AH 93-W-174 (ah93w174-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: AH 93-W-174 (ah93w174-il) Reynolds number: 1,000,000 Max Cl/Cd: 138.44 at α=7.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-ah93w174-il-1000000-n5.txt Download as CSV file: xf-ah93w174-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: AH 93-W-174
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
------ -------- --------- --------- -------- -------- --------
-18.500 -0.9325 0.09413 0.09120 -0.0518 1.0000 0.0158
-18.250 -0.9842 0.08222 0.07910 -0.0588 1.0000 0.0158
-18.000 -1.0316 0.07122 0.06791 -0.0655 1.0000 0.0157
-17.750 -1.0673 0.06220 0.05872 -0.0710 1.0000 0.0157
-17.500 -1.0940 0.05474 0.05110 -0.0758 1.0000 0.0158
-17.250 -1.1114 0.04889 0.04512 -0.0795 1.0000 0.0158
-17.000 -1.1219 0.04429 0.04040 -0.0822 1.0000 0.0159
-16.750 -1.1180 0.04021 0.03622 -0.0865 0.9983 0.0162
-16.500 -1.0327 0.03566 0.03139 -0.1062 0.9063 0.0169
-16.250 -0.9979 0.03321 0.02842 -0.1137 0.8011 0.0172
-16.000 -0.9953 0.03128 0.02629 -0.1139 0.7673 0.0174
-15.750 -0.9913 0.02956 0.02441 -0.1139 0.7433 0.0176
-15.500 -0.9868 0.02801 0.02272 -0.1136 0.7225 0.0180
-15.250 -0.9832 0.02646 0.02105 -0.1130 0.7062 0.0182
-15.000 -0.9777 0.02514 0.01962 -0.1122 0.6925 0.0184
-14.750 -0.9705 0.02401 0.01841 -0.1113 0.6803 0.0189
-14.500 -0.9621 0.02300 0.01731 -0.1102 0.6704 0.0192
-14.250 -0.9532 0.02209 0.01632 -0.1090 0.6619 0.0195
-14.000 -0.9432 0.02128 0.01543 -0.1077 0.6536 0.0199
-13.750 -0.9329 0.02055 0.01463 -0.1062 0.6463 0.0202
-13.500 -0.9222 0.01988 0.01389 -0.1045 0.6396 0.0206
-13.250 -0.9120 0.01929 0.01321 -0.1026 0.6325 0.0209
-13.000 -0.9025 0.01877 0.01262 -0.1003 0.6269 0.0212
-12.750 -0.8919 0.01826 0.01206 -0.0980 0.6211 0.0217
-12.500 -0.8757 0.01778 0.01152 -0.0967 0.6158 0.0222
-12.250 -0.8578 0.01733 0.01103 -0.0955 0.6114 0.0229
-12.000 -0.8384 0.01691 0.01057 -0.0945 0.6074 0.0234
-11.750 -0.8179 0.01653 0.01013 -0.0936 0.6030 0.0240
-11.500 -0.7967 0.01618 0.00971 -0.0928 0.5987 0.0245
-11.250 -0.7747 0.01585 0.00932 -0.0921 0.5946 0.0250
-11.000 -0.7531 0.01543 0.00887 -0.0914 0.5912 0.0258
-10.750 -0.7304 0.01506 0.00848 -0.0908 0.5872 0.0267
-10.500 -0.7071 0.01474 0.00812 -0.0902 0.5835 0.0276
-10.250 -0.6833 0.01445 0.00778 -0.0897 0.5800 0.0284
-10.000 -0.6588 0.01418 0.00746 -0.0893 0.5771 0.0292
-9.750 -0.6344 0.01386 0.00711 -0.0889 0.5745 0.0302
-9.500 -0.6097 0.01355 0.00679 -0.0885 0.5716 0.0313
-9.250 -0.5845 0.01329 0.00649 -0.0882 0.5684 0.0326
-9.000 -0.5589 0.01306 0.00622 -0.0879 0.5651 0.0338
-8.750 -0.5334 0.01281 0.00593 -0.0876 0.5618 0.0350
-8.500 -0.5076 0.01255 0.00566 -0.0874 0.5595 0.0366
-8.250 -0.4812 0.01232 0.00542 -0.0873 0.5572 0.0381
-8.000 -0.4546 0.01212 0.00519 -0.0871 0.5547 0.0396
-7.750 -0.4282 0.01188 0.00494 -0.0869 0.5522 0.0418
-7.500 -0.4015 0.01168 0.00472 -0.0868 0.5497 0.0441
-7.250 -0.3746 0.01151 0.00452 -0.0867 0.5471 0.0459
-6.750 -0.3205 0.01112 0.00413 -0.0866 0.5423 0.0514
-6.500 -0.2929 0.01096 0.00395 -0.0865 0.5400 0.0540
-6.250 -0.2655 0.01077 0.00377 -0.0865 0.5378 0.0575
-6.000 -0.2378 0.01062 0.00361 -0.0865 0.5356 0.0605
-5.750 -0.2102 0.01046 0.00345 -0.0865 0.5333 0.0645
-5.500 -0.1825 0.01032 0.00330 -0.0865 0.5310 0.0687
-5.250 -0.1548 0.01020 0.00316 -0.0865 0.5286 0.0729
-5.000 -0.1268 0.01005 0.00303 -0.0866 0.5266 0.0782
-4.750 -0.0986 0.00991 0.00291 -0.0867 0.5246 0.0836
-4.500 -0.0704 0.00978 0.00279 -0.0868 0.5226 0.0897
-4.250 -0.0422 0.00965 0.00268 -0.0869 0.5206 0.0966
-4.000 -0.0139 0.00953 0.00258 -0.0870 0.5185 0.1043
-3.750 0.0143 0.00941 0.00248 -0.0871 0.5164 0.1136
-3.500 0.0425 0.00930 0.00239 -0.0872 0.5142 0.1232
-3.250 0.0707 0.00921 0.00231 -0.0873 0.5118 0.1338
-3.000 0.0992 0.00909 0.00224 -0.0874 0.5100 0.1466
-2.750 0.1278 0.00897 0.00217 -0.0876 0.5082 0.1602
-2.500 0.1564 0.00886 0.00211 -0.0878 0.5064 0.1747
-2.250 0.1850 0.00876 0.00205 -0.0880 0.5045 0.1904
-2.000 0.2136 0.00866 0.00200 -0.0882 0.5025 0.2092
-1.750 0.2421 0.00856 0.00195 -0.0883 0.5003 0.2289
-1.500 0.2705 0.00846 0.00191 -0.0885 0.4980 0.2514
-1.250 0.2988 0.00836 0.00188 -0.0887 0.4957 0.2780
-1.000 0.3274 0.00824 0.00185 -0.0889 0.4940 0.3089
-0.750 0.3561 0.00810 0.00183 -0.0892 0.4925 0.3446
-0.500 0.3847 0.00797 0.00181 -0.0894 0.4908 0.3825
-0.250 0.4134 0.00784 0.00181 -0.0897 0.4887 0.4230
0.000 0.4420 0.00773 0.00181 -0.0899 0.4866 0.4633
0.250 0.4705 0.00764 0.00182 -0.0901 0.4843 0.5003
0.500 0.4991 0.00760 0.00184 -0.0903 0.4822 0.5292
0.750 0.5276 0.00757 0.00187 -0.0904 0.4801 0.5557
1.000 0.5564 0.00756 0.00191 -0.0906 0.4783 0.5800
1.250 0.5853 0.00753 0.00196 -0.0909 0.4766 0.6021
1.500 0.6142 0.00752 0.00200 -0.0911 0.4746 0.6215
1.750 0.6430 0.00753 0.00205 -0.0913 0.4724 0.6396
2.000 0.6718 0.00754 0.00211 -0.0915 0.4704 0.6560
2.250 0.7004 0.00758 0.00217 -0.0916 0.4683 0.6708
2.500 0.7288 0.00761 0.00224 -0.0917 0.4660 0.6856
2.750 0.7569 0.00767 0.00232 -0.0918 0.4636 0.7006
3.000 0.7855 0.00770 0.00240 -0.0920 0.4618 0.7135
3.250 0.8143 0.00774 0.00247 -0.0922 0.4600 0.7241
3.500 0.8428 0.00778 0.00255 -0.0923 0.4578 0.7336
3.750 0.8713 0.00784 0.00263 -0.0925 0.4554 0.7416
4.000 0.8994 0.00790 0.00271 -0.0926 0.4530 0.7492
4.250 0.9275 0.00798 0.00280 -0.0927 0.4506 0.7570
4.500 0.9551 0.00806 0.00290 -0.0927 0.4480 0.7643
4.750 0.9833 0.00813 0.00300 -0.0928 0.4460 0.7715
5.000 1.0117 0.00819 0.00310 -0.0929 0.4438 0.7778
5.250 1.0396 0.00825 0.00321 -0.0930 0.4412 0.7843
5.500 1.0674 0.00834 0.00331 -0.0931 0.4383 0.7910
5.750 1.0948 0.00843 0.00343 -0.0931 0.4354 0.7969
6.000 1.1214 0.00855 0.00356 -0.0930 0.4317 0.8035
6.250 1.1493 0.00862 0.00367 -0.0931 0.4279 0.8099
6.500 1.1763 0.00871 0.00380 -0.0930 0.4229 0.8159
6.750 1.2023 0.00885 0.00394 -0.0928 0.4175 0.8224
7.000 1.2293 0.00896 0.00408 -0.0927 0.4123 0.8287
7.250 1.2553 0.00908 0.00424 -0.0925 0.4062 0.8348
7.500 1.2805 0.00925 0.00441 -0.0922 0.3994 0.8416
7.750 1.3055 0.00943 0.00459 -0.0918 0.3897 0.8479
8.000 1.3293 0.00964 0.00480 -0.0912 0.3788 0.8550
8.250 1.3515 0.00994 0.00506 -0.0904 0.3638 0.8624
8.500 1.3718 0.01028 0.00536 -0.0893 0.3473 0.8702
8.750 1.3914 0.01066 0.00571 -0.0881 0.3311 0.8789
9.000 1.4058 0.01120 0.00617 -0.0859 0.3086 0.8891
9.250 1.4121 0.01201 0.00683 -0.0825 0.2751 0.9024
9.500 1.4086 0.01286 0.00756 -0.0773 0.2430 0.9249
10.000 1.4047 0.01475 0.00928 -0.0684 0.1941 1.0000
10.250 1.4015 0.01588 0.01034 -0.0644 0.1769 1.0000
10.750 1.3877 0.01919 0.01354 -0.0574 0.1444 1.0000
11.000 1.3843 0.02111 0.01543 -0.0552 0.1326 1.0000
11.500 1.3770 0.02553 0.01981 -0.0516 0.1100 1.0000
11.750 1.3732 0.02792 0.02219 -0.0501 0.0999 1.0000
12.000 1.3699 0.03035 0.02461 -0.0488 0.0914 1.0000
12.250 1.3664 0.03283 0.02709 -0.0476 0.0839 1.0000
12.500 1.3654 0.03517 0.02944 -0.0465 0.0771 1.0000
12.750 1.3629 0.03765 0.03192 -0.0456 0.0709 1.0000
13.000 1.3589 0.04033 0.03459 -0.0446 0.0636 1.0000
13.250 1.3604 0.04263 0.03691 -0.0440 0.0593 1.0000
13.500 1.3589 0.04527 0.03955 -0.0434 0.0539 1.0000
13.750 1.3593 0.04780 0.04208 -0.0430 0.0482 1.0000
14.000 1.3606 0.05032 0.04462 -0.0427 0.0446 1.0000
14.250 1.3626 0.05279 0.04710 -0.0424 0.0408 1.0000
14.500 1.3646 0.05535 0.04968 -0.0422 0.0374 1.0000
15.000 1.3701 0.06042 0.05478 -0.0421 0.0316 1.0000
15.500 1.3764 0.06556 0.05997 -0.0423 0.0268 1.0000
15.750 1.3798 0.06817 0.06260 -0.0424 0.0248 1.0000
16.000 1.3835 0.07077 0.06523 -0.0427 0.0229 1.0000
16.250 1.3861 0.07355 0.06804 -0.0430 0.0210 1.0000
16.500 1.3903 0.07616 0.07068 -0.0433 0.0195 1.0000
16.750 1.3929 0.07904 0.07359 -0.0437 0.0181 1.0000
17.000 1.3967 0.08178 0.07637 -0.0442 0.0170 1.0000
17.250 1.4001 0.08460 0.07923 -0.0447 0.0160 1.0000
17.500 1.4032 0.08749 0.08216 -0.0453 0.0152 1.0000
17.750 1.4064 0.09040 0.08510 -0.0460 0.0142 1.0000
18.000 1.4095 0.09338 0.08814 -0.0467 0.0138 1.0000
18.250 1.4135 0.09625 0.09105 -0.0474 0.0131 1.0000
18.500 1.4162 0.09931 0.09416 -0.0483 0.0126 1.0000
18.750 1.4180 0.10253 0.09742 -0.0492 0.0120 1.0000
19.000 1.4210 0.10558 0.10052 -0.0501 0.0116 1.0000
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