AH 83-159 (ah83159-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: AH 83-159 (ah83159-il) Reynolds number: 1,000,000 Max Cl/Cd: 133.8 at α=5.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-ah83159-il-1000000-n5.txt Download as CSV file: xf-ah83159-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: AH 83-159
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
------ -------- --------- --------- -------- -------- --------
-12.250 -0.5292 0.03966 0.03640 -0.1163 0.7343 0.0044
-12.000 -0.5669 0.03461 0.03104 -0.1137 0.7311 0.0044
-11.750 -0.5806 0.03192 0.02814 -0.1110 0.7281 0.0044
-11.500 -0.5840 0.03010 0.02616 -0.1086 0.7255 0.0045
-11.250 -0.5847 0.02852 0.02443 -0.1061 0.7227 0.0046
-11.000 -0.5937 0.02642 0.02210 -0.1022 0.7199 0.0047
-10.750 -0.5909 0.02537 0.02091 -0.0992 0.7172 0.0048
-10.500 -0.5856 0.02386 0.01919 -0.0967 0.7149 0.0048
-10.000 -0.5611 0.02146 0.01645 -0.0934 0.7107 0.0050
-9.750 -0.5456 0.02035 0.01518 -0.0921 0.7085 0.0051
-9.500 -0.5275 0.01949 0.01418 -0.0911 0.7062 0.0051
-9.250 -0.5088 0.01860 0.01315 -0.0901 0.7038 0.0052
-9.000 -0.4890 0.01779 0.01220 -0.0892 0.7015 0.0053
-8.750 -0.4683 0.01706 0.01135 -0.0885 0.6995 0.0053
-8.500 -0.4467 0.01640 0.01057 -0.0878 0.6976 0.0054
-8.250 -0.4239 0.01584 0.00993 -0.0874 0.6959 0.0054
-8.000 -0.4014 0.01520 0.00920 -0.0868 0.6940 0.0055
-7.750 -0.3777 0.01473 0.00866 -0.0865 0.6919 0.0055
-7.500 -0.3542 0.01422 0.00807 -0.0861 0.6898 0.0056
-7.250 -0.3322 0.01351 0.00726 -0.0854 0.6877 0.0057
-7.000 -0.3095 0.01293 0.00660 -0.0848 0.6857 0.0059
-6.500 -0.2600 0.01218 0.00577 -0.0843 0.6823 0.0064
-6.250 -0.2347 0.01184 0.00540 -0.0842 0.6806 0.0066
-6.000 -0.2092 0.01152 0.00504 -0.0841 0.6786 0.0068
-5.750 -0.1835 0.01121 0.00470 -0.0839 0.6766 0.0070
-5.500 -0.1576 0.01094 0.00439 -0.0839 0.6746 0.0074
-5.250 -0.1314 0.01069 0.00410 -0.0838 0.6727 0.0077
-5.000 -0.1050 0.01048 0.00383 -0.0838 0.6710 0.0080
-4.750 -0.0788 0.01024 0.00355 -0.0837 0.6692 0.0087
-4.500 -0.0519 0.01001 0.00334 -0.0838 0.6676 0.0097
-4.250 -0.0246 0.00983 0.00315 -0.0840 0.6657 0.0110
-4.000 0.0026 0.00964 0.00296 -0.0841 0.6638 0.0130
-3.750 0.0300 0.00949 0.00280 -0.0843 0.6620 0.0158
-3.500 0.0573 0.00933 0.00266 -0.0845 0.6601 0.0204
-3.250 0.0846 0.00917 0.00252 -0.0847 0.6581 0.0273
-3.000 0.1119 0.00903 0.00239 -0.0848 0.6563 0.0371
-2.750 0.1392 0.00885 0.00228 -0.0850 0.6546 0.0551
-2.500 0.1662 0.00858 0.00216 -0.0853 0.6529 0.0953
-2.250 0.1928 0.00824 0.00204 -0.0855 0.6510 0.1608
-2.000 0.2191 0.00787 0.00193 -0.0857 0.6490 0.2416
-1.750 0.2451 0.00742 0.00181 -0.0860 0.6470 0.3462
-1.500 0.2708 0.00689 0.00168 -0.0862 0.6450 0.4747
-1.250 0.2949 0.00613 0.00153 -0.0862 0.6431 0.6617
-1.000 0.3212 0.00602 0.00165 -0.0860 0.6412 0.7427
-0.750 0.3496 0.00610 0.00178 -0.0862 0.6394 0.7678
-0.500 0.3786 0.00618 0.00187 -0.0865 0.6375 0.7804
-0.250 0.4080 0.00625 0.00190 -0.0870 0.6354 0.7888
0.000 0.4367 0.00635 0.00200 -0.0873 0.6333 0.7936
0.250 0.4655 0.00645 0.00208 -0.0876 0.6311 0.7987
0.500 0.4945 0.00654 0.00212 -0.0881 0.6288 0.8034
0.750 0.5229 0.00662 0.00217 -0.0884 0.6267 0.8056
1.000 0.5519 0.00666 0.00223 -0.0888 0.6245 0.8071
1.250 0.5808 0.00670 0.00227 -0.0893 0.6219 0.8084
1.500 0.6095 0.00674 0.00231 -0.0897 0.6190 0.8098
1.750 0.6381 0.00679 0.00234 -0.0901 0.6158 0.8111
2.000 0.6664 0.00685 0.00237 -0.0904 0.6128 0.8124
2.250 0.6952 0.00688 0.00241 -0.0909 0.6094 0.8136
2.500 0.7238 0.00692 0.00245 -0.0914 0.6050 0.8148
2.750 0.7520 0.00698 0.00249 -0.0917 0.6004 0.8161
3.000 0.7803 0.00703 0.00253 -0.0921 0.5968 0.8172
3.250 0.8090 0.00707 0.00258 -0.0926 0.5930 0.8181
3.500 0.8371 0.00712 0.00264 -0.0930 0.5886 0.8189
3.750 0.8645 0.00719 0.00270 -0.0932 0.5843 0.8197
4.000 0.8925 0.00724 0.00278 -0.0935 0.5797 0.8205
4.250 0.9200 0.00731 0.00287 -0.0937 0.5742 0.8212
4.500 0.9469 0.00740 0.00296 -0.0939 0.5690 0.8220
4.750 0.9745 0.00747 0.00305 -0.0942 0.5628 0.8227
5.000 1.0006 0.00759 0.00316 -0.0942 0.5547 0.8235
5.250 1.0267 0.00770 0.00329 -0.0942 0.5445 0.8244
5.500 1.0517 0.00786 0.00343 -0.0940 0.5320 0.8254
5.750 1.0748 0.00809 0.00360 -0.0934 0.5148 0.8264
6.000 1.0961 0.00838 0.00383 -0.0926 0.4936 0.8273
6.250 1.1147 0.00877 0.00411 -0.0913 0.4682 0.8283
6.500 1.1306 0.00923 0.00445 -0.0895 0.4397 0.8294
6.750 1.1422 0.00980 0.00488 -0.0869 0.4065 0.8307
7.000 1.1469 0.01046 0.00537 -0.0831 0.3716 0.8320
7.250 1.1436 0.01116 0.00592 -0.0778 0.3401 0.8332
7.500 1.1377 0.01209 0.00672 -0.0724 0.3092 0.8345
7.750 1.1359 0.01307 0.00759 -0.0682 0.2819 0.8357
8.000 1.1384 0.01403 0.00846 -0.0649 0.2584 0.8370
8.250 1.1394 0.01513 0.00946 -0.0615 0.2330 0.8382
8.500 1.1419 0.01625 0.01048 -0.0585 0.2098 0.8393
8.750 1.1394 0.01769 0.01175 -0.0551 0.1776 0.8404
9.000 1.1380 0.01915 0.01306 -0.0519 0.1476 0.8414
9.250 1.1405 0.02047 0.01427 -0.0494 0.1249 0.8425
9.500 1.1411 0.02195 0.01562 -0.0468 0.0991 0.8436
9.750 1.1438 0.02338 0.01694 -0.0445 0.0775 0.8445
10.000 1.1466 0.02485 0.01829 -0.0424 0.0568 0.8452
10.250 1.1542 0.02607 0.01946 -0.0408 0.0450 0.8458
10.500 1.1628 0.02727 0.02062 -0.0395 0.0361 0.8463
10.750 1.1722 0.02846 0.02179 -0.0382 0.0287 0.8468
11.000 1.1821 0.02964 0.02296 -0.0371 0.0236 0.8474
11.250 1.1928 0.03078 0.02412 -0.0360 0.0197 0.8481
11.500 1.2035 0.03195 0.02531 -0.0351 0.0168 0.8489
11.750 1.2129 0.03325 0.02661 -0.0340 0.0130 0.8496
12.000 1.2234 0.03450 0.02789 -0.0332 0.0106 0.8501
12.250 1.2339 0.03579 0.02919 -0.0324 0.0089 0.8506
12.500 1.2425 0.03725 0.03067 -0.0315 0.0065 0.8512
12.750 1.2530 0.03860 0.03206 -0.0308 0.0055 0.8517
13.000 1.2621 0.04008 0.03357 -0.0300 0.0045 0.8522
13.250 1.2717 0.04156 0.03510 -0.0294 0.0040 0.8527
13.500 1.2818 0.04302 0.03661 -0.0288 0.0037 0.8532
13.750 1.2908 0.04462 0.03826 -0.0283 0.0034 0.8537
14.000 1.2984 0.04636 0.04005 -0.0277 0.0029 0.8542
14.250 1.3056 0.04819 0.04194 -0.0271 0.0027 0.8547
14.500 1.3147 0.04987 0.04367 -0.0268 0.0026 0.8552
14.750 1.3229 0.05167 0.04554 -0.0264 0.0026 0.8558
15.000 1.3309 0.05353 0.04746 -0.0261 0.0025 0.8565
15.250 1.3375 0.05556 0.04956 -0.0259 0.0024 0.8570
15.500 1.3451 0.05752 0.05158 -0.0257 0.0023 0.8575
15.750 1.3502 0.05980 0.05395 -0.0255 0.0023 0.8579
16.000 1.3566 0.06198 0.05620 -0.0255 0.0022 0.8583
16.250 1.3613 0.06439 0.05869 -0.0255 0.0021 0.8587
16.500 1.3663 0.06682 0.06119 -0.0256 0.0021 0.8590
16.750 1.3702 0.06943 0.06388 -0.0258 0.0020 0.8594
17.000 1.3738 0.07210 0.06662 -0.0260 0.0020 0.8597
17.250 1.3767 0.07494 0.06954 -0.0264 0.0020 0.8600
17.500 1.3785 0.07797 0.07266 -0.0268 0.0019 0.8603
17.750 1.3774 0.08148 0.07626 -0.0274 0.0018 0.8606
18.250 1.3777 0.08828 0.08324 -0.0289 0.0017 0.8612
18.500 1.3775 0.09182 0.08689 -0.0299 0.0017 0.8616
18.750 1.3748 0.09583 0.09100 -0.0310 0.0017 0.8619
19.000 1.3691 0.10037 0.09565 -0.0324 0.0017 0.8622
19.250 1.3656 0.10461 0.10000 -0.0339 0.0016 0.8626
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