FX 83-W-227 (fx83w227-il) Xfoil prediction polar at RE=200,000 Ncrit=5
| Details | Polar file |
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Airfoil: FX 83-W-227 (fx83w227-il) Reynolds number: 200,000 Max Cl/Cd: 49.98 at α=8° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx83w227-il-200000-n5.txt Download as CSV file: xf-fx83w227-il-200000-n5.csv |
XFOIL Version 6.96
Calculated polar for: FX 83-W-227
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
------ -------- --------- --------- -------- -------- --------
-19.250 -0.6859 0.11101 0.10618 -0.0836 1.0000 0.0549
-19.000 -0.7364 0.09975 0.09467 -0.0892 1.0000 0.0556
-18.750 -0.7664 0.09240 0.08714 -0.0925 1.0000 0.0563
-18.500 -0.7913 0.08616 0.08073 -0.0950 1.0000 0.0571
-18.250 -0.8116 0.08089 0.07529 -0.0968 1.0000 0.0578
-18.000 -0.8301 0.07614 0.07036 -0.0982 1.0000 0.0585
-17.750 -0.8415 0.07261 0.06674 -0.0987 1.0000 0.0591
-17.500 -0.8463 0.07016 0.06428 -0.0985 1.0000 0.0598
-17.250 -0.8527 0.06764 0.06173 -0.0983 1.0000 0.0604
-17.000 -0.8563 0.06497 0.05901 -0.0987 0.9996 0.0611
-16.750 -0.8469 0.06168 0.05562 -0.1020 0.9972 0.0622
-16.500 -0.8379 0.05852 0.05233 -0.1052 0.9943 0.0634
-16.250 -0.8292 0.05550 0.04915 -0.1080 0.9913 0.0645
-16.000 -0.8208 0.05261 0.04607 -0.1105 0.9876 0.0657
-15.750 -0.8051 0.05058 0.04405 -0.1127 0.9845 0.0667
-15.500 -0.7889 0.04851 0.04193 -0.1152 0.9819 0.0678
-15.250 -0.7772 0.04651 0.03986 -0.1166 0.9766 0.0690
-15.000 -0.7621 0.04457 0.03783 -0.1185 0.9724 0.0703
-14.750 -0.7443 0.04269 0.03583 -0.1208 0.9695 0.0718
-14.500 -0.7329 0.04103 0.03403 -0.1213 0.9624 0.0730
-14.250 -0.7145 0.03943 0.03244 -0.1230 0.9582 0.0743
-14.000 -0.6981 0.03794 0.03092 -0.1241 0.9528 0.0756
-13.750 -0.6828 0.03653 0.02945 -0.1249 0.9462 0.0771
-13.500 -0.6610 0.03512 0.02796 -0.1267 0.9422 0.0790
-13.250 -0.6455 0.03393 0.02665 -0.1270 0.9340 0.0807
-13.000 -0.6235 0.03264 0.02532 -0.1286 0.9288 0.0824
-12.750 -0.5993 0.03139 0.02405 -0.1306 0.9239 0.0841
-12.500 -0.5789 0.03030 0.02290 -0.1316 0.9159 0.0861
-12.250 -0.5502 0.02919 0.02170 -0.1339 0.9108 0.0886
-12.000 -0.5274 0.02823 0.02065 -0.1350 0.9029 0.0910
-11.750 -0.5028 0.02715 0.01956 -0.1367 0.8957 0.0933
-11.500 -0.4774 0.02623 0.01858 -0.1382 0.8880 0.0959
-11.250 -0.4525 0.02542 0.01766 -0.1394 0.8792 0.0989
-11.000 -0.4279 0.02458 0.01676 -0.1405 0.8711 0.1019
-10.750 -0.4091 0.02383 0.01597 -0.1405 0.8616 0.1047
-10.500 -0.3868 0.02316 0.01522 -0.1409 0.8533 0.1082
-10.250 -0.3685 0.02264 0.01458 -0.1403 0.8438 0.1113
-10.000 -0.3512 0.02196 0.01388 -0.1398 0.8355 0.1146
-9.750 -0.3381 0.02146 0.01334 -0.1383 0.8263 0.1183
-9.500 -0.3184 0.02101 0.01277 -0.1377 0.8191 0.1225
-9.250 -0.3079 0.02053 0.01228 -0.1356 0.8103 0.1259
-9.000 -0.2937 0.02008 0.01178 -0.1340 0.8027 0.1301
-8.750 -0.2783 0.01972 0.01135 -0.1325 0.7957 0.1351
-8.500 -0.2674 0.01932 0.01094 -0.1301 0.7880 0.1395
-8.250 -0.2526 0.01894 0.01050 -0.1284 0.7815 0.1446
-8.000 -0.2393 0.01866 0.01017 -0.1263 0.7747 0.1502
-7.750 -0.2293 0.01829 0.00981 -0.1236 0.7675 0.1556
-7.500 -0.2139 0.01797 0.00943 -0.1218 0.7618 0.1625
-7.250 -0.2039 0.01769 0.00915 -0.1189 0.7551 0.1687
-7.000 -0.1933 0.01741 0.00887 -0.1161 0.7485 0.1763
-6.750 -0.1792 0.01714 0.00855 -0.1138 0.7429 0.1848
-6.500 -0.1707 0.01693 0.00836 -0.1104 0.7367 0.1935
-6.250 -0.1618 0.01675 0.00818 -0.1071 0.7303 0.2026
-6.000 -0.1491 0.01655 0.00796 -0.1044 0.7249 0.2146
-5.750 -0.1379 0.01633 0.00777 -0.1015 0.7194 0.2270
-5.500 -0.1274 0.01613 0.00762 -0.0984 0.7132 0.2405
-5.250 -0.1136 0.01590 0.00741 -0.0959 0.7078 0.2572
-5.000 -0.0971 0.01566 0.00718 -0.0940 0.7033 0.2764
-4.750 -0.0871 0.01548 0.00709 -0.0907 0.6973 0.2957
-4.500 -0.0741 0.01527 0.00694 -0.0880 0.6916 0.3173
-4.250 -0.0577 0.01504 0.00676 -0.0859 0.6869 0.3421
-4.000 -0.0428 0.01485 0.00663 -0.0836 0.6819 0.3670
-3.750 -0.0308 0.01467 0.00656 -0.0806 0.6763 0.3917
-3.500 -0.0152 0.01450 0.00645 -0.0783 0.6711 0.4181
-3.250 0.0040 0.01433 0.00633 -0.0767 0.6667 0.4458
-3.000 0.0186 0.01422 0.00631 -0.0741 0.6615 0.4707
-2.750 0.0341 0.01413 0.00630 -0.0717 0.6562 0.4953
-2.500 0.0535 0.01406 0.00626 -0.0701 0.6512 0.5190
-2.250 0.0769 0.01401 0.00619 -0.0692 0.6471 0.5412
-2.000 0.0922 0.01400 0.00624 -0.0667 0.6416 0.5592
-1.750 0.1102 0.01399 0.00626 -0.0647 0.6364 0.5762
-1.500 0.1321 0.01398 0.00624 -0.0635 0.6317 0.5921
-1.250 0.1561 0.01399 0.00622 -0.0627 0.6275 0.6073
-1.000 0.1710 0.01402 0.00627 -0.0602 0.6219 0.6213
-0.750 0.1900 0.01405 0.00633 -0.0584 0.6168 0.6350
-0.500 0.2126 0.01407 0.00633 -0.0573 0.6123 0.6487
-0.250 0.2341 0.01412 0.00633 -0.0561 0.6078 0.6620
0.000 0.2492 0.01416 0.00643 -0.0535 0.6022 0.6724
0.250 0.2670 0.01418 0.00643 -0.0515 0.5971 0.6834
0.500 0.2907 0.01422 0.00645 -0.0507 0.5928 0.6932
0.750 0.3086 0.01426 0.00646 -0.0488 0.5881 0.7031
1.000 0.3235 0.01431 0.00656 -0.0463 0.5825 0.7113
1.250 0.3422 0.01436 0.00657 -0.0445 0.5776 0.7206
1.500 0.3671 0.01440 0.00658 -0.0440 0.5733 0.7282
1.750 0.3830 0.01450 0.00670 -0.0417 0.5683 0.7370
2.000 0.3981 0.01460 0.00681 -0.0394 0.5628 0.7454
2.250 0.4192 0.01467 0.00689 -0.0381 0.5579 0.7532
2.500 0.4426 0.01474 0.00688 -0.0374 0.5536 0.7625
2.750 0.4564 0.01488 0.00711 -0.0348 0.5482 0.7707
3.000 0.4731 0.01500 0.00725 -0.0328 0.5429 0.7799
3.250 0.4944 0.01509 0.00731 -0.0317 0.5382 0.7883
3.500 0.5148 0.01520 0.00742 -0.0304 0.5335 0.7972
3.750 0.5286 0.01536 0.00763 -0.0280 0.5280 0.8069
4.000 0.5484 0.01549 0.00779 -0.0267 0.5230 0.8161
4.250 0.5705 0.01559 0.00785 -0.0258 0.5186 0.8261
4.500 0.5898 0.01576 0.00809 -0.0245 0.5134 0.8363
4.750 0.6076 0.01596 0.00834 -0.0230 0.5079 0.8480
5.000 0.6336 0.01613 0.00853 -0.0230 0.5031 0.8595
5.250 0.6654 0.01630 0.00868 -0.0242 0.4990 0.8712
5.500 0.6912 0.01663 0.00912 -0.0245 0.4933 0.8857
5.750 0.7257 0.01695 0.00948 -0.0265 0.4875 0.8983
6.000 0.7650 0.01724 0.00974 -0.0294 0.4826 0.9104
6.250 0.8016 0.01761 0.01015 -0.0319 0.4779 0.9236
6.500 0.8357 0.01802 0.01062 -0.0341 0.4721 0.9371
6.750 0.8719 0.01838 0.01097 -0.0365 0.4670 0.9483
7.000 0.9079 0.01871 0.01125 -0.0388 0.4623 0.9591
7.250 0.9366 0.01920 0.01182 -0.0401 0.4570 0.9719
7.500 0.9665 0.01964 0.01227 -0.0415 0.4518 0.9837
7.750 0.9995 0.02004 0.01263 -0.0434 0.4469 0.9937
8.000 1.0265 0.02054 0.01314 -0.0444 0.4423 1.0000
8.250 1.0295 0.02094 0.01356 -0.0407 0.4376 1.0000
8.500 1.0375 0.02132 0.01393 -0.0379 0.4332 1.0000
8.750 1.0500 0.02165 0.01421 -0.0358 0.4291 1.0000
9.000 1.0598 0.02210 0.01467 -0.0334 0.4248 1.0000
9.250 1.0660 0.02269 0.01531 -0.0306 0.4199 1.0000
9.500 1.0764 0.02320 0.01582 -0.0284 0.4154 1.0000
9.750 1.0908 0.02361 0.01621 -0.0268 0.4114 1.0000
10.000 1.1017 0.02418 0.01679 -0.0249 0.4071 1.0000
10.250 1.1082 0.02494 0.01762 -0.0225 0.4022 1.0000
10.500 1.1191 0.02557 0.01826 -0.0207 0.3978 1.0000
10.750 1.1338 0.02607 0.01873 -0.0193 0.3937 1.0000
11.000 1.1444 0.02677 0.01947 -0.0176 0.3894 1.0000
11.250 1.1500 0.02773 0.02050 -0.0154 0.3845 1.0000
11.500 1.1601 0.02851 0.02130 -0.0137 0.3798 1.0000
11.750 1.1752 0.02905 0.02181 -0.0126 0.3756 1.0000
12.000 1.1809 0.03011 0.02295 -0.0107 0.3706 1.0000
12.250 1.1859 0.03126 0.02417 -0.0088 0.3653 1.0000
12.500 1.1966 0.03211 0.02501 -0.0075 0.3604 1.0000
12.750 1.2099 0.03282 0.02572 -0.0064 0.3561 1.0000
13.000 1.2107 0.03437 0.02739 -0.0044 0.3506 1.0000
13.250 1.2174 0.03556 0.02862 -0.0030 0.3453 1.0000
13.500 1.2305 0.03632 0.02934 -0.0021 0.3405 1.0000
13.750 1.2297 0.03815 0.03128 -0.0003 0.3344 1.0000
14.000 1.2326 0.03970 0.03286 0.0011 0.3275 1.0000
14.250 1.2388 0.04104 0.03419 0.0023 0.3211 1.0000
14.500 1.2362 0.04318 0.03643 0.0038 0.3136 1.0000
14.750 1.2425 0.04458 0.03779 0.0048 0.3070 1.0000
15.000 1.2403 0.04686 0.04017 0.0060 0.2999 1.0000
15.250 1.2426 0.04873 0.04206 0.0070 0.2929 1.0000
15.500 1.2451 0.05065 0.04402 0.0079 0.2868 1.0000
15.750 1.2439 0.05300 0.04645 0.0087 0.2799 1.0000
16.000 1.2488 0.05472 0.04814 0.0094 0.2736 1.0000
16.250 1.2456 0.05739 0.05093 0.0101 0.2668 1.0000
16.500 1.2454 0.05972 0.05327 0.0108 0.2595 1.0000
16.750 1.2450 0.06216 0.05577 0.0113 0.2532 1.0000
17.000 1.2422 0.06490 0.05856 0.0118 0.2455 1.0000
17.250 1.2404 0.06753 0.06121 0.0122 0.2382 1.0000
17.500 1.2357 0.07057 0.06431 0.0125 0.2302 1.0000
17.750 1.2328 0.07341 0.06716 0.0127 0.2224 1.0000
18.000 1.2276 0.07658 0.07037 0.0129 0.2142 1.0000
18.250 1.2221 0.07982 0.07364 0.0129 0.2058 1.0000
18.500 1.2170 0.08305 0.07687 0.0129 0.1976 1.0000
18.750 1.2106 0.08650 0.08036 0.0128 0.1889 1.0000
19.000 1.2038 0.08999 0.08382 0.0126 0.1806 1.0000
19.250 1.1972 0.09355 0.08743 0.0123 0.1718 1.0000
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