WORTMANN FX 75-193 (fx75193-il) Xfoil prediction polar at RE=200,000 Ncrit=9
| Details | Polar file |
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Airfoil: WORTMANN FX 75-193 (fx75193-il) Reynolds number: 200,000 Max Cl/Cd: 43.37 at α=10° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-fx75193-il-200000.txt Download as CSV file: xf-fx75193-il-200000.csv |
XFOIL Version 6.96
Calculated polar for: WORTMANN FX 75-193
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
------ -------- --------- --------- -------- -------- --------
-13.750 -0.0441 0.10753 0.10308 -0.1585 0.8862 0.0584
-13.500 -0.0233 0.10635 0.10189 -0.1578 0.8854 0.0593
-13.250 -0.0131 0.10411 0.09965 -0.1588 0.8845 0.0620
-13.000 -0.0311 0.09747 0.09307 -0.1631 0.8836 0.0647
-12.750 -0.0152 0.09600 0.09159 -0.1630 0.8828 0.0661
-12.500 -0.2520 0.05660 0.05149 -0.1785 0.8813 0.0302
-12.250 -0.2821 0.05386 0.04854 -0.1768 0.8796 0.0303
-12.000 -0.2809 0.05154 0.04617 -0.1760 0.8780 0.0301
-11.750 -0.2801 0.04954 0.04412 -0.1750 0.8764 0.0298
-11.500 -0.3076 0.04750 0.04184 -0.1716 0.8747 0.0300
-11.250 -0.3140 0.04574 0.03999 -0.1692 0.8732 0.0297
-11.000 -0.3275 0.04417 0.03831 -0.1656 0.8710 0.0296
-10.750 -0.3479 0.04302 0.03699 -0.1608 0.8683 0.0298
-10.500 -0.3551 0.04167 0.03552 -0.1573 0.8657 0.0295
-10.250 -0.3662 0.04066 0.03434 -0.1529 0.8630 0.0293
-10.000 -0.3710 0.03952 0.03301 -0.1491 0.8604 0.0290
-9.750 -0.3671 0.03784 0.03105 -0.1465 0.8583 0.0285
-9.500 -0.3565 0.03620 0.02914 -0.1445 0.8567 0.0281
-9.250 -0.3384 0.03479 0.02745 -0.1434 0.8553 0.0279
-9.000 -0.3449 0.03460 0.02718 -0.1384 0.8524 0.0279
-8.750 -0.3635 0.03498 0.02752 -0.1312 0.8473 0.0278
-8.500 -0.3556 0.03449 0.02693 -0.1281 0.8443 0.0279
-8.250 -0.3310 0.03359 0.02595 -0.1275 0.8424 0.0285
-8.000 -0.2869 0.03241 0.02467 -0.1296 0.8415 0.0293
-7.750 -0.2556 0.03168 0.02383 -0.1299 0.8402 0.0303
-7.500 -0.4129 0.03563 0.02791 -0.1015 0.8254 0.0283
-7.250 -0.3858 0.03480 0.02700 -0.1014 0.8234 0.0291
-7.000 -0.3506 0.03388 0.02597 -0.1025 0.8221 0.0302
-6.750 -0.3150 0.03293 0.02510 -0.1042 0.8209 0.0318
-6.500 -0.3127 0.03287 0.02500 -0.1005 0.8164 0.0335
-6.250 -0.2544 0.03124 0.02339 -0.1064 0.8182 0.0394
-6.000 -0.3465 0.03329 0.02535 -0.0870 0.8037 0.0345
-5.750 -0.3131 0.03223 0.02433 -0.0887 0.8023 0.0392
-5.500 -0.2889 0.03138 0.02356 -0.0891 0.7998 0.0496
-5.250 -0.3368 0.03249 0.02460 -0.0777 0.7883 0.0453
-5.000 -0.3059 0.03155 0.02377 -0.0790 0.7864 0.0678
-4.750 -0.2692 0.03083 0.02321 -0.0813 0.7850 0.0950
-4.500 -0.2305 0.02985 0.02250 -0.0842 0.7841 0.1437
-2.750 -0.1398 0.03357 0.02829 -0.0666 0.7523 0.6676
-2.500 -0.1426 0.03432 0.02893 -0.0629 0.7435 0.6775
-2.250 -0.1239 0.03525 0.02987 -0.0596 0.7401 0.6838
-2.000 -0.0951 0.03587 0.03041 -0.0587 0.7382 0.6958
-1.750 -0.0672 0.03650 0.03101 -0.0566 0.7369 0.7043
-1.500 -0.0769 0.03725 0.03173 -0.0518 0.7271 0.7126
-1.250 -0.0584 0.03795 0.03243 -0.0483 0.7247 0.7244
-1.000 -0.0382 0.03835 0.03282 -0.0445 0.7231 0.7359
-0.750 -0.0399 0.03900 0.03344 -0.0411 0.7145 0.7469
-0.500 -0.0242 0.03909 0.03351 -0.0379 0.7114 0.7529
-0.250 0.0085 0.03894 0.03326 -0.0391 0.7097 0.7582
0.000 0.0501 0.03874 0.03293 -0.0428 0.7085 0.7629
0.250 0.0796 0.03833 0.03248 -0.0426 0.7076 0.7652
0.500 0.0639 0.03910 0.03327 -0.0369 0.6964 0.7692
0.750 0.0965 0.03884 0.03294 -0.0379 0.6946 0.7729
1.000 0.1338 0.03854 0.03257 -0.0400 0.6934 0.7754
1.250 0.1732 0.03826 0.03222 -0.0427 0.6925 0.7777
1.500 0.1701 0.03931 0.03323 -0.0407 0.6812 0.7806
1.750 0.1996 0.03887 0.03276 -0.0409 0.6793 0.7822
2.000 0.2317 0.03844 0.03230 -0.0415 0.6779 0.7843
2.250 0.2664 0.03803 0.03186 -0.0425 0.6769 0.7866
2.500 0.3040 0.03760 0.03140 -0.0442 0.6761 0.7885
2.750 0.2925 0.03892 0.03273 -0.0405 0.6635 0.7910
3.000 0.3284 0.03862 0.03240 -0.0423 0.6622 0.7928
3.250 0.3667 0.03825 0.03200 -0.0444 0.6612 0.7947
3.500 0.4072 0.03782 0.03156 -0.0468 0.6604 0.7964
3.750 0.3996 0.03932 0.03305 -0.0439 0.6477 0.7983
4.000 0.4310 0.03881 0.03255 -0.0444 0.6463 0.7999
4.250 0.4654 0.03823 0.03199 -0.0452 0.6453 0.8018
4.500 0.5014 0.03761 0.03140 -0.0464 0.6445 0.8038
4.750 0.4923 0.03914 0.03295 -0.0428 0.6314 0.8058
5.000 0.5289 0.03858 0.03240 -0.0443 0.6301 0.8073
5.250 0.5660 0.03801 0.03185 -0.0458 0.6291 0.8091
5.500 0.6044 0.03735 0.03123 -0.0474 0.6282 0.8111
5.750 0.6435 0.03670 0.03060 -0.0493 0.6275 0.8129
6.000 0.6331 0.03878 0.03270 -0.0461 0.6137 0.8143
6.250 0.6712 0.03817 0.03212 -0.0478 0.6126 0.8153
6.500 0.7085 0.03720 0.03121 -0.0489 0.6117 0.8165
6.750 0.7469 0.03610 0.03018 -0.0501 0.6111 0.8180
7.000 0.7862 0.03492 0.02906 -0.0513 0.6107 0.8197
7.250 0.8268 0.03379 0.02801 -0.0528 0.6104 0.8212
7.500 0.8687 0.03271 0.02701 -0.0546 0.6100 0.8224
7.750 0.8517 0.03501 0.02935 -0.0502 0.5950 0.8234
8.000 0.8485 0.03672 0.03111 -0.0476 0.5830 0.8244
8.250 0.8886 0.03553 0.03000 -0.0490 0.5815 0.8254
8.500 0.9317 0.03420 0.02876 -0.0507 0.5804 0.8265
8.750 0.9870 0.03197 0.02663 -0.0536 0.5798 0.8280
9.000 1.0690 0.02794 0.02268 -0.0591 0.5778 0.8295
9.250 1.0887 0.02756 0.02232 -0.0580 0.5640 0.8307
9.500 1.1172 0.02681 0.02157 -0.0580 0.5491 0.8315
9.750 1.1424 0.02647 0.02123 -0.0577 0.5340 0.8321
10.000 1.1576 0.02669 0.02143 -0.0564 0.5164 0.8327
10.250 1.1671 0.02721 0.02193 -0.0544 0.4976 0.8335
10.500 1.1726 0.02794 0.02265 -0.0519 0.4777 0.8345
10.750 1.1777 0.02876 0.02343 -0.0495 0.4545 0.8356
11.000 1.1833 0.02966 0.02423 -0.0473 0.4297 0.8364
11.250 1.1832 0.03100 0.02548 -0.0447 0.4009 0.8369
11.500 1.1800 0.03261 0.02692 -0.0419 0.3683 0.8373
11.750 1.1750 0.03448 0.02864 -0.0392 0.3355 0.8378
12.000 1.1656 0.03679 0.03075 -0.0362 0.2992 0.8386
12.250 1.1536 0.03952 0.03326 -0.0335 0.2576 0.8394
12.500 1.1367 0.04285 0.03629 -0.0307 0.2095 0.8398
12.750 1.1200 0.04644 0.03957 -0.0284 0.1602 0.8400
13.000 1.1042 0.05021 0.04300 -0.0265 0.1138 0.8402
13.250 1.0898 0.05408 0.04658 -0.0250 0.0761 0.8403
13.500 1.0793 0.05779 0.05011 -0.0238 0.0532 0.8405
13.750 1.0731 0.06125 0.05350 -0.0231 0.0434 0.8407
14.000 1.0702 0.06446 0.05674 -0.0226 0.0388 0.8412
14.250 1.0685 0.06760 0.05992 -0.0223 0.0358 0.8419
14.500 1.0708 0.07039 0.06279 -0.0222 0.0333 0.8426
14.750 1.0719 0.07336 0.06577 -0.0223 0.0321 0.8430
15.000 1.0779 0.07583 0.06835 -0.0223 0.0305 0.8434
15.250 1.0834 0.07836 0.07091 -0.0225 0.0294 0.8438
15.500 1.0900 0.08074 0.07329 -0.0228 0.0286 0.8442
15.750 1.0997 0.08277 0.07535 -0.0229 0.0278 0.8446
16.000 1.1118 0.08451 0.07717 -0.0231 0.0271 0.8451
16.250 1.1253 0.08608 0.07878 -0.0232 0.0264 0.8457
16.500 1.1412 0.08735 0.08009 -0.0234 0.0260 0.8462
16.750 1.1592 0.08837 0.08110 -0.0235 0.0254 0.8469
17.000 1.1840 0.08859 0.08128 -0.0235 0.0250 0.8476
17.250 1.2099 0.08893 0.08166 -0.0235 0.0247 0.8483
17.500 1.2296 0.09011 0.08298 -0.0237 0.0246 0.8490
17.750 1.2484 0.09151 0.08453 -0.0239 0.0245 0.8497
18.000 1.2658 0.09316 0.08636 -0.0242 0.0244 0.8503
18.250 1.2806 0.09515 0.08853 -0.0246 0.0245 0.8511
18.500 1.2923 0.09752 0.09109 -0.0251 0.0245 0.8519
18.750 1.3029 0.10006 0.09382 -0.0256 0.0246 0.8529
19.000 1.3113 0.10286 0.09681 -0.0262 0.0247 0.8540
19.250 1.3222 0.10555 0.09966 -0.0268 0.0248 0.8553
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