WORTMANN FX 05-H-126 AIRFOIL (fx05h126-il) Xfoil prediction polar at RE=200,000 Ncrit=9
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Airfoil: WORTMANN FX 05-H-126 AIRFOIL (fx05h126-il) Reynolds number: 200,000 Max Cl/Cd: 66.25 at α=9.75° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-fx05h126-il-200000.txt Download as CSV file: xf-fx05h126-il-200000.csv |
XFOIL Version 6.96
Calculated polar for: WORTMANN FX 05-H-126 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
------ -------- --------- --------- -------- -------- --------
-8.500 -0.3905 0.09868 0.09484 -0.0115 0.6662 0.0438
-8.250 -0.3988 0.09485 0.09104 -0.0173 0.6653 0.0440
-8.000 -0.4046 0.09109 0.08722 -0.0216 0.6645 0.0441
-7.750 -0.3937 0.08578 0.08198 -0.0189 0.6637 0.0451
-7.500 -0.3814 0.08322 0.07942 -0.0175 0.6628 0.0462
-7.250 -0.3734 0.08017 0.07638 -0.0191 0.6619 0.0472
-7.000 -0.3657 0.07687 0.07307 -0.0218 0.6608 0.0488
-6.750 -0.3579 0.07317 0.06934 -0.0254 0.6597 0.0514
-6.500 -0.3521 0.06998 0.06567 -0.0324 0.6585 0.0549
-6.250 -0.3443 0.06354 0.05923 -0.0339 0.6571 0.0560
-6.000 -0.3283 0.06043 0.05621 -0.0342 0.6556 0.0573
-5.750 -0.3118 0.05793 0.05368 -0.0347 0.6544 0.0589
-5.500 -0.2946 0.05530 0.05094 -0.0354 0.6533 0.0616
-5.250 -0.2718 0.05545 0.05031 -0.0358 0.6522 0.0680
-5.000 -0.2599 0.04873 0.04371 -0.0368 0.6513 0.0700
-4.750 -0.2403 0.04643 0.04140 -0.0370 0.6504 0.0722
-4.500 -0.2197 0.04448 0.03932 -0.0369 0.6495 0.0760
-4.250 -0.1999 0.04223 0.03654 -0.0363 0.6486 0.0844
-4.000 -0.1794 0.04028 0.03464 -0.0361 0.6477 0.0882
-3.750 -0.1550 0.03885 0.03289 -0.0367 0.6458 0.0998
-3.500 -0.1296 0.03728 0.03138 -0.0377 0.6442 0.1043
-3.250 -0.1053 0.03607 0.02998 -0.0383 0.6427 0.1167
-3.000 -0.0688 0.03100 0.02360 -0.0355 0.6414 0.0541
-2.750 -0.0426 0.02908 0.02148 -0.0355 0.6396 0.0516
-2.500 -0.0157 0.02808 0.02026 -0.0353 0.6379 0.0516
-2.250 0.0114 0.02740 0.01940 -0.0352 0.6367 0.0525
-2.000 0.0384 0.02661 0.01847 -0.0350 0.6355 0.0522
-1.750 0.0645 0.02592 0.01767 -0.0343 0.6343 0.0526
-1.500 0.0897 0.02536 0.01701 -0.0334 0.6332 0.0537
-1.250 0.1160 0.02539 0.01702 -0.0337 0.6312 0.0550
-1.000 0.1417 0.02575 0.01758 -0.0359 0.6267 0.0592
-0.750 0.1661 0.02591 0.01776 -0.0360 0.6240 0.0649
-0.500 0.1893 0.02572 0.01755 -0.0353 0.6219 0.0717
-0.250 0.2110 0.02520 0.01722 -0.0339 0.6203 0.1191
0.000 0.3565 0.02213 0.01662 -0.0559 0.6195 1.0000
0.250 0.3778 0.02223 0.01657 -0.0544 0.6182 1.0000
0.500 0.3990 0.02239 0.01659 -0.0528 0.6172 1.0000
0.750 0.4270 0.02464 0.01895 -0.0577 0.6092 1.0000
1.000 0.4492 0.02501 0.01924 -0.0570 0.6067 1.0000
1.250 0.4713 0.02521 0.01936 -0.0558 0.6051 1.0000
1.500 0.4935 0.02528 0.01934 -0.0544 0.6037 1.0000
1.750 0.5159 0.02530 0.01926 -0.0528 0.6026 1.0000
2.000 0.5339 0.02783 0.02189 -0.0560 0.5929 1.0000
2.250 0.5562 0.02806 0.02208 -0.0549 0.5907 1.0000
2.500 0.5795 0.02803 0.02199 -0.0535 0.5892 1.0000
2.750 0.6033 0.02790 0.02180 -0.0519 0.5880 1.0000
3.000 0.6275 0.02773 0.02157 -0.0503 0.5871 1.0000
3.250 0.6377 0.03055 0.02450 -0.0526 0.5754 1.0000
3.500 0.6625 0.03040 0.02431 -0.0512 0.5740 1.0000
3.750 0.6881 0.03012 0.02400 -0.0498 0.5729 1.0000
4.000 0.7138 0.02986 0.02372 -0.0483 0.5721 1.0000
4.250 0.7199 0.03254 0.02650 -0.0496 0.5597 1.0000
4.500 0.7465 0.03223 0.02618 -0.0483 0.5586 1.0000
4.750 0.7500 0.03472 0.02873 -0.0487 0.5473 1.0000
5.000 0.7763 0.03450 0.02853 -0.0476 0.5454 1.0000
5.250 0.8043 0.03408 0.02811 -0.0465 0.5442 1.0000
5.500 0.8325 0.03361 0.02767 -0.0453 0.5433 1.0000
5.750 0.8615 0.03302 0.02709 -0.0441 0.5426 1.0000
6.000 0.8910 0.03236 0.02647 -0.0429 0.5421 1.0000
6.250 0.8623 0.03797 0.03218 -0.0440 0.5190 1.0000
6.500 0.8953 0.03695 0.03121 -0.0430 0.5173 1.0000
6.750 0.9380 0.03449 0.02880 -0.0416 0.5167 1.0000
7.000 0.9819 0.03157 0.02594 -0.0398 0.5168 1.0000
7.250 1.0248 0.02869 0.02309 -0.0383 0.5169 1.0000
7.500 1.0614 0.02677 0.02122 -0.0371 0.5161 1.0000
7.750 1.0983 0.02479 0.01927 -0.0360 0.5150 1.0000
8.000 1.1353 0.02275 0.01724 -0.0350 0.5136 1.0000
8.250 1.1530 0.02323 0.01792 -0.0347 0.5029 1.0000
8.500 1.1897 0.02130 0.01602 -0.0338 0.5001 1.0000
8.750 1.2094 0.02156 0.01648 -0.0336 0.4893 1.0000
9.000 1.2337 0.02123 0.01629 -0.0332 0.4791 1.0000
9.250 1.2576 0.02093 0.01615 -0.0328 0.4652 1.0000
9.500 1.2827 0.02050 0.01580 -0.0324 0.4462 1.0000
9.750 1.3091 0.01976 0.01497 -0.0315 0.4146 1.0000
10.000 1.3193 0.02042 0.01527 -0.0299 0.3643 1.0000
10.250 1.3031 0.02330 0.01790 -0.0278 0.3230 1.0000
10.500 1.2811 0.02656 0.02089 -0.0252 0.2836 1.0000
10.750 1.2581 0.03021 0.02424 -0.0231 0.2436 1.0000
11.000 1.2364 0.03394 0.02766 -0.0212 0.2056 1.0000
11.250 1.2180 0.03751 0.03097 -0.0197 0.1749 1.0000
11.500 1.2054 0.04069 0.03395 -0.0184 0.1514 1.0000
11.750 1.1992 0.04350 0.03661 -0.0175 0.1337 1.0000
12.000 1.1977 0.04599 0.03902 -0.0167 0.1203 1.0000
12.250 1.1983 0.04834 0.04131 -0.0161 0.1090 1.0000
12.500 1.1999 0.05065 0.04355 -0.0156 0.1005 1.0000
12.750 1.2030 0.05284 0.04574 -0.0151 0.0931 1.0000
13.000 1.2069 0.05494 0.04785 -0.0146 0.0871 1.0000
13.250 1.2117 0.05703 0.04999 -0.0142 0.0813 1.0000
13.500 1.2150 0.05924 0.05219 -0.0137 0.0756 1.0000
13.750 1.2203 0.06140 0.05444 -0.0136 0.0697 1.0000
14.000 1.2224 0.06380 0.05684 -0.0132 0.0639 1.0000
14.250 1.2253 0.06644 0.05957 -0.0133 0.0569 1.0000
14.500 1.2260 0.06922 0.06239 -0.0132 0.0497 1.0000
14.750 1.2228 0.07258 0.06573 -0.0133 0.0419 1.0000
15.000 1.2234 0.07558 0.06875 -0.0134 0.0369 1.0000
15.250 1.2239 0.07841 0.07162 -0.0132 0.0331 1.0000
15.500 1.2258 0.08131 0.07459 -0.0135 0.0300 1.0000
15.750 1.2260 0.08405 0.07727 -0.0132 0.0279 1.0000
16.000 1.2312 0.08639 0.07977 -0.0129 0.0266 1.0000
16.250 1.2353 0.08893 0.08241 -0.0128 0.0251 1.0000
16.500 1.2395 0.09138 0.08493 -0.0128 0.0241 1.0000
16.750 1.2433 0.09388 0.08748 -0.0127 0.0232 1.0000
17.000 1.2498 0.09573 0.08934 -0.0119 0.0224 1.0000
17.250 1.2528 0.09842 0.09219 -0.0116 0.0216 1.0000
17.500 1.2546 0.10146 0.09541 -0.0118 0.0214 1.0000
17.750 1.2515 0.10542 0.09959 -0.0128 0.0206 1.0000
18.000 1.2486 0.10936 0.10372 -0.0137 0.0202 1.0000
18.250 1.2445 0.11358 0.10812 -0.0149 0.0197 1.0000
18.500 1.2395 0.11806 0.11275 -0.0166 0.0192 1.0000
18.750 1.2328 0.12291 0.11779 -0.0183 0.0191 1.0000
19.000 1.2235 0.12836 0.12345 -0.0205 0.0190 1.0000
19.250 1.2131 0.13419 0.12945 -0.0232 0.0187 1.0000
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