AH 93-W-174 (ah93w174-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: AH 93-W-174 (ah93w174-il) Reynolds number: 500,000 Max Cl/Cd: 112.46 at α=8.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-ah93w174-il-500000-n5.txt Download as CSV file: xf-ah93w174-il-500000-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 = 0.500 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-18.250 -0.7394 0.12216 0.11909 -0.0370 1.0000 0.0202
-18.000 -0.7692 0.11250 0.10930 -0.0424 1.0000 0.0204
-17.750 -0.7944 0.10403 0.10071 -0.0471 1.0000 0.0206
-17.500 -0.8196 0.09576 0.09232 -0.0518 1.0000 0.0207
-17.250 -0.8430 0.08810 0.08453 -0.0563 1.0000 0.0208
-17.000 -0.8656 0.08070 0.07700 -0.0606 1.0000 0.0209
-16.750 -0.8870 0.07365 0.06983 -0.0648 1.0000 0.0210
-16.500 -0.9063 0.06701 0.06306 -0.0689 1.0000 0.0211
-16.250 -0.9235 0.06087 0.05679 -0.0726 1.0000 0.0212
-16.000 -0.9391 0.05512 0.05093 -0.0762 1.0000 0.0213
-15.750 -0.9518 0.04995 0.04565 -0.0795 1.0000 0.0215
-15.500 -0.9605 0.04557 0.04117 -0.0821 1.0000 0.0217
-15.250 -0.9484 0.04124 0.03672 -0.0880 0.9348 0.0220
-14.750 -0.8512 0.03426 0.02890 -0.1114 0.7894 0.0236
-14.500 -0.8476 0.03250 0.02693 -0.1114 0.7621 0.0240
-14.250 -0.8447 0.03077 0.02503 -0.1112 0.7411 0.0243
-14.000 -0.8399 0.02927 0.02336 -0.1107 0.7232 0.0247
-13.750 -0.8339 0.02794 0.02187 -0.1100 0.7084 0.0250
-13.500 -0.8311 0.02647 0.02030 -0.1091 0.6971 0.0255
-13.250 -0.8252 0.02528 0.01902 -0.1080 0.6866 0.0259
-13.000 -0.8177 0.02425 0.01789 -0.1067 0.6778 0.0264
-12.750 -0.8083 0.02338 0.01694 -0.1054 0.6692 0.0269
-12.500 -0.7992 0.02257 0.01603 -0.1038 0.6619 0.0273
-12.250 -0.7900 0.02182 0.01518 -0.1020 0.6544 0.0279
-11.750 -0.7689 0.02073 0.01389 -0.0980 0.6417 0.0292
-11.500 -0.7555 0.02011 0.01320 -0.0964 0.6357 0.0298
-11.000 -0.7212 0.01907 0.01205 -0.0940 0.6261 0.0314
-10.750 -0.7017 0.01861 0.01151 -0.0931 0.6215 0.0323
-10.500 -0.6813 0.01819 0.01100 -0.0923 0.6169 0.0333
-10.000 -0.6392 0.01732 0.01002 -0.0907 0.6089 0.0354
-9.750 -0.6170 0.01691 0.00957 -0.0901 0.6046 0.0366
-9.500 -0.5942 0.01656 0.00915 -0.0895 0.6006 0.0379
-9.250 -0.5707 0.01624 0.00875 -0.0890 0.5970 0.0392
-9.000 -0.5473 0.01587 0.00834 -0.0885 0.5940 0.0406
-8.750 -0.5232 0.01551 0.00796 -0.0881 0.5909 0.0424
-8.500 -0.4985 0.01521 0.00762 -0.0877 0.5877 0.0442
-8.250 -0.4734 0.01495 0.00729 -0.0874 0.5844 0.0459
-8.000 -0.4489 0.01462 0.00694 -0.0870 0.5812 0.0480
-7.500 -0.3975 0.01412 0.00636 -0.0865 0.5753 0.0528
-7.250 -0.3718 0.01383 0.00606 -0.0863 0.5726 0.0556
-7.000 -0.3456 0.01359 0.00580 -0.0862 0.5699 0.0587
-6.750 -0.3190 0.01340 0.00556 -0.0860 0.5672 0.0614
-6.500 -0.2929 0.01315 0.00531 -0.0858 0.5646 0.0654
-6.250 -0.2663 0.01297 0.00508 -0.0857 0.5621 0.0694
-6.000 -0.2395 0.01276 0.00486 -0.0856 0.5598 0.0734
-5.750 -0.2124 0.01255 0.00467 -0.0856 0.5572 0.0783
-5.500 -0.1852 0.01237 0.00447 -0.0855 0.5545 0.0835
-5.250 -0.1580 0.01218 0.00429 -0.0855 0.5521 0.0895
-5.000 -0.1306 0.01202 0.00412 -0.0855 0.5497 0.0958
-4.750 -0.1033 0.01186 0.00396 -0.0854 0.5475 0.1033
-4.500 -0.0760 0.01171 0.00381 -0.0854 0.5454 0.1117
-4.250 -0.0483 0.01157 0.00367 -0.0855 0.5433 0.1210
-4.000 -0.0204 0.01140 0.00355 -0.0855 0.5410 0.1320
-3.750 0.0074 0.01124 0.00343 -0.0856 0.5385 0.1440
-3.500 0.0353 0.01110 0.00332 -0.0857 0.5362 0.1571
-3.250 0.0632 0.01096 0.00321 -0.0858 0.5340 0.1718
-3.000 0.0911 0.01083 0.00312 -0.0859 0.5320 0.1881
-2.750 0.1189 0.01071 0.00303 -0.0859 0.5300 0.2073
-2.500 0.1468 0.01060 0.00295 -0.0860 0.5279 0.2280
-2.250 0.1749 0.01045 0.00289 -0.0862 0.5259 0.2522
-2.000 0.2031 0.01029 0.00283 -0.0864 0.5237 0.2798
-1.750 0.2312 0.01012 0.00277 -0.0865 0.5215 0.3132
-1.500 0.2593 0.00996 0.00273 -0.0867 0.5194 0.3509
-1.250 0.2873 0.00979 0.00269 -0.0869 0.5174 0.3930
-1.000 0.3152 0.00965 0.00266 -0.0870 0.5153 0.4369
-0.750 0.3432 0.00953 0.00266 -0.0871 0.5133 0.4800
-0.500 0.3712 0.00945 0.00267 -0.0872 0.5111 0.5190
-0.250 0.3996 0.00938 0.00271 -0.0874 0.5092 0.5528
0.000 0.4282 0.00934 0.00275 -0.0875 0.5073 0.5804
0.250 0.4567 0.00931 0.00280 -0.0876 0.5053 0.6042
0.500 0.4851 0.00931 0.00285 -0.0877 0.5032 0.6257
0.750 0.5134 0.00932 0.00290 -0.0878 0.5010 0.6454
1.000 0.5417 0.00935 0.00295 -0.0879 0.4988 0.6627
1.250 0.5699 0.00939 0.00301 -0.0879 0.4967 0.6787
1.500 0.5980 0.00946 0.00308 -0.0879 0.4948 0.6934
1.750 0.6265 0.00950 0.00317 -0.0881 0.4931 0.7071
2.000 0.6548 0.00954 0.00326 -0.0881 0.4910 0.7213
2.250 0.6829 0.00958 0.00336 -0.0881 0.4887 0.7344
2.500 0.7110 0.00964 0.00344 -0.0882 0.4864 0.7455
2.750 0.7390 0.00970 0.00352 -0.0882 0.4842 0.7556
3.000 0.7669 0.00978 0.00361 -0.0882 0.4823 0.7638
3.250 0.7947 0.00987 0.00370 -0.0882 0.4803 0.7720
3.500 0.8225 0.00996 0.00380 -0.0883 0.4782 0.7795
3.750 0.8503 0.01002 0.00393 -0.0883 0.4760 0.7872
4.000 0.8784 0.01010 0.00404 -0.0884 0.4738 0.7947
4.250 0.9058 0.01017 0.00416 -0.0883 0.4714 0.8013
4.500 0.9334 0.01025 0.00427 -0.0883 0.4690 0.8084
4.750 0.9606 0.01034 0.00438 -0.0882 0.4666 0.8149
5.000 0.9875 0.01045 0.00451 -0.0881 0.4645 0.8217
5.250 1.0148 0.01057 0.00464 -0.0881 0.4623 0.8287
5.500 1.0416 0.01064 0.00480 -0.0880 0.4598 0.8350
5.750 1.0685 0.01074 0.00496 -0.0879 0.4572 0.8421
6.000 1.0951 0.01084 0.00510 -0.0877 0.4545 0.8487
6.250 1.1210 0.01094 0.00525 -0.0874 0.4517 0.8557
6.750 1.1724 0.01118 0.00556 -0.0868 0.4461 0.8699
7.000 1.1982 0.01127 0.00573 -0.0865 0.4419 0.8778
7.250 1.2225 0.01136 0.00588 -0.0860 0.4372 0.8855
7.500 1.2464 0.01149 0.00602 -0.0853 0.4328 0.8944
7.750 1.2700 0.01159 0.00621 -0.0846 0.4279 0.9037
8.000 1.2929 0.01170 0.00638 -0.0838 0.4222 0.9144
8.250 1.3137 0.01184 0.00654 -0.0826 0.4166 0.9281
8.500 1.3365 0.01193 0.00673 -0.0818 0.4089 0.9474
8.750 1.3641 0.01213 0.00693 -0.0822 0.3991 1.0000
9.000 1.3857 0.01241 0.00721 -0.0814 0.3874 1.0000
9.250 1.4061 0.01273 0.00752 -0.0804 0.3748 1.0000
9.500 1.4248 0.01309 0.00786 -0.0792 0.3628 1.0000
9.750 1.4389 0.01356 0.00829 -0.0772 0.3476 1.0000
10.000 1.4447 0.01419 0.00885 -0.0738 0.3283 1.0000
10.250 1.4443 0.01509 0.00964 -0.0697 0.3056 1.0000
10.500 1.4382 0.01630 0.01074 -0.0652 0.2816 1.0000
10.750 1.4298 0.01781 0.01217 -0.0610 0.2610 1.0000
11.000 1.4169 0.01991 0.01419 -0.0573 0.2393 1.0000
11.250 1.4058 0.02232 0.01655 -0.0545 0.2216 1.0000
11.500 1.3953 0.02499 0.01918 -0.0523 0.2055 1.0000
11.750 1.3845 0.02787 0.02202 -0.0504 0.1903 1.0000
12.000 1.3730 0.03095 0.02506 -0.0488 0.1750 1.0000
12.250 1.3632 0.03397 0.02806 -0.0473 0.1614 1.0000
12.500 1.3548 0.03695 0.03102 -0.0461 0.1488 1.0000
12.750 1.3463 0.04001 0.03405 -0.0450 0.1363 1.0000
13.000 1.3403 0.04293 0.03695 -0.0442 0.1256 1.0000
13.250 1.3345 0.04597 0.03997 -0.0435 0.1148 1.0000
13.500 1.3285 0.04914 0.04310 -0.0430 0.1032 1.0000
13.750 1.3257 0.05208 0.04602 -0.0426 0.0945 1.0000
14.000 1.3228 0.05512 0.04904 -0.0424 0.0848 1.0000
14.250 1.3229 0.05791 0.05183 -0.0422 0.0774 1.0000
14.500 1.3222 0.06084 0.05476 -0.0422 0.0708 1.0000
14.750 1.3224 0.06372 0.05763 -0.0422 0.0640 1.0000
15.000 1.3238 0.06656 0.06049 -0.0424 0.0585 1.0000
15.250 1.3249 0.06945 0.06338 -0.0425 0.0534 1.0000
15.500 1.3261 0.07239 0.06633 -0.0428 0.0486 1.0000
15.750 1.3282 0.07524 0.06921 -0.0431 0.0445 1.0000
16.000 1.3299 0.07823 0.07223 -0.0435 0.0410 1.0000
16.250 1.3326 0.08112 0.07514 -0.0440 0.0378 1.0000
16.500 1.3338 0.08422 0.07825 -0.0445 0.0345 1.0000
16.750 1.3365 0.08718 0.08126 -0.0451 0.0319 1.0000
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