WORTMANN FX 05-188 AIRFOIL (fx05188-il) Xfoil prediction polar at RE=200,000 Ncrit=9
| Details | Polar file |
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Airfoil: WORTMANN FX 05-188 AIRFOIL (fx05188-il) Reynolds number: 200,000 Max Cl/Cd: 60.55 at α=8.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-fx05188-il-200000.txt Download as CSV file: xf-fx05188-il-200000.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 = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-12.250 -0.2842 0.09910 0.09551 -0.0961 0.9532 0.0874
-12.000 -0.1360 0.08024 0.07657 -0.1185 0.9212 0.0999
-11.750 -0.4024 0.06873 0.06483 -0.1277 0.9381 0.0957
-11.500 -0.3517 0.06716 0.06333 -0.1288 0.9348 0.0985
-11.250 -0.4526 0.03740 0.03216 -0.1310 0.8994 0.0580
-11.000 -0.5446 0.04567 0.03943 -0.1272 0.8999 0.0500
-10.750 -0.5070 0.04013 0.03387 -0.1301 0.8977 0.0472
-10.500 -0.5048 0.03739 0.03079 -0.1278 0.8910 0.0454
-10.250 -0.5094 0.03493 0.02766 -0.1242 0.8843 0.0431
-10.000 -0.4869 0.03309 0.02561 -0.1242 0.8806 0.0433
-9.750 -0.4637 0.03151 0.02389 -0.1241 0.8767 0.0436
-9.500 -0.4406 0.03020 0.02251 -0.1237 0.8725 0.0443
-9.250 -0.4080 0.02872 0.02089 -0.1245 0.8693 0.0444
-9.000 -0.3653 0.02730 0.01935 -0.1265 0.8669 0.0446
-8.750 -0.3279 0.02634 0.01832 -0.1277 0.8644 0.0452
-8.500 -0.2942 0.02561 0.01753 -0.1284 0.8618 0.0461
-8.250 -0.2706 0.02509 0.01701 -0.1276 0.8582 0.0469
-8.000 -0.2485 0.02460 0.01650 -0.1266 0.8542 0.0477
-7.750 -0.2291 0.02416 0.01602 -0.1256 0.8505 0.0494
-7.500 -0.2106 0.02351 0.01540 -0.1245 0.8472 0.0512
-7.250 -0.1960 0.02296 0.01487 -0.1231 0.8439 0.0531
-7.000 -0.1886 0.02254 0.01447 -0.1205 0.8394 0.0544
-6.750 -0.1806 0.02207 0.01399 -0.1180 0.8350 0.0562
-6.500 -0.1712 0.02164 0.01349 -0.1157 0.8312 0.0585
-6.250 -0.1689 0.02110 0.01294 -0.1125 0.8277 0.0612
-6.000 -0.1704 0.02091 0.01277 -0.1085 0.8228 0.0645
-5.750 -0.1647 0.02052 0.01237 -0.1059 0.8182 0.0711
-5.500 -0.1596 0.01968 0.01172 -0.1034 0.8142 0.0998
-5.250 -0.1710 0.01707 0.01049 -0.1007 0.8105 0.3627
-5.000 -0.1643 0.01664 0.01084 -0.0981 0.8050 0.5210
-4.750 -0.1416 0.01697 0.01132 -0.0969 0.8014 0.5674
-4.500 -0.1141 0.01739 0.01172 -0.0963 0.7985 0.5940
-4.250 -0.0846 0.01814 0.01243 -0.0957 0.7961 0.6191
-4.000 -0.0539 0.01930 0.01354 -0.0948 0.7940 0.6387
-3.750 -0.0428 0.02071 0.01503 -0.0905 0.7880 0.6475
-3.500 -0.0194 0.02177 0.01608 -0.0883 0.7844 0.6568
-3.250 0.0086 0.02241 0.01663 -0.0877 0.7818 0.6689
-3.000 0.0378 0.02333 0.01753 -0.0859 0.7797 0.6717
-2.750 0.0678 0.02367 0.01780 -0.0855 0.7776 0.6746
-2.500 0.0738 0.02358 0.01768 -0.0837 0.7700 0.6853
-2.250 0.0993 0.02382 0.01788 -0.0827 0.7670 0.6873
-2.000 0.1283 0.02393 0.01794 -0.0824 0.7647 0.6897
-1.750 0.1593 0.02391 0.01784 -0.0829 0.7629 0.6936
-1.500 0.1672 0.02397 0.01789 -0.0811 0.7557 0.7026
-1.250 0.1901 0.02416 0.01806 -0.0798 0.7520 0.7047
-1.000 0.2189 0.02416 0.01803 -0.0797 0.7496 0.7076
-0.750 0.2507 0.02401 0.01780 -0.0806 0.7477 0.7126
-0.500 0.2666 0.02411 0.01789 -0.0798 0.7424 0.7196
-0.250 0.2805 0.02445 0.01826 -0.0772 0.7369 0.7221
0.000 0.3093 0.02441 0.01819 -0.0771 0.7344 0.7256
0.250 0.3445 0.02413 0.01785 -0.0791 0.7324 0.7328
0.500 0.3775 0.02395 0.01762 -0.0799 0.7307 0.7368
0.750 0.3712 0.02477 0.01855 -0.0741 0.7214 0.7403
1.000 0.4019 0.02459 0.01834 -0.0746 0.7186 0.7444
1.250 0.4464 0.02402 0.01768 -0.0789 0.7165 0.7516
1.500 0.4774 0.02377 0.01742 -0.0788 0.7146 0.7535
1.750 0.4732 0.02455 0.01830 -0.0735 0.7061 0.7570
2.000 0.5002 0.02447 0.01823 -0.0736 0.7026 0.7608
2.250 0.5386 0.02414 0.01787 -0.0761 0.7003 0.7657
2.500 0.5757 0.02382 0.01752 -0.0781 0.6984 0.7695
2.750 0.6078 0.02362 0.01732 -0.0784 0.6968 0.7719
3.000 0.5958 0.02461 0.01844 -0.0724 0.6865 0.7766
3.250 0.6330 0.02432 0.01814 -0.0745 0.6839 0.7809
3.500 0.6744 0.02397 0.01778 -0.0775 0.6820 0.7849
3.750 0.7070 0.02370 0.01752 -0.0780 0.6802 0.7871
4.000 0.6951 0.02468 0.01864 -0.0720 0.6703 0.7912
4.250 0.7300 0.02441 0.01839 -0.0734 0.6674 0.7952
4.500 0.7753 0.02404 0.01802 -0.0771 0.6654 0.7995
4.750 0.8113 0.02365 0.01766 -0.0783 0.6636 0.8017
5.000 0.7997 0.02454 0.01868 -0.0723 0.6538 0.8051
5.250 0.8347 0.02417 0.01835 -0.0735 0.6508 0.8082
5.500 0.8834 0.02332 0.01751 -0.0769 0.6485 0.8115
5.750 0.9041 0.02344 0.01770 -0.0766 0.6408 0.8157
6.000 0.9317 0.02286 0.01717 -0.0761 0.6356 0.8179
6.250 0.9755 0.02201 0.01635 -0.0784 0.6324 0.8201
6.500 0.9843 0.02209 0.01653 -0.0754 0.6236 0.8235
6.750 1.0344 0.02077 0.01518 -0.0785 0.6169 0.8265
7.000 1.0541 0.02049 0.01497 -0.0775 0.6059 0.8300
7.250 1.0823 0.01984 0.01434 -0.0773 0.5958 0.8324
7.500 1.1093 0.01922 0.01371 -0.0766 0.5847 0.8349
7.750 1.1147 0.01921 0.01379 -0.0728 0.5725 0.8382
8.000 1.1307 0.01915 0.01377 -0.0709 0.5598 0.8413
8.250 1.1515 0.01916 0.01380 -0.0701 0.5465 0.8443
8.500 1.1686 0.01930 0.01395 -0.0688 0.5312 0.8470
8.750 1.1770 0.01953 0.01421 -0.0658 0.5149 0.8496
9.000 1.1837 0.01995 0.01467 -0.0629 0.4971 0.8524
9.250 1.1893 0.02056 0.01528 -0.0602 0.4759 0.8555
9.500 1.1964 0.02130 0.01598 -0.0580 0.4517 0.8583
9.750 1.2002 0.02238 0.01696 -0.0557 0.4222 0.8611
10.000 1.1986 0.02364 0.01811 -0.0527 0.3915 0.8636
10.250 1.1929 0.02524 0.01956 -0.0494 0.3575 0.8660
10.500 1.1840 0.02723 0.02138 -0.0463 0.3160 0.8684
10.750 1.1698 0.02979 0.02369 -0.0431 0.2704 0.8711
11.000 1.1540 0.03278 0.02640 -0.0403 0.2247 0.8737
11.250 1.1407 0.03593 0.02927 -0.0381 0.1823 0.8757
11.500 1.1315 0.03903 0.03214 -0.0366 0.1464 0.8775
11.750 1.1238 0.04185 0.03479 -0.0349 0.1183 0.8793
12.000 1.1175 0.04474 0.03754 -0.0335 0.0982 0.8813
12.250 1.1119 0.04771 0.04043 -0.0324 0.0847 0.8837
12.500 1.1104 0.05049 0.04320 -0.0315 0.0745 0.8861
12.750 1.1114 0.05318 0.04590 -0.0310 0.0679 0.8885
13.000 1.1167 0.05556 0.04831 -0.0309 0.0632 0.8907
13.250 1.1212 0.05808 0.05081 -0.0307 0.0598 0.8927
13.500 1.1305 0.05991 0.05274 -0.0304 0.0570 0.8950
13.750 1.1395 0.06179 0.05466 -0.0302 0.0546 0.8976
14.000 1.1480 0.06375 0.05660 -0.0300 0.0524 0.9003
14.250 1.1599 0.06542 0.05833 -0.0298 0.0505 0.9033
14.500 1.1731 0.06709 0.06009 -0.0299 0.0488 0.9065
14.750 1.1855 0.06861 0.06167 -0.0296 0.0473 0.9102
15.000 1.1978 0.07006 0.06315 -0.0292 0.0460 0.9145
15.250 1.2133 0.07128 0.06436 -0.0290 0.0449 0.9188
15.500 1.2341 0.07202 0.06511 -0.0285 0.0436 0.9229
15.750 1.2448 0.07359 0.06685 -0.0280 0.0427 0.9285
16.000 1.2560 0.07527 0.06868 -0.0277 0.0417 0.9353
16.250 1.2642 0.07674 0.07029 -0.0268 0.0408 0.9466
16.500 1.2728 0.07812 0.07180 -0.0262 0.0401 1.0000
16.750 1.2887 0.08013 0.07390 -0.0270 0.0393 1.0000
17.000 1.3054 0.08205 0.07589 -0.0277 0.0386 1.0000
17.250 1.3290 0.08342 0.07726 -0.0282 0.0377 1.0000
17.500 1.3403 0.08631 0.08033 -0.0288 0.0371 1.0000
17.750 1.3386 0.09030 0.08459 -0.0301 0.0367 1.0000
18.000 1.3354 0.09457 0.08912 -0.0315 0.0363 1.0000
18.250 1.3303 0.09914 0.09395 -0.0331 0.0360 1.0000
18.500 1.3231 0.10410 0.09917 -0.0349 0.0358 1.0000
18.750 1.3130 0.10958 0.10492 -0.0372 0.0356 1.0000
19.000 1.2995 0.11564 0.11124 -0.0399 0.0355 1.0000
19.250 1.2831 0.12233 0.11819 -0.0432 0.0355 1.0000
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