WORTMANN FX 75-193 (fx75193-il) Xfoil prediction polar at RE=200,000 Ncrit=5
| Details | Polar file |
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Airfoil: WORTMANN FX 75-193 (fx75193-il) Reynolds number: 200,000 Max Cl/Cd: 44.09 at α=7.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx75193-il-200000-n5.txt Download as CSV file: xf-fx75193-il-200000-n5.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 = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-14.750 -0.2453 0.07984 0.07445 -0.1516 0.8182 0.0132
-14.500 -0.2831 0.06945 0.06384 -0.1580 0.8177 0.0131
-14.250 -0.3117 0.06217 0.05634 -0.1618 0.8172 0.0129
-14.000 -0.3273 0.05750 0.05150 -0.1639 0.8165 0.0129
-13.750 -0.3409 0.05351 0.04731 -0.1651 0.8157 0.0130
-13.500 -0.3542 0.04982 0.04341 -0.1656 0.8149 0.0129
-13.250 -0.3604 0.04718 0.04061 -0.1656 0.8141 0.0130
-13.000 -0.3657 0.04469 0.03792 -0.1652 0.8131 0.0132
-12.750 -0.3682 0.04247 0.03551 -0.1645 0.8122 0.0133
-12.500 -0.3669 0.04059 0.03346 -0.1636 0.8110 0.0133
-12.250 -0.3628 0.03897 0.03169 -0.1627 0.8097 0.0133
-12.000 -0.3569 0.03742 0.02997 -0.1616 0.8084 0.0134
-11.750 -0.3486 0.03610 0.02852 -0.1607 0.8074 0.0135
-11.500 -0.3388 0.03489 0.02718 -0.1596 0.8064 0.0135
-11.250 -0.3281 0.03377 0.02594 -0.1586 0.8054 0.0136
-11.000 -0.3166 0.03278 0.02484 -0.1575 0.8044 0.0138
-10.750 -0.3045 0.03190 0.02388 -0.1564 0.8035 0.0138
-10.500 -0.2927 0.03103 0.02291 -0.1552 0.8025 0.0140
-10.250 -0.2823 0.03016 0.02199 -0.1539 0.8014 0.0141
-10.000 -0.2721 0.02942 0.02122 -0.1524 0.8000 0.0143
-9.750 -0.2632 0.02868 0.02045 -0.1507 0.7987 0.0145
-9.500 -0.2539 0.02801 0.01976 -0.1489 0.7972 0.0148
-9.250 -0.2442 0.02739 0.01911 -0.1471 0.7954 0.0150
-9.000 -0.2347 0.02676 0.01845 -0.1452 0.7933 0.0153
-8.750 -0.2243 0.02619 0.01782 -0.1433 0.7913 0.0156
-8.500 -0.2134 0.02564 0.01722 -0.1415 0.7895 0.0161
-8.250 -0.2027 0.02506 0.01660 -0.1396 0.7878 0.0169
-8.000 -0.1907 0.02456 0.01607 -0.1379 0.7862 0.0175
-7.750 -0.1785 0.02409 0.01556 -0.1361 0.7848 0.0184
-7.250 -0.1623 0.02342 0.01491 -0.1312 0.7815 0.0226
-7.000 -0.1596 0.02324 0.01476 -0.1277 0.7789 0.0259
-6.750 -0.1564 0.02307 0.01458 -0.1243 0.7762 0.0303
-6.500 -0.1477 0.02278 0.01428 -0.1219 0.7737 0.0379
-6.250 -0.1368 0.02240 0.01395 -0.1200 0.7717 0.0464
-6.000 -0.1223 0.02206 0.01364 -0.1186 0.7700 0.0557
-5.750 -0.1052 0.02174 0.01331 -0.1176 0.7687 0.0663
-5.500 -0.0868 0.02140 0.01298 -0.1168 0.7674 0.0776
-5.250 -0.0724 0.02115 0.01279 -0.1153 0.7653 0.0934
-5.000 -0.0670 0.02103 0.01283 -0.1124 0.7608 0.1159
-4.750 -0.0543 0.02048 0.01254 -0.1110 0.7579 0.1682
-4.500 -0.0404 0.01951 0.01205 -0.1103 0.7556 0.2718
-4.250 -0.0236 0.01826 0.01155 -0.1102 0.7539 0.4330
-4.000 -0.0023 0.01854 0.01240 -0.1081 0.7525 0.5474
-3.750 0.0256 0.01904 0.01292 -0.1073 0.7515 0.5798
-3.500 0.0370 0.01983 0.01376 -0.1041 0.7468 0.5977
-3.250 0.0542 0.02049 0.01440 -0.1021 0.7428 0.6144
-3.000 0.0809 0.02080 0.01460 -0.1020 0.7405 0.6300
-2.500 0.1379 0.02169 0.01533 -0.1016 0.7376 0.6543
-2.000 0.1582 0.02294 0.01658 -0.0952 0.7277 0.6690
-1.750 0.1865 0.02278 0.01627 -0.0962 0.7255 0.6770
-1.500 0.2128 0.02278 0.01623 -0.0958 0.7240 0.6787
-1.250 0.2411 0.02272 0.01613 -0.0959 0.7229 0.6807
-1.000 0.2274 0.02343 0.01689 -0.0891 0.7134 0.6838
-0.750 0.2533 0.02329 0.01667 -0.0891 0.7113 0.6867
-0.500 0.2842 0.02304 0.01634 -0.0902 0.7099 0.6898
-0.250 0.3182 0.02271 0.01591 -0.0921 0.7089 0.6934
0.000 0.3285 0.02285 0.01604 -0.0893 0.7047 0.6949
0.250 0.3812 0.02223 0.01535 -0.0935 0.7072 0.6960
0.750 0.3850 0.02282 0.01596 -0.0853 0.6940 0.7001
1.000 0.4168 0.02250 0.01561 -0.0861 0.6932 0.7019
1.250 0.4494 0.02216 0.01523 -0.0872 0.6924 0.7039
1.750 0.4617 0.02334 0.01635 -0.0821 0.6783 0.7100
2.000 0.4914 0.02304 0.01605 -0.0825 0.6774 0.7111
2.250 0.5221 0.02270 0.01571 -0.0830 0.6765 0.7123
3.250 0.5939 0.02352 0.01657 -0.0783 0.6587 0.7190
3.750 0.6251 0.02421 0.01728 -0.0757 0.6470 0.7232
4.000 0.6577 0.02385 0.01692 -0.0766 0.6457 0.7250
4.250 0.6915 0.02346 0.01653 -0.0778 0.6446 0.7265
4.750 0.7186 0.02438 0.01751 -0.0747 0.6317 0.7291
5.000 0.7505 0.02397 0.01713 -0.0753 0.6298 0.7302
5.250 0.7859 0.02341 0.01660 -0.0764 0.6283 0.7314
5.750 0.8176 0.02412 0.01741 -0.0737 0.6152 0.7338
6.000 0.8517 0.02367 0.01699 -0.0748 0.6128 0.7349
6.250 0.8898 0.02308 0.01643 -0.0763 0.6111 0.7358
6.750 0.9210 0.02390 0.01736 -0.0737 0.5969 0.7382
7.000 0.9616 0.02318 0.01666 -0.0756 0.5937 0.7394
7.250 0.9660 0.02412 0.01767 -0.0729 0.5840 0.7409
7.500 0.9930 0.02404 0.01764 -0.0731 0.5785 0.7421
7.750 1.0327 0.02342 0.01704 -0.0748 0.5747 0.7429
8.000 1.0312 0.02461 0.01830 -0.0715 0.5630 0.7438
8.250 1.0581 0.02443 0.01812 -0.0715 0.5525 0.7445
8.500 1.0780 0.02455 0.01825 -0.0706 0.5400 0.7454
8.750 1.0892 0.02501 0.01870 -0.0686 0.5230 0.7463
9.000 1.1018 0.02543 0.01909 -0.0668 0.5044 0.7472
9.250 1.1107 0.02602 0.01960 -0.0646 0.4796 0.7479
9.500 1.1159 0.02686 0.02032 -0.0620 0.4521 0.7485
9.750 1.1218 0.02775 0.02108 -0.0596 0.4270 0.7492
10.000 1.1239 0.02892 0.02216 -0.0570 0.3986 0.7500
10.250 1.1212 0.03040 0.02348 -0.0539 0.3666 0.7509
10.500 1.1173 0.03211 0.02501 -0.0509 0.3339 0.7516
10.750 1.1124 0.03401 0.02674 -0.0481 0.3008 0.7522
11.000 1.1076 0.03606 0.02862 -0.0455 0.2674 0.7526
11.250 1.0997 0.03846 0.03081 -0.0429 0.2290 0.7530
11.500 1.0912 0.04107 0.03319 -0.0404 0.1893 0.7535
11.750 1.0846 0.04369 0.03559 -0.0384 0.1514 0.7542
12.000 1.0783 0.04640 0.03808 -0.0366 0.1144 0.7548
12.250 1.0762 0.04888 0.04041 -0.0352 0.0864 0.7553
12.500 1.0751 0.05137 0.04277 -0.0340 0.0655 0.7556
12.750 1.0781 0.05358 0.04492 -0.0332 0.0499 0.7559
13.000 1.0816 0.05582 0.04713 -0.0325 0.0411 0.7562
13.250 1.0874 0.05789 0.04924 -0.0320 0.0340 0.7565
13.500 1.0931 0.06004 0.05142 -0.0315 0.0280 0.7568
13.750 1.0985 0.06225 0.05366 -0.0312 0.0240 0.7571
14.250 1.1088 0.06686 0.05839 -0.0307 0.0199 0.7578
14.500 1.1124 0.06942 0.06100 -0.0305 0.0187 0.7581
14.750 1.1181 0.07180 0.06348 -0.0305 0.0179 0.7584
15.000 1.1225 0.07436 0.06615 -0.0305 0.0170 0.7587
15.250 1.1268 0.07699 0.06887 -0.0306 0.0163 0.7590
15.500 1.1298 0.07981 0.07178 -0.0308 0.0159 0.7593
15.750 1.1331 0.08266 0.07472 -0.0311 0.0154 0.7596
16.000 1.1367 0.08551 0.07768 -0.0315 0.0151 0.7599
16.250 1.1402 0.08842 0.08069 -0.0319 0.0147 0.7603
16.500 1.1433 0.09139 0.08378 -0.0324 0.0145 0.7608
16.750 1.1465 0.09438 0.08687 -0.0331 0.0141 0.7613
17.000 1.1496 0.09743 0.09001 -0.0338 0.0139 0.7617
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