AH 82-150 F (ah82150f-il) Xfoil prediction polar at RE=100,000 Ncrit=5
| Details | Polar file |
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Airfoil: AH 82-150 F (ah82150f-il) Reynolds number: 100,000 Max Cl/Cd: 33.49 at α=9° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-ah82150f-il-100000-n5.txt Download as CSV file: xf-ah82150f-il-100000-n5.csv |
XFOIL Version 6.96
Calculated polar for: AH 82-150 F
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.100 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-13.000 -0.1648 0.12174 0.11620 -0.1109 0.9071 0.0313
-12.750 -0.1569 0.11833 0.11277 -0.1119 0.9055 0.0301
-12.500 -0.1521 0.11460 0.10904 -0.1134 0.9040 0.0291
-12.250 -0.1485 0.11079 0.10523 -0.1152 0.9025 0.0284
-12.000 -0.1462 0.10691 0.10135 -0.1172 0.9011 0.0289
-11.750 -0.1454 0.10316 0.09762 -0.1189 0.8994 0.0290
-11.500 -0.1465 0.09921 0.09371 -0.1208 0.8975 0.0299
-11.250 -0.1454 0.09551 0.09003 -0.1225 0.8957 0.0295
-11.000 -0.1473 0.09125 0.08580 -0.1247 0.8939 0.0297
-10.750 -0.1495 0.08697 0.08155 -0.1268 0.8919 0.0296
-10.500 -0.1526 0.08253 0.07713 -0.1292 0.8899 0.0292
-10.250 -0.1595 0.07727 0.07190 -0.1323 0.8880 0.0289
-10.000 -0.1707 0.07163 0.06629 -0.1363 0.8856 0.0284
-9.750 -0.1898 0.06654 0.06119 -0.1388 0.8827 0.0279
-9.500 -0.2107 0.06273 0.05731 -0.1388 0.8798 0.0276
-9.250 -0.2325 0.05964 0.05412 -0.1370 0.8769 0.0274
-9.000 -0.2532 0.05719 0.05154 -0.1336 0.8742 0.0271
-8.750 -0.2745 0.05550 0.04973 -0.1288 0.8706 0.0271
-8.500 -0.2933 0.05381 0.04789 -0.1239 0.8673 0.0269
-8.250 -0.3083 0.05186 0.04574 -0.1192 0.8645 0.0269
-8.000 -0.3179 0.04950 0.04311 -0.1150 0.8620 0.0269
-7.750 -0.3210 0.04698 0.04025 -0.1115 0.8599 0.0271
-7.500 -0.3381 0.04619 0.03929 -0.1048 0.8561 0.0273
-7.250 -0.3500 0.04503 0.03791 -0.0988 0.8525 0.0275
-7.000 -0.3501 0.04310 0.03563 -0.0948 0.8497 0.0280
-6.750 -0.3437 0.04102 0.03314 -0.0917 0.8479 0.0287
-6.500 -0.3313 0.03906 0.03072 -0.0894 0.8465 0.0302
-6.250 -0.3370 0.03853 0.02988 -0.0837 0.8427 0.0316
-6.000 -0.3431 0.03804 0.02915 -0.0779 0.8388 0.0326
-5.750 -0.3302 0.03665 0.02763 -0.0760 0.8366 0.0346
-5.500 -0.3095 0.03548 0.02625 -0.0751 0.8349 0.0367
-5.250 -0.2854 0.03433 0.02485 -0.0746 0.8336 0.0395
-5.000 -0.2592 0.03360 0.02379 -0.0743 0.8325 0.0437
-4.750 -0.2547 0.03293 0.02313 -0.0706 0.8290 0.0463
-4.500 -0.2484 0.03256 0.02273 -0.0671 0.8253 0.0485
-4.250 -0.2293 0.03204 0.02210 -0.0658 0.8229 0.0533
-4.000 -0.2065 0.03143 0.02137 -0.0652 0.8210 0.0589
-3.750 -0.1822 0.03082 0.02074 -0.0648 0.8194 0.0641
-3.500 -0.1556 0.03033 0.02015 -0.0649 0.8181 0.0721
-3.250 -0.1587 0.03045 0.02028 -0.0599 0.8126 0.0763
-3.000 -0.1411 0.03022 0.01998 -0.0583 0.8094 0.0853
-2.500 -0.0925 0.02933 0.01927 -0.0577 0.8054 0.1382
-2.250 -0.0699 0.02825 0.01911 -0.0573 0.8041 0.3285
-2.000 -0.0783 0.02793 0.01943 -0.0515 0.7973 0.4698
-1.750 -0.0721 0.02831 0.02111 -0.0439 0.7943 0.8011
-1.500 -0.0588 0.02862 0.02123 -0.0405 0.7916 0.8546
-1.250 -0.0411 0.02920 0.02166 -0.0372 0.7891 0.8910
-1.000 0.1129 0.03125 0.02337 -0.0597 0.7927 0.9520
-0.750 0.1804 0.03148 0.02337 -0.0680 0.7922 0.9629
-0.500 0.2276 0.03155 0.02329 -0.0722 0.7911 0.9707
-0.250 0.2551 0.03182 0.02345 -0.0735 0.7863 0.9754
0.000 0.2792 0.03201 0.02356 -0.0737 0.7815 0.9801
0.250 0.3100 0.03203 0.02350 -0.0749 0.7789 0.9832
0.500 0.3480 0.03194 0.02332 -0.0773 0.7771 0.9847
1.000 0.3885 0.03233 0.02364 -0.0764 0.7659 0.9909
1.250 0.4220 0.03222 0.02348 -0.0778 0.7636 0.9923
1.750 0.4591 0.03259 0.02381 -0.0760 0.7518 0.9969
2.000 0.4923 0.03240 0.02361 -0.0772 0.7495 0.9978
2.500 0.5215 0.03265 0.02387 -0.0736 0.7368 1.0000
2.750 0.5515 0.03237 0.02359 -0.0741 0.7345 1.0000
3.000 0.5419 0.03277 0.02401 -0.0681 0.7236 1.0000
3.250 0.5699 0.03248 0.02373 -0.0681 0.7210 1.0000
3.500 0.5634 0.03282 0.02410 -0.0627 0.7102 1.0000
4.000 0.5857 0.03279 0.02414 -0.0574 0.6964 1.0000
4.500 0.6093 0.03266 0.02408 -0.0523 0.6825 1.0000
4.750 0.6087 0.03291 0.02437 -0.0480 0.6719 1.0000
5.000 0.6339 0.03245 0.02399 -0.0473 0.6685 1.0000
5.250 0.6341 0.03268 0.02426 -0.0431 0.6576 1.0000
5.500 0.6528 0.03236 0.02401 -0.0415 0.6524 1.0000
5.750 0.6611 0.03234 0.02405 -0.0384 0.6434 1.0000
6.250 0.6905 0.03193 0.02381 -0.0341 0.6293 1.0000
6.500 0.7020 0.03196 0.02391 -0.0317 0.6204 1.0000
6.750 0.7259 0.03150 0.02355 -0.0309 0.6151 1.0000
7.000 0.7416 0.03156 0.02371 -0.0292 0.6059 1.0000
7.250 0.7696 0.03101 0.02328 -0.0290 0.6007 1.0000
7.750 0.8201 0.03040 0.02297 -0.0280 0.5858 1.0000
8.000 0.8396 0.03052 0.02324 -0.0271 0.5750 1.0000
8.250 0.8679 0.03014 0.02302 -0.0270 0.5667 1.0000
8.500 0.8948 0.02947 0.02246 -0.0263 0.5482 1.0000
8.750 0.9241 0.02800 0.02083 -0.0248 0.4974 1.0000
9.000 0.9390 0.02804 0.02058 -0.0225 0.4387 1.0000
9.250 0.9428 0.02899 0.02112 -0.0195 0.3706 1.0000
9.500 0.9353 0.03087 0.02242 -0.0157 0.2812 1.0000
9.750 0.9193 0.03367 0.02435 -0.0117 0.1614 1.0000
10.000 0.9034 0.03692 0.02665 -0.0082 0.0506 1.0000
10.250 0.9060 0.03889 0.02849 -0.0063 0.0339 1.0000
10.500 0.9124 0.04059 0.03025 -0.0048 0.0289 1.0000
10.750 0.9184 0.04236 0.03214 -0.0034 0.0259 1.0000
11.000 0.9252 0.04410 0.03406 -0.0021 0.0245 1.0000
11.250 0.9303 0.04604 0.03620 -0.0009 0.0231 1.0000
11.500 0.9344 0.04809 0.03841 0.0003 0.0221 1.0000
11.750 0.9381 0.05022 0.04068 0.0015 0.0214 1.0000
12.000 0.9409 0.05250 0.04307 0.0026 0.0206 1.0000
12.250 0.9426 0.05492 0.04558 0.0038 0.0195 1.0000
12.500 0.9505 0.05685 0.04758 0.0048 0.0187 1.0000
12.750 0.9621 0.05848 0.04935 0.0054 0.0175 1.0000
13.000 0.9754 0.06004 0.05103 0.0061 0.0167 1.0000
13.250 0.9926 0.06148 0.05259 0.0068 0.0161 1.0000
13.500 1.0119 0.06297 0.05421 0.0075 0.0157 1.0000
13.750 1.0303 0.06470 0.05616 0.0080 0.0153 1.0000
14.000 1.0473 0.06683 0.05849 0.0085 0.0150 1.0000
14.250 1.0597 0.06934 0.06124 0.0089 0.0148 1.0000
14.500 1.0672 0.07225 0.06440 0.0094 0.0147 1.0000
14.750 1.0699 0.07557 0.06799 0.0099 0.0146 1.0000
15.000 1.0682 0.07924 0.07194 0.0102 0.0145 1.0000
15.250 1.0634 0.08310 0.07606 0.0103 0.0144 1.0000
15.500 1.0559 0.08730 0.08052 0.0101 0.0143 1.0000
15.750 1.0471 0.09167 0.08510 0.0095 0.0141 1.0000
16.000 1.0363 0.09643 0.09010 0.0085 0.0140 1.0000
16.250 1.0238 0.10160 0.09551 0.0070 0.0140 1.0000
16.500 1.0110 0.10695 0.10105 0.0051 0.0138 1.0000
16.750 0.9906 0.11406 0.10848 0.0022 0.0142 1.0000
17.000 0.9744 0.12073 0.11536 -0.0012 0.0141 1.0000
17.250 0.9492 0.12987 0.12477 -0.0062 0.0146 1.0000
17.500 0.9247 0.13981 0.13493 -0.0122 0.0150 1.0000
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