WORTMANN FX 05-188 AIRFOIL (fx05188-il) Xfoil prediction polar at RE=200,000 Ncrit=5
| Details | Polar file |
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Airfoil: WORTMANN FX 05-188 AIRFOIL (fx05188-il) Reynolds number: 200,000 Max Cl/Cd: 64.55 at α=7° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx05188-il-200000-n5.txt Download as CSV file: xf-fx05188-il-200000-n5.csv |
XFOIL Version 6.96
Calculated polar for: WORTMANN FX 05-188 AIRFOIL
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.200 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-14.750 -0.5902 0.07820 0.07363 -0.0920 0.9775 0.0214
-14.500 -0.6079 0.07010 0.06521 -0.0995 0.9525 0.0214
-14.250 -0.6171 0.06331 0.05807 -0.1066 0.9404 0.0213
-14.000 -0.6176 0.05791 0.05235 -0.1126 0.9290 0.0214
-13.750 -0.6112 0.05361 0.04777 -0.1175 0.9166 0.0215
-13.500 -0.6023 0.05003 0.04392 -0.1215 0.9039 0.0217
-13.250 -0.5918 0.04700 0.04063 -0.1246 0.8926 0.0218
-13.000 -0.5810 0.04447 0.03786 -0.1267 0.8824 0.0220
-12.750 -0.5708 0.04219 0.03534 -0.1280 0.8738 0.0222
-12.500 -0.5589 0.04015 0.03306 -0.1289 0.8662 0.0223
-12.250 -0.5456 0.03844 0.03116 -0.1294 0.8598 0.0225
-12.000 -0.5336 0.03705 0.02964 -0.1293 0.8533 0.0230
-11.750 -0.5197 0.03565 0.02805 -0.1291 0.8477 0.0233
-11.500 -0.5047 0.03437 0.02660 -0.1289 0.8428 0.0238
-11.250 -0.4896 0.03322 0.02529 -0.1283 0.8376 0.0241
-11.000 -0.4721 0.03213 0.02402 -0.1279 0.8327 0.0246
-10.750 -0.4518 0.03113 0.02286 -0.1276 0.8286 0.0249
-10.500 -0.4314 0.03025 0.02187 -0.1272 0.8246 0.0251
-10.250 -0.4122 0.02946 0.02097 -0.1265 0.8205 0.0254
-10.000 -0.3905 0.02867 0.02014 -0.1261 0.8169 0.0257
-9.750 -0.3703 0.02790 0.01936 -0.1255 0.8135 0.0261
-9.500 -0.3516 0.02719 0.01861 -0.1250 0.8103 0.0266
-9.250 -0.3357 0.02650 0.01792 -0.1240 0.8063 0.0270
-9.000 -0.3200 0.02581 0.01721 -0.1229 0.8026 0.0275
-8.750 -0.3048 0.02513 0.01650 -0.1219 0.7990 0.0280
-8.500 -0.2896 0.02448 0.01579 -0.1209 0.7958 0.0290
-8.250 -0.2749 0.02385 0.01510 -0.1198 0.7926 0.0297
-8.000 -0.2614 0.02324 0.01445 -0.1184 0.7888 0.0303
-7.750 -0.2512 0.02246 0.01368 -0.1168 0.7850 0.0313
-7.500 -0.2391 0.02179 0.01297 -0.1153 0.7818 0.0320
-7.250 -0.2264 0.02115 0.01228 -0.1138 0.7790 0.0330
-7.000 -0.2139 0.02059 0.01168 -0.1122 0.7758 0.0338
-6.750 -0.2029 0.02007 0.01113 -0.1102 0.7722 0.0350
-6.500 -0.1923 0.01961 0.01063 -0.1081 0.7688 0.0364
-6.250 -0.1826 0.01917 0.01016 -0.1059 0.7658 0.0380
-6.000 -0.1687 0.01872 0.00967 -0.1044 0.7632 0.0410
-5.750 -0.1547 0.01825 0.00921 -0.1030 0.7605 0.0470
-5.500 -0.1419 0.01773 0.00880 -0.1014 0.7570 0.0620
-5.250 -0.1299 0.01703 0.00830 -0.0998 0.7537 0.1009
-4.750 -0.1079 0.01463 0.00694 -0.0978 0.7482 0.3306
-4.250 -0.0647 0.01362 0.00684 -0.0971 0.7429 0.5370
-4.000 -0.0397 0.01384 0.00722 -0.0963 0.7399 0.5776
-3.750 -0.0131 0.01416 0.00758 -0.0957 0.7373 0.5996
-3.500 0.0148 0.01447 0.00785 -0.0955 0.7348 0.6161
-3.250 0.0435 0.01473 0.00803 -0.0955 0.7325 0.6277
-3.000 0.0740 0.01473 0.00789 -0.0964 0.7304 0.6375
-2.750 0.0997 0.01488 0.00802 -0.0960 0.7273 0.6404
-2.500 0.1259 0.01497 0.00808 -0.0958 0.7242 0.6443
-2.250 0.1544 0.01495 0.00798 -0.0964 0.7214 0.6503
-2.000 0.1830 0.01497 0.00792 -0.0967 0.7187 0.6545
-1.750 0.2114 0.01503 0.00793 -0.0969 0.7162 0.6574
-1.500 0.2411 0.01506 0.00789 -0.0974 0.7140 0.6614
-1.250 0.2696 0.01503 0.00779 -0.0981 0.7109 0.6677
-1.000 0.2947 0.01517 0.00794 -0.0977 0.7075 0.6707
-0.750 0.3207 0.01530 0.00808 -0.0974 0.7043 0.6740
-0.500 0.3489 0.01537 0.00812 -0.0976 0.7014 0.6786
-0.250 0.3809 0.01529 0.00794 -0.0990 0.6988 0.6847
0.000 0.4098 0.01536 0.00798 -0.0991 0.6965 0.6867
0.250 0.4329 0.01551 0.00818 -0.0984 0.6928 0.6892
0.500 0.4579 0.01561 0.00831 -0.0981 0.6890 0.6921
0.750 0.4858 0.01563 0.00833 -0.0984 0.6855 0.6955
1.000 0.5171 0.01558 0.00822 -0.0995 0.6826 0.6999
1.250 0.5469 0.01559 0.00820 -0.1001 0.6800 0.7025
1.500 0.5692 0.01572 0.00840 -0.0991 0.6753 0.7046
1.750 0.5933 0.01578 0.00851 -0.0986 0.6702 0.7071
2.000 0.6213 0.01578 0.00851 -0.0988 0.6662 0.7097
2.250 0.6518 0.01575 0.00845 -0.0995 0.6632 0.7127
2.500 0.6772 0.01582 0.00857 -0.0996 0.6585 0.7166
2.750 0.7019 0.01589 0.00870 -0.0993 0.6539 0.7191
3.000 0.7279 0.01595 0.00880 -0.0990 0.6502 0.7210
3.250 0.7562 0.01596 0.00883 -0.0992 0.6472 0.7231
3.500 0.7783 0.01610 0.00906 -0.0984 0.6421 0.7255
3.750 0.8030 0.01617 0.00920 -0.0982 0.6373 0.7281
4.000 0.8316 0.01619 0.00923 -0.0986 0.6336 0.7311
4.500 0.8822 0.01635 0.00952 -0.0984 0.6242 0.7363
4.750 0.9067 0.01640 0.00963 -0.0979 0.6195 0.7381
5.000 0.9345 0.01636 0.00962 -0.0980 0.6148 0.7399
5.250 0.9537 0.01649 0.00986 -0.0966 0.6067 0.7422
5.500 0.9826 0.01639 0.00975 -0.0969 0.6002 0.7447
5.750 1.0027 0.01656 0.01000 -0.0959 0.5922 0.7474
6.000 1.0313 0.01654 0.01000 -0.0963 0.5855 0.7502
6.250 1.0511 0.01666 0.01018 -0.0951 0.5752 0.7524
6.500 1.0700 0.01672 0.01024 -0.0935 0.5624 0.7542
6.750 1.0850 0.01682 0.01035 -0.0912 0.5467 0.7562
7.000 1.0973 0.01700 0.01053 -0.0885 0.5300 0.7585
7.250 1.1088 0.01729 0.01080 -0.0859 0.5118 0.7610
7.500 1.1204 0.01769 0.01116 -0.0835 0.4913 0.7636
7.750 1.1308 0.01821 0.01161 -0.0811 0.4688 0.7664
8.000 1.1381 0.01888 0.01222 -0.0783 0.4431 0.7687
8.250 1.1410 0.01971 0.01297 -0.0750 0.4178 0.7706
8.500 1.1413 0.02078 0.01394 -0.0715 0.3910 0.7727
8.750 1.1403 0.02207 0.01512 -0.0683 0.3617 0.7750
9.000 1.1373 0.02362 0.01653 -0.0651 0.3273 0.7771
9.250 1.1295 0.02558 0.01827 -0.0618 0.2865 0.7795
9.500 1.1217 0.02775 0.02023 -0.0588 0.2470 0.7820
9.750 1.1151 0.03003 0.02230 -0.0563 0.2089 0.7840
10.000 1.1110 0.03217 0.02428 -0.0540 0.1774 0.7854
10.250 1.1086 0.03430 0.02628 -0.0520 0.1495 0.7868
10.500 1.1095 0.03628 0.02817 -0.0504 0.1245 0.7884
10.750 1.1119 0.03824 0.03005 -0.0491 0.1052 0.7902
11.000 1.1162 0.04014 0.03190 -0.0480 0.0917 0.7922
11.250 1.1218 0.04201 0.03376 -0.0471 0.0822 0.7942
11.500 1.1292 0.04381 0.03558 -0.0465 0.0741 0.7960
11.750 1.1371 0.04562 0.03742 -0.0459 0.0666 0.7978
12.000 1.1443 0.04758 0.03939 -0.0455 0.0592 0.7996
12.250 1.1515 0.04947 0.04131 -0.0449 0.0521 0.8011
12.500 1.1588 0.05139 0.04328 -0.0444 0.0465 0.8026
12.750 1.1654 0.05344 0.04537 -0.0440 0.0426 0.8042
13.000 1.1723 0.05551 0.04750 -0.0436 0.0399 0.8061
13.250 1.1782 0.05776 0.04979 -0.0433 0.0378 0.8081
13.500 1.1845 0.06005 0.05215 -0.0432 0.0364 0.8104
13.750 1.1913 0.06234 0.05453 -0.0432 0.0350 0.8127
14.000 1.1976 0.06477 0.05704 -0.0433 0.0338 0.8149
14.250 1.2025 0.06729 0.05963 -0.0433 0.0327 0.8166
14.500 1.2060 0.07002 0.06243 -0.0433 0.0318 0.8183
14.750 1.2113 0.07260 0.06511 -0.0435 0.0310 0.8203
15.000 1.2171 0.07516 0.06778 -0.0437 0.0302 0.8223
15.250 1.2228 0.07779 0.07050 -0.0440 0.0294 0.8246
15.500 1.2282 0.08051 0.07332 -0.0444 0.0288 0.8269
15.750 1.2336 0.08326 0.07616 -0.0449 0.0282 0.8293
16.000 1.2386 0.08608 0.07906 -0.0454 0.0277 0.8316
16.250 1.2429 0.08887 0.08193 -0.0459 0.0273 0.8337
16.500 1.2468 0.09174 0.08486 -0.0463 0.0268 0.8360
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