AH 94-145 (ah94145-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: AH 94-145 (ah94145-il) Reynolds number: 1,000,000 Max Cl/Cd: 164.41 at α=5.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-ah94145-il-1000000-n5.txt Download as CSV file: xf-ah94145-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: AH 94-145
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
------ -------- --------- --------- -------- -------- --------
-13.500 -0.8065 0.03342 0.02963 -0.1088 0.6863 0.0093
-13.250 -0.7992 0.03060 0.02661 -0.1106 0.6841 0.0094
-13.000 -0.7859 0.02850 0.02433 -0.1117 0.6819 0.0095
-12.750 -0.7691 0.02679 0.02245 -0.1124 0.6797 0.0096
-12.250 -0.7295 0.02399 0.01935 -0.1135 0.6759 0.0098
-12.000 -0.7075 0.02281 0.01804 -0.1140 0.6740 0.0099
-11.750 -0.6845 0.02175 0.01685 -0.1144 0.6720 0.0101
-11.500 -0.6606 0.02079 0.01575 -0.1147 0.6700 0.0102
-11.250 -0.6361 0.01991 0.01475 -0.1151 0.6682 0.0103
-11.000 -0.6108 0.01912 0.01383 -0.1154 0.6664 0.0104
-10.750 -0.5850 0.01841 0.01300 -0.1158 0.6646 0.0105
-10.500 -0.5588 0.01776 0.01224 -0.1161 0.6628 0.0107
-10.250 -0.5325 0.01706 0.01142 -0.1165 0.6610 0.0108
-10.000 -0.5061 0.01629 0.01056 -0.1169 0.6598 0.0111
-9.750 -0.4789 0.01570 0.00991 -0.1173 0.6583 0.0113
-9.500 -0.4512 0.01521 0.00935 -0.1176 0.6566 0.0115
-9.250 -0.4233 0.01476 0.00884 -0.1180 0.6548 0.0117
-9.000 -0.3952 0.01434 0.00836 -0.1184 0.6531 0.0120
-8.750 -0.3670 0.01396 0.00792 -0.1188 0.6515 0.0123
-8.500 -0.3386 0.01360 0.00749 -0.1191 0.6500 0.0126
-8.250 -0.3100 0.01325 0.00708 -0.1195 0.6484 0.0129
-8.000 -0.2814 0.01292 0.00668 -0.1199 0.6468 0.0132
-7.750 -0.2527 0.01262 0.00630 -0.1203 0.6450 0.0134
-7.500 -0.2239 0.01218 0.00583 -0.1207 0.6437 0.0139
-7.250 -0.1948 0.01186 0.00548 -0.1212 0.6424 0.0143
-7.000 -0.1657 0.01158 0.00517 -0.1216 0.6410 0.0147
-6.750 -0.1364 0.01132 0.00488 -0.1221 0.6395 0.0152
-6.500 -0.1071 0.01108 0.00460 -0.1225 0.6379 0.0158
-6.250 -0.0777 0.01086 0.00434 -0.1229 0.6362 0.0162
-6.000 -0.0483 0.01061 0.00406 -0.1234 0.6345 0.0169
-5.750 -0.0189 0.01039 0.00382 -0.1238 0.6330 0.0178
-5.500 0.0106 0.01022 0.00362 -0.1243 0.6315 0.0188
-5.250 0.0401 0.01007 0.00343 -0.1247 0.6299 0.0197
-5.000 0.0698 0.00987 0.00322 -0.1252 0.6285 0.0211
-4.750 0.0996 0.00970 0.00306 -0.1257 0.6272 0.0226
-4.500 0.1294 0.00955 0.00289 -0.1262 0.6257 0.0241
-4.250 0.1593 0.00939 0.00274 -0.1268 0.6243 0.0264
-4.000 0.1891 0.00925 0.00261 -0.1273 0.6228 0.0289
-3.750 0.2190 0.00913 0.00249 -0.1278 0.6213 0.0325
-3.500 0.2489 0.00900 0.00238 -0.1283 0.6198 0.0369
-3.250 0.2787 0.00890 0.00228 -0.1288 0.6182 0.0416
-3.000 0.3085 0.00881 0.00219 -0.1293 0.6166 0.0468
-2.750 0.3383 0.00873 0.00212 -0.1298 0.6148 0.0528
-2.500 0.3682 0.00865 0.00206 -0.1304 0.6133 0.0588
-2.250 0.3982 0.00858 0.00201 -0.1309 0.6120 0.0642
-2.000 0.4282 0.00849 0.00196 -0.1314 0.6104 0.0710
-1.750 0.4582 0.00842 0.00191 -0.1320 0.6087 0.0781
-1.500 0.4882 0.00836 0.00187 -0.1325 0.6070 0.0865
-1.250 0.5181 0.00829 0.00183 -0.1331 0.6054 0.0978
-1.000 0.5481 0.00821 0.00180 -0.1337 0.6038 0.1144
-0.750 0.5781 0.00811 0.00178 -0.1343 0.6022 0.1450
-0.500 0.6083 0.00798 0.00177 -0.1350 0.6004 0.1919
-0.250 0.6385 0.00783 0.00177 -0.1358 0.5985 0.2558
0.000 0.6693 0.00762 0.00179 -0.1367 0.5971 0.3353
0.250 0.7002 0.00738 0.00182 -0.1377 0.5956 0.4322
0.500 0.7310 0.00720 0.00186 -0.1386 0.5939 0.5141
0.750 0.7618 0.00704 0.00191 -0.1395 0.5921 0.5975
1.000 0.7921 0.00696 0.00196 -0.1401 0.5901 0.6506
1.250 0.8223 0.00684 0.00204 -0.1408 0.5881 0.7234
1.500 0.8508 0.00673 0.00216 -0.1410 0.5861 0.8099
1.750 0.8784 0.00675 0.00226 -0.1410 0.5841 0.8542
2.000 0.9065 0.00678 0.00234 -0.1411 0.5822 0.8726
2.250 0.9350 0.00682 0.00241 -0.1412 0.5803 0.8855
2.500 0.9632 0.00685 0.00248 -0.1414 0.5781 0.8943
2.750 0.9920 0.00691 0.00254 -0.1417 0.5757 0.9020
3.000 1.0199 0.00696 0.00260 -0.1418 0.5733 0.9081
3.250 1.0481 0.00702 0.00267 -0.1420 0.5708 0.9145
3.500 1.0761 0.00710 0.00274 -0.1422 0.5680 0.9204
3.750 1.1039 0.00713 0.00281 -0.1423 0.5649 0.9259
4.000 1.1321 0.00719 0.00288 -0.1425 0.5602 0.9312
4.250 1.1589 0.00728 0.00295 -0.1424 0.5539 0.9362
4.500 1.1859 0.00733 0.00302 -0.1424 0.5465 0.9417
5.000 1.2380 0.00754 0.00321 -0.1421 0.5275 0.9534
5.500 1.2873 0.00783 0.00345 -0.1412 0.5046 0.9705
5.750 1.3125 0.00801 0.00359 -0.1409 0.4902 0.9934
6.000 1.3396 0.00827 0.00380 -0.1412 0.4757 0.9998
6.250 1.3655 0.00860 0.00406 -0.1412 0.4572 0.9998
6.500 1.3894 0.00905 0.00441 -0.1410 0.4340 0.9998
6.750 1.4091 0.00978 0.00494 -0.1401 0.3944 0.9998
7.000 1.4234 0.01082 0.00571 -0.1384 0.3453 0.9998
7.250 1.4357 0.01189 0.00652 -0.1364 0.3007 0.9998
7.500 1.4478 0.01284 0.00730 -0.1344 0.2672 0.9998
7.750 1.4576 0.01372 0.00805 -0.1319 0.2407 0.9998
8.000 1.4647 0.01474 0.00896 -0.1292 0.2176 0.9998
8.250 1.4705 0.01597 0.01010 -0.1267 0.1943 0.9998
8.500 1.4765 0.01736 0.01139 -0.1246 0.1737 0.9998
8.750 1.4826 0.01889 0.01284 -0.1227 0.1546 0.9998
9.000 1.4895 0.02047 0.01435 -0.1212 0.1389 0.9998
9.250 1.4977 0.02200 0.01586 -0.1198 0.1263 0.9998
9.500 1.5065 0.02353 0.01736 -0.1186 0.1160 0.9998
9.750 1.5143 0.02513 0.01893 -0.1173 0.1065 0.9998
10.000 1.5216 0.02679 0.02056 -0.1159 0.0976 0.9998
10.250 1.5298 0.02837 0.02214 -0.1147 0.0897 0.9998
10.500 1.5368 0.03002 0.02378 -0.1133 0.0828 0.9998
10.750 1.5445 0.03162 0.02538 -0.1121 0.0769 0.9998
11.000 1.5512 0.03332 0.02707 -0.1108 0.0712 0.9998
11.250 1.5572 0.03504 0.02879 -0.1094 0.0653 0.9998
11.500 1.5635 0.03675 0.03051 -0.1081 0.0604 0.9998
11.750 1.5700 0.03849 0.03225 -0.1069 0.0559 0.9998
12.000 1.5769 0.04023 0.03401 -0.1057 0.0521 0.9998
12.250 1.5840 0.04195 0.03574 -0.1046 0.0483 0.9998
12.500 1.5898 0.04385 0.03764 -0.1034 0.0447 0.9998
12.750 1.5980 0.04553 0.03935 -0.1025 0.0419 0.9998
13.000 1.6037 0.04748 0.04132 -0.1015 0.0392 0.9998
13.250 1.6111 0.04926 0.04312 -0.1005 0.0370 0.9998
13.500 1.6180 0.05111 0.04501 -0.0996 0.0348 0.9998
13.750 1.6234 0.05316 0.04707 -0.0987 0.0325 0.9998
14.000 1.6310 0.05498 0.04893 -0.0978 0.0309 0.9998
14.250 1.6371 0.05699 0.05098 -0.0970 0.0292 0.9998
14.500 1.6424 0.05906 0.05307 -0.0962 0.0275 0.9998
14.750 1.6484 0.06109 0.05514 -0.0954 0.0261 0.9998
15.000 1.6543 0.06317 0.05727 -0.0947 0.0249 0.9998
15.250 1.6599 0.06527 0.05940 -0.0940 0.0235 0.9998
15.500 1.6634 0.06765 0.06180 -0.0933 0.0221 0.9998
15.750 1.6692 0.06977 0.06399 -0.0927 0.0213 0.9998
16.000 1.6742 0.07197 0.06623 -0.0921 0.0204 0.9998
16.250 1.6775 0.07441 0.06872 -0.0916 0.0194 0.9998
16.500 1.6810 0.07682 0.07117 -0.0910 0.0184 0.9998
16.750 1.6844 0.07931 0.07371 -0.0906 0.0177 0.9998
17.000 1.6882 0.08173 0.07619 -0.0902 0.0169 0.9998
17.250 1.6909 0.08430 0.07882 -0.0898 0.0162 0.9998
17.500 1.6925 0.08701 0.08158 -0.0895 0.0155 0.9998
17.750 1.6938 0.08978 0.08439 -0.0892 0.0149 0.9998
18.000 1.6959 0.09249 0.08718 -0.0890 0.0145 0.9998
18.250 1.6984 0.09516 0.08991 -0.0888 0.0139 0.9998
18.500 1.6988 0.09812 0.09294 -0.0888 0.0134 0.9998
18.750 1.6997 0.10102 0.09590 -0.0888 0.0128 0.9998
19.000 1.6981 0.10427 0.09920 -0.0889 0.0123 0.9998
19.250 1.6983 0.10728 0.10228 -0.0890 0.0118 0.9998
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