WORTMANN FX 76-100 (fx76100-il) Xfoil prediction polar at RE=200,000 Ncrit=5
| Details | Polar file |
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Airfoil: WORTMANN FX 76-100 (fx76100-il) Reynolds number: 200,000 Max Cl/Cd: 46.1 at α=5.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx76100-il-200000-n5.txt Download as CSV file: xf-fx76100-il-200000-n5.csv |
XFOIL Version 6.96
Calculated polar for: WORTMANN FX 76-100
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
------ -------- --------- --------- -------- -------- --------
-14.500 -0.8688 0.09910 0.09505 -0.0091 1.0000 0.0183
-14.250 -0.9235 0.08301 0.07872 -0.0195 1.0000 0.0178
-14.000 -0.9659 0.07058 0.06599 -0.0279 1.0000 0.0171
-13.750 -0.9832 0.06367 0.05890 -0.0328 1.0000 0.0173
-13.500 -0.9996 0.05752 0.05255 -0.0368 1.0000 0.0174
-13.250 -1.0117 0.05265 0.04748 -0.0395 1.0000 0.0175
-13.000 -1.0224 0.04852 0.04315 -0.0411 1.0000 0.0177
-12.750 -1.0295 0.04532 0.03977 -0.0415 1.0000 0.0181
-12.500 -1.0349 0.04263 0.03687 -0.0411 1.0000 0.0186
-12.250 -1.0405 0.04005 0.03406 -0.0398 1.0000 0.0190
-12.000 -1.0428 0.03786 0.03167 -0.0378 1.0000 0.0192
-11.750 -1.0436 0.03601 0.02956 -0.0354 1.0000 0.0198
-11.500 -1.0425 0.03431 0.02768 -0.0327 1.0000 0.0203
-11.250 -1.0387 0.03282 0.02612 -0.0301 1.0000 0.0208
-11.000 -1.0302 0.03159 0.02479 -0.0280 1.0000 0.0213
-10.750 -1.0200 0.03037 0.02347 -0.0260 1.0000 0.0221
-10.500 -1.0083 0.02915 0.02211 -0.0241 1.0000 0.0229
-10.250 -0.9951 0.02803 0.02083 -0.0222 1.0000 0.0240
-10.000 -0.9808 0.02690 0.01953 -0.0204 1.0000 0.0250
-9.750 -0.9669 0.02573 0.01825 -0.0186 1.0000 0.0260
-9.500 -0.9520 0.02479 0.01727 -0.0169 1.0000 0.0273
-9.250 -0.9357 0.02392 0.01631 -0.0152 1.0000 0.0287
-9.000 -0.9190 0.02303 0.01532 -0.0136 1.0000 0.0300
-8.750 -0.9014 0.02223 0.01438 -0.0120 1.0000 0.0316
-8.500 -0.8852 0.02132 0.01343 -0.0102 1.0000 0.0335
-8.250 -0.8675 0.02059 0.01266 -0.0086 1.0000 0.0354
-8.000 -0.8490 0.01992 0.01190 -0.0071 1.0000 0.0377
-7.750 -0.8299 0.01931 0.01118 -0.0055 1.0000 0.0400
-7.500 -0.8127 0.01851 0.01038 -0.0038 1.0000 0.0427
-7.250 -0.7936 0.01793 0.00976 -0.0023 1.0000 0.0460
-7.000 -0.7740 0.01740 0.00914 -0.0008 1.0000 0.0494
-6.750 -0.7556 0.01676 0.00850 0.0009 1.0000 0.0540
-6.500 -0.7359 0.01627 0.00797 0.0023 1.0000 0.0595
-6.250 -0.7169 0.01572 0.00743 0.0039 1.0000 0.0658
-6.000 -0.6971 0.01526 0.00695 0.0054 1.0000 0.0743
-5.750 -0.6776 0.01478 0.00650 0.0069 1.0000 0.0860
-5.500 -0.6584 0.01429 0.00610 0.0085 1.0000 0.1021
-5.250 -0.6389 0.01386 0.00575 0.0100 1.0000 0.1225
-5.000 -0.6191 0.01348 0.00546 0.0114 1.0000 0.1446
-4.750 -0.5991 0.01316 0.00519 0.0128 1.0000 0.1662
-4.500 -0.5789 0.01287 0.00496 0.0142 1.0000 0.1870
-4.250 -0.5587 0.01259 0.00476 0.0156 1.0000 0.2072
-4.000 -0.5384 0.01235 0.00457 0.0170 1.0000 0.2283
-3.750 -0.5124 0.01209 0.00439 0.0172 0.9984 0.2511
-3.500 -0.4782 0.01183 0.00421 0.0156 0.9936 0.2783
-3.250 -0.4438 0.01154 0.00406 0.0140 0.9891 0.3108
-3.000 -0.4101 0.01124 0.00390 0.0126 0.9833 0.3465
-2.750 -0.3754 0.01094 0.00375 0.0110 0.9767 0.3857
-2.500 -0.3390 0.01062 0.00361 0.0091 0.9702 0.4281
-2.250 -0.3070 0.01032 0.00347 0.0083 0.9623 0.4684
-2.000 -0.2737 0.01001 0.00336 0.0072 0.9556 0.5150
-1.750 -0.2407 0.00972 0.00326 0.0063 0.9474 0.5637
-1.500 -0.2078 0.00944 0.00317 0.0055 0.9374 0.6119
-1.250 -0.1730 0.00917 0.00310 0.0044 0.9276 0.6593
-1.000 -0.1399 0.00895 0.00305 0.0037 0.9153 0.7048
-0.750 -0.1070 0.00878 0.00303 0.0032 0.9011 0.7466
-0.500 -0.0720 0.00866 0.00301 0.0023 0.8851 0.7843
-0.250 -0.0358 0.00859 0.00301 0.0011 0.8670 0.8169
0.000 0.0001 0.00857 0.00302 0.0000 0.8439 0.8443
0.250 0.0359 0.00859 0.00301 -0.0011 0.8170 0.8670
0.500 0.0721 0.00866 0.00302 -0.0023 0.7850 0.8852
0.750 0.1069 0.00878 0.00302 -0.0031 0.7459 0.9009
1.000 0.1399 0.00895 0.00305 -0.0037 0.7046 0.9153
1.250 0.1729 0.00917 0.00310 -0.0043 0.6583 0.9275
1.500 0.2077 0.00944 0.00317 -0.0054 0.6109 0.9374
1.750 0.2406 0.00971 0.00326 -0.0063 0.5645 0.9474
2.000 0.2737 0.01001 0.00336 -0.0072 0.5148 0.9557
2.250 0.3069 0.01032 0.00347 -0.0083 0.4686 0.9622
2.500 0.3390 0.01062 0.00361 -0.0091 0.4272 0.9702
2.750 0.3754 0.01094 0.00375 -0.0110 0.3853 0.9767
3.000 0.4101 0.01124 0.00390 -0.0126 0.3469 0.9833
3.250 0.4439 0.01154 0.00406 -0.0140 0.3105 0.9891
3.500 0.4785 0.01182 0.00421 -0.0156 0.2794 0.9937
3.750 0.5125 0.01210 0.00439 -0.0172 0.2504 0.9984
4.000 0.5383 0.01235 0.00457 -0.0170 0.2282 1.0000
4.250 0.5586 0.01259 0.00475 -0.0156 0.2069 1.0000
4.500 0.5787 0.01288 0.00496 -0.0142 0.1864 1.0000
4.750 0.5990 0.01316 0.00519 -0.0128 0.1658 1.0000
5.000 0.6190 0.01349 0.00546 -0.0114 0.1443 1.0000
5.250 0.6389 0.01386 0.00575 -0.0099 0.1224 1.0000
5.500 0.6583 0.01429 0.00610 -0.0085 0.1020 1.0000
5.750 0.6776 0.01478 0.00650 -0.0069 0.0863 1.0000
6.000 0.6970 0.01526 0.00695 -0.0054 0.0740 1.0000
6.250 0.7168 0.01572 0.00743 -0.0039 0.0656 1.0000
6.500 0.7359 0.01627 0.00796 -0.0023 0.0592 1.0000
6.750 0.7556 0.01676 0.00850 -0.0008 0.0537 1.0000
7.000 0.7740 0.01740 0.00914 0.0008 0.0493 1.0000
7.250 0.7936 0.01794 0.00977 0.0023 0.0459 1.0000
7.500 0.8126 0.01853 0.01040 0.0038 0.0429 1.0000
7.750 0.8298 0.01931 0.01119 0.0056 0.0400 1.0000
8.000 0.8490 0.01992 0.01190 0.0071 0.0377 1.0000
8.250 0.8673 0.02062 0.01270 0.0087 0.0356 1.0000
8.500 0.8852 0.02133 0.01345 0.0102 0.0336 1.0000
8.750 0.9008 0.02231 0.01445 0.0120 0.0318 1.0000
9.000 0.9187 0.02308 0.01536 0.0136 0.0302 1.0000
9.250 0.9356 0.02395 0.01634 0.0153 0.0288 1.0000
9.500 0.9523 0.02476 0.01722 0.0168 0.0273 1.0000
9.750 0.9674 0.02571 0.01823 0.0185 0.0261 1.0000
10.000 0.9812 0.02687 0.01949 0.0204 0.0249 1.0000
10.250 0.9957 0.02794 0.02075 0.0221 0.0238 1.0000
10.500 1.0086 0.02915 0.02211 0.0240 0.0229 1.0000
10.750 1.0203 0.03035 0.02344 0.0259 0.0220 1.0000
11.000 1.0309 0.03153 0.02473 0.0279 0.0213 1.0000
11.250 1.0394 0.03281 0.02612 0.0300 0.0208 1.0000
11.500 1.0432 0.03429 0.02767 0.0326 0.0203 1.0000
11.750 1.0443 0.03600 0.02955 0.0353 0.0198 1.0000
12.000 1.0439 0.03786 0.03165 0.0377 0.0193 1.0000
12.250 1.0410 0.04001 0.03404 0.0396 0.0187 1.0000
12.500 1.0372 0.04239 0.03662 0.0409 0.0184 1.0000
12.750 1.0319 0.04505 0.03949 0.0413 0.0178 1.0000
13.000 1.0233 0.04852 0.04316 0.0409 0.0176 1.0000
13.250 1.0140 0.05245 0.04728 0.0394 0.0174 1.0000
13.500 1.0019 0.05734 0.05235 0.0367 0.0173 1.0000
13.750 0.9867 0.06328 0.05849 0.0328 0.0171 1.0000
14.000 0.9637 0.07128 0.06672 0.0273 0.0172 1.0000
14.250 0.9285 0.08232 0.07801 0.0197 0.0175 1.0000
14.500 0.8707 0.09907 0.09502 0.0089 0.0183 1.0000
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