0664 0.1111 0.5691
16.250 1.3716 0.07927 0.07331 -0.0662 0.1008 0.5742
16.500 1.3659 0.08300 0.07708 -0.0663 0.0967 0.5773
16.750 1.3627 0.08644 0.08055 -0.0664 0.0918 0.5804
17.000 1.3573 0.09016 0.08430 -0.0666 0.0877 0.5835
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