FX 83-W-160 (fx83w160-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: FX 83-W-160 (fx83w160-il) Reynolds number: 1,000,000 Max Cl/Cd: 131.22 at α=4.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-fx83w160-il-1000000.txt Download as CSV file: xf-fx83w160-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: FX 83-W-160
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 1.000 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-18.750 -0.8877 0.09617 0.09312 -0.0800 1.0000 0.0187
-18.500 -0.9042 0.09061 0.08748 -0.0823 1.0000 0.0188
-18.250 -0.9215 0.08519 0.08197 -0.0845 1.0000 0.0188
-18.000 -0.9372 0.08004 0.07675 -0.0865 1.0000 0.0191
-17.750 -0.9521 0.07525 0.07188 -0.0881 1.0000 0.0192
-17.500 -0.9694 0.07038 0.06692 -0.0896 1.0000 0.0193
-17.250 -0.9833 0.06622 0.06269 -0.0906 1.0000 0.0194
-17.000 -0.9914 0.06206 0.05844 -0.0926 0.9998 0.0196
-16.750 -0.9905 0.05756 0.05383 -0.0967 0.9990 0.0199
-16.500 -0.9855 0.05372 0.04989 -0.1004 0.9979 0.0201
-16.250 -0.9772 0.05043 0.04650 -0.1039 0.9967 0.0203
-16.000 -0.9794 0.04589 0.04185 -0.1083 0.9953 0.0206
-15.750 -0.9777 0.04212 0.03800 -0.1119 0.9935 0.0209
-15.500 -0.9714 0.03897 0.03479 -0.1150 0.9912 0.0214
-15.250 -0.9604 0.03624 0.03199 -0.1183 0.9892 0.0217
-15.000 -0.9443 0.03398 0.02966 -0.1214 0.9876 0.0222
-14.750 -0.9251 0.03197 0.02760 -0.1246 0.9864 0.0227
-14.500 -0.9116 0.03003 0.02559 -0.1265 0.9828 0.0231
-14.250 -0.8934 0.02820 0.02368 -0.1291 0.9799 0.0234
-14.000 -0.8685 0.02691 0.02233 -0.1316 0.9782 0.0239
-13.750 -0.8507 0.02441 0.01975 -0.1356 0.9764 0.0247
-13.500 -0.8365 0.02278 0.01809 -0.1370 0.9709 0.0254
-13.250 -0.8129 0.02141 0.01667 -0.1395 0.9679 0.0260
-13.000 -0.7852 0.02016 0.01537 -0.1425 0.9656 0.0267
-12.750 -0.7624 0.01910 0.01424 -0.1442 0.9604 0.0274
-12.500 -0.7342 0.01824 0.01331 -0.1465 0.9563 0.0279
-12.250 -0.7018 0.01678 0.01179 -0.1511 0.9533 0.0293
-12.000 -0.6776 0.01610 0.01108 -0.1521 0.9475 0.0305
-11.750 -0.6503 0.01553 0.01045 -0.1534 0.9421 0.0316
-11.500 -0.6174 0.01495 0.00980 -0.1556 0.9385 0.0329
-11.250 -0.6014 0.01436 0.00919 -0.1546 0.9303 0.0343
-11.000 -0.5741 0.01389 0.00867 -0.1554 0.9249 0.0359
-10.750 -0.5500 0.01357 0.00829 -0.1553 0.9190 0.0373
-10.500 -0.5309 0.01306 0.00775 -0.1545 0.9120 0.0394
-10.250 -0.5040 0.01267 0.00732 -0.1550 0.9070 0.0417
-10.000 -0.4839 0.01241 0.00702 -0.1539 0.9011 0.0435
-9.750 -0.4626 0.01198 0.00658 -0.1533 0.8952 0.0464
-9.500 -0.4355 0.01171 0.00625 -0.1536 0.8901 0.0489
-9.250 -0.4155 0.01141 0.00594 -0.1524 0.8846 0.0517
-9.000 -0.3921 0.01113 0.00566 -0.1519 0.8793 0.0550
-8.750 -0.3660 0.01089 0.00537 -0.1520 0.8745 0.0587
-8.500 -0.3428 0.01063 0.00512 -0.1514 0.8698 0.0628
-8.250 -0.3189 0.01042 0.00489 -0.1508 0.8648 0.0668
-8.000 -0.2938 0.01016 0.00463 -0.1506 0.8603 0.0719
-7.750 -0.2666 0.00998 0.00441 -0.1507 0.8559 0.0765
-7.500 -0.2432 0.00974 0.00420 -0.1501 0.8518 0.0821
-7.250 -0.2180 0.00956 0.00401 -0.1497 0.8475 0.0871
-7.000 -0.1920 0.00935 0.00381 -0.1496 0.8432 0.0942
-6.750 -0.1646 0.00919 0.00363 -0.1497 0.8389 0.1012
-6.500 -0.1399 0.00901 0.00347 -0.1493 0.8350 0.1082
-6.250 -0.1147 0.00880 0.00330 -0.1489 0.8308 0.1182
-6.000 -0.0881 0.00864 0.00314 -0.1488 0.8270 0.1279
-5.750 -0.0605 0.00850 0.00299 -0.1490 0.8230 0.1382
-5.500 -0.0346 0.00831 0.00285 -0.1487 0.8195 0.1512
-5.250 -0.0089 0.00812 0.00271 -0.1484 0.8158 0.1650
-5.000 0.0173 0.00794 0.00257 -0.1482 0.8117 0.1812
-4.750 0.0441 0.00777 0.00243 -0.1482 0.8075 0.2024
-4.500 0.0706 0.00756 0.00230 -0.1481 0.8034 0.2295
-4.250 0.0958 0.00731 0.00218 -0.1478 0.7996 0.2635
-4.000 0.1217 0.00708 0.00207 -0.1476 0.7960 0.2993
-3.750 0.1484 0.00689 0.00197 -0.1475 0.7924 0.3349
-3.500 0.1762 0.00676 0.00189 -0.1476 0.7888 0.3658
-3.250 0.2032 0.00664 0.00185 -0.1476 0.7856 0.3953
-3.000 0.2299 0.00653 0.00182 -0.1474 0.7823 0.4184
-2.750 0.2571 0.00646 0.00180 -0.1472 0.7789 0.4384
-2.500 0.2850 0.00643 0.00178 -0.1472 0.7755 0.4549
-2.250 0.3138 0.00644 0.00177 -0.1474 0.7720 0.4685
-2.000 0.3416 0.00644 0.00178 -0.1474 0.7687 0.4821
-1.750 0.3685 0.00642 0.00181 -0.1472 0.7651 0.4949
-1.500 0.3959 0.00642 0.00182 -0.1470 0.7614 0.5040
-1.250 0.4240 0.00645 0.00183 -0.1470 0.7578 0.5128
-1.000 0.4532 0.00651 0.00185 -0.1473 0.7542 0.5192
-0.750 0.4807 0.00652 0.00189 -0.1472 0.7512 0.5255
-0.500 0.5079 0.00655 0.00192 -0.1470 0.7478 0.5326
-0.250 0.5350 0.00655 0.00194 -0.1468 0.7440 0.5393
0.000 0.5625 0.00659 0.00197 -0.1467 0.7398 0.5459
0.250 0.5904 0.00667 0.00200 -0.1466 0.7350 0.5513
0.500 0.6156 0.00664 0.00202 -0.1460 0.7300 0.5565
0.750 0.6422 0.00665 0.00205 -0.1457 0.7256 0.5612
1.000 0.6694 0.00672 0.00207 -0.1455 0.7201 0.5653
1.250 0.6933 0.00672 0.00209 -0.1445 0.7129 0.5686
1.500 0.7167 0.00676 0.00207 -0.1435 0.7029 0.5722
1.750 0.7406 0.00675 0.00211 -0.1426 0.6951 0.5771
2.000 0.7648 0.00680 0.00214 -0.1417 0.6876 0.5811
2.250 0.7906 0.00685 0.00219 -0.1413 0.6826 0.5844
2.500 0.8162 0.00689 0.00224 -0.1407 0.6769 0.5873
2.750 0.8401 0.00695 0.00228 -0.1399 0.6700 0.5904
3.000 0.8638 0.00697 0.00234 -0.1390 0.6621 0.5945
3.250 0.8858 0.00705 0.00240 -0.1377 0.6528 0.5982
3.500 0.9085 0.00710 0.00247 -0.1365 0.6443 0.6018
3.750 0.9269 0.00719 0.00252 -0.1344 0.6328 0.6051
4.000 0.9465 0.00727 0.00259 -0.1326 0.6207 0.6081
4.250 0.9658 0.00736 0.00269 -0.1308 0.6080 0.6124
4.500 0.9836 0.00751 0.00281 -0.1287 0.5928 0.6160
4.750 0.9989 0.00772 0.00297 -0.1261 0.5728 0.6193
5.000 1.0109 0.00803 0.00317 -0.1228 0.5480 0.6226
5.250 1.0182 0.00847 0.00346 -0.1186 0.5095 0.6257
5.500 1.0208 0.00906 0.00384 -0.1137 0.4656 0.6301
5.750 1.0247 0.00969 0.00428 -0.1092 0.4190 0.6344
6.000 1.0281 0.01040 0.00477 -0.1047 0.3732 0.6388
6.250 1.0347 0.01105 0.00524 -0.1009 0.3354 0.6433
6.500 1.0432 0.01164 0.00571 -0.0975 0.3020 0.6490
6.750 1.0521 0.01226 0.00620 -0.0943 0.2732 0.6547
7.000 1.0631 0.01284 0.00667 -0.0915 0.2466 0.6604
7.250 1.0734 0.01344 0.00718 -0.0886 0.2234 0.6670
7.500 1.0858 0.01398 0.00767 -0.0862 0.2038 0.6747
7.750 1.0986 0.01453 0.00817 -0.0838 0.1874 0.6832
8.000 1.1118 0.01507 0.00868 -0.0816 0.1727 0.6941
8.250 1.1243 0.01565 0.00924 -0.0793 0.1591 0.7072
8.500 1.1388 0.01614 0.00975 -0.0774 0.1492 0.7241
8.750 1.1526 0.01665 0.01029 -0.0753 0.1390 0.7474
9.000 1.1648 0.01718 0.01089 -0.0731 0.1297 0.7841
9.250 1.1776 0.01739 0.01143 -0.0707 0.1236 0.9055
9.500 1.2165 0.01808 0.01214 -0.0743 0.1139 1.0000
9.750 1.2320 0.01871 0.01275 -0.0728 0.1078 1.0000
10.000 1.2478 0.01935 0.01337 -0.0714 0.1016 1.0000
10.250 1.2633 0.02002 0.01402 -0.0700 0.0962 1.0000
10.500 1.2780 0.02075 0.01473 -0.0685 0.0904 1.0000
10.750 1.2940 0.02142 0.01539 -0.0672 0.0860 1.0000
11.000 1.3071 0.02226 0.01619 -0.0656 0.0802 1.0000
11.250 1.3230 0.02295 0.01691 -0.0644 0.0765 1.0000
11.500 1.3359 0.02385 0.01777 -0.0629 0.0718 1.0000
11.750 1.3506 0.02465 0.01859 -0.0616 0.0683 1.0000
12.000 1.3647 0.02550 0.01943 -0.0603 0.0645 1.0000
12.250 1.3767 0.02650 0.02042 -0.0589 0.0607 1.0000
12.500 1.3917 0.02732 0.02126 -0.0577 0.0579 1.0000
12.750 1.4033 0.02838 0.02230 -0.0563 0.0541 1.0000
13.000 1.4166 0.02935 0.02330 -0.0551 0.0518 1.0000
13.250 1.4293 0.03037 0.02432 -0.0539 0.0489 1.0000
13.500 1.4389 0.03163 0.02558 -0.0525 0.0459 1.0000
13.750 1.4525 0.03262 0.02660 -0.0514 0.0444 1.0000
14.000 1.4635 0.03382 0.02782 -0.0502 0.0423 1.0000
14.250 1.4722 0.03522 0.02922 -0.0489 0.0400 1.0000
14.500 1.4844 0.03637 0.03042 -0.0479 0.0387 1.0000
14.750 1.4954 0.03763 0.03172 -0.0469 0.0368 1.0000
15.000 1.5038 0.03910 0.03319 -0.0457 0.0351 1.0000
15.250 1.5120 0.04065 0.03478 -0.0445 0.0338 1.0000
15.500 1.5235 0.04191 0.03609 -0.0437 0.0326 1.0000
15.750 1.5321 0.04347 0.03769 -0.0427 0.0315 1.0000
16.000 1.5396 0.04514 0.03938 -0.0418 0.0303 1.0000
16.250 1.5449 0.04704 0.04133 -0.0407 0.0291 1.0000
16.500 1.5542 0.04859 0.04294 -0.0400 0.0283 1.0000
16.750 1.5616 0.05034 0.04474 -0.0392 0.0275 1.0000
17.000 1.5676 0.05226 0.04671 -0.0385 0.0267 1.0000
17.250 1.5715 0.05444 0.04891 -0.0377 0.0258 1.0000
17.500 1.5732 0.05688 0.05141 -0.0370 0.0249 1.0000
17.750 1.5783 0.05901 0.05362 -0.0365 0.0245 1.0000
18.000 1.5847 0.06101 0.05569 -0.0361 0.0238 1.0000
18.250 1.5880 0.06340 0.05814 -0.0357 0.0232 1.0000
18.500 1.5895 0.06603 0.06082 -0.0354 0.0226 1.0000
18.750 1.5904 0.06879 0.06365 -0.0352 0.0222 1.0000
19.000 1.5854 0.07233 0.06726 -0.0351 0.0214 1.0000
19.250 1.5838 0.07552 0.07054 -0.0352 0.0211 1.0000
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