FX 83-W-160 (fx83w160-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
|---|---|
|
Airfoil: FX 83-W-160 (fx83w160-il) Reynolds number: 1,000,000 Max Cl/Cd: 109.62 at α=3° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx83w160-il-1000000-n5.txt Download as CSV file: xf-fx83w160-il-1000000-n5.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 = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.250 -0.8625 0.10729 0.10427 -0.0747 1.0000 0.0148
-19.000 -0.8904 0.09959 0.09646 -0.0783 1.0000 0.0149
-18.750 -0.9199 0.09181 0.08857 -0.0819 1.0000 0.0149
-18.500 -0.9445 0.08381 0.08044 -0.0869 0.9997 0.0150
-18.250 -0.9630 0.07651 0.07300 -0.0920 0.9993 0.0149
-18.000 -0.9757 0.07023 0.06661 -0.0966 0.9987 0.0152
-17.750 -0.9849 0.06450 0.06077 -0.1010 0.9979 0.0153
-17.500 -0.9911 0.05933 0.05549 -0.1051 0.9969 0.0154
-17.250 -0.9931 0.05486 0.05093 -0.1088 0.9955 0.0156
-17.000 -0.9932 0.05099 0.04696 -0.1119 0.9938 0.0159
-16.750 -0.9922 0.04737 0.04326 -0.1147 0.9920 0.0161
-16.500 -0.9886 0.04415 0.03995 -0.1174 0.9901 0.0163
-16.250 -0.9810 0.04141 0.03713 -0.1200 0.9883 0.0165
-16.000 -0.9726 0.03869 0.03433 -0.1227 0.9867 0.0167
-15.750 -0.9649 0.03639 0.03195 -0.1245 0.9839 0.0169
-15.500 -0.9559 0.03422 0.02971 -0.1262 0.9803 0.0171
-15.250 -0.9459 0.03181 0.02723 -0.1286 0.9776 0.0174
-15.000 -0.9343 0.02974 0.02510 -0.1305 0.9742 0.0178
-14.750 -0.9224 0.02792 0.02324 -0.1320 0.9689 0.0182
-14.500 -0.9035 0.02619 0.02144 -0.1345 0.9658 0.0186
-14.250 -0.8849 0.02464 0.01983 -0.1366 0.9610 0.0189
-14.000 -0.8616 0.02330 0.01843 -0.1392 0.9561 0.0195
-13.750 -0.8331 0.02199 0.01704 -0.1426 0.9524 0.0200
-13.500 -0.8079 0.02083 0.01582 -0.1451 0.9461 0.0204
-13.250 -0.7778 0.01953 0.01446 -0.1489 0.9410 0.0211
-13.000 -0.7435 0.01843 0.01330 -0.1531 0.9366 0.0218
-12.750 -0.7176 0.01751 0.01233 -0.1552 0.9287 0.0226
-12.500 -0.6885 0.01668 0.01141 -0.1578 0.9222 0.0233
-12.250 -0.6708 0.01599 0.01064 -0.1578 0.9130 0.0239
-12.000 -0.6537 0.01537 0.00996 -0.1574 0.9050 0.0248
-11.750 -0.6380 0.01489 0.00943 -0.1562 0.8970 0.0257
-11.500 -0.6175 0.01446 0.00894 -0.1558 0.8905 0.0268
-11.250 -0.5989 0.01409 0.00853 -0.1548 0.8841 0.0277
-11.000 -0.5793 0.01371 0.00810 -0.1540 0.8774 0.0288
-10.750 -0.5588 0.01336 0.00771 -0.1533 0.8715 0.0302
-10.500 -0.5381 0.01304 0.00736 -0.1525 0.8656 0.0317
-10.250 -0.5165 0.01274 0.00701 -0.1518 0.8600 0.0332
-10.000 -0.4945 0.01242 0.00666 -0.1512 0.8551 0.0350
-9.750 -0.4721 0.01214 0.00636 -0.1505 0.8502 0.0366
-9.500 -0.4490 0.01190 0.00607 -0.1500 0.8449 0.0380
-9.250 -0.4261 0.01162 0.00576 -0.1494 0.8399 0.0401
-9.000 -0.4025 0.01137 0.00549 -0.1490 0.8355 0.0421
-8.750 -0.3786 0.01113 0.00522 -0.1485 0.8308 0.0443
-8.500 -0.3547 0.01088 0.00497 -0.1480 0.8260 0.0472
-8.250 -0.3301 0.01067 0.00473 -0.1477 0.8216 0.0503
-8.000 -0.3055 0.01043 0.00450 -0.1473 0.8177 0.0542
-7.750 -0.2803 0.01023 0.00429 -0.1470 0.8136 0.0577
-7.500 -0.2552 0.01003 0.00408 -0.1467 0.8095 0.0621
-7.250 -0.2295 0.00988 0.00390 -0.1465 0.8057 0.0655
-7.000 -0.2040 0.00966 0.00370 -0.1463 0.8022 0.0706
-6.750 -0.1779 0.00951 0.00354 -0.1461 0.7982 0.0746
-6.500 -0.1522 0.00932 0.00336 -0.1458 0.7940 0.0799
-6.250 -0.1264 0.00916 0.00320 -0.1456 0.7900 0.0868
-6.000 -0.1003 0.00899 0.00304 -0.1454 0.7866 0.0948
-5.750 -0.0738 0.00882 0.00290 -0.1453 0.7834 0.1025
-5.500 -0.0471 0.00868 0.00277 -0.1452 0.7798 0.1091
-5.250 -0.0207 0.00853 0.00264 -0.1450 0.7762 0.1169
-5.000 0.0060 0.00844 0.00252 -0.1449 0.7724 0.1235
-4.750 0.0324 0.00829 0.00240 -0.1447 0.7685 0.1332
-4.500 0.0591 0.00815 0.00230 -0.1446 0.7644 0.1435
-4.250 0.0855 0.00801 0.00219 -0.1444 0.7600 0.1573
-4.000 0.1119 0.00788 0.00208 -0.1442 0.7564 0.1728
-3.750 0.1383 0.00771 0.00198 -0.1441 0.7531 0.1939
-3.500 0.1652 0.00754 0.00188 -0.1440 0.7503 0.2185
-3.250 0.1920 0.00736 0.00180 -0.1440 0.7470 0.2436
-3.000 0.2187 0.00721 0.00172 -0.1438 0.7437 0.2713
-2.750 0.2455 0.00708 0.00165 -0.1437 0.7404 0.2951
-2.500 0.2722 0.00697 0.00160 -0.1436 0.7372 0.3204
-2.250 0.2995 0.00688 0.00156 -0.1435 0.7344 0.3420
-2.000 0.3265 0.00674 0.00152 -0.1435 0.7313 0.3691
-1.750 0.3533 0.00663 0.00150 -0.1433 0.7275 0.4007
-1.500 0.3800 0.00657 0.00149 -0.1431 0.7235 0.4222
-1.250 0.4067 0.00655 0.00149 -0.1429 0.7198 0.4408
-1.000 0.4343 0.00652 0.00150 -0.1428 0.7167 0.4545
-0.750 0.4620 0.00652 0.00151 -0.1428 0.7136 0.4649
-0.500 0.4892 0.00650 0.00153 -0.1426 0.7099 0.4776
-0.250 0.5160 0.00650 0.00156 -0.1424 0.7059 0.4912
0.000 0.5424 0.00654 0.00160 -0.1420 0.7015 0.5024
0.250 0.5692 0.00655 0.00164 -0.1417 0.6962 0.5122
0.500 0.5946 0.00659 0.00166 -0.1412 0.6891 0.5188
0.750 0.6203 0.00663 0.00170 -0.1407 0.6838 0.5246
1.000 0.6467 0.00666 0.00174 -0.1403 0.6781 0.5294
1.500 0.6912 0.00683 0.00180 -0.1378 0.6527 0.5363
1.750 0.7131 0.00691 0.00186 -0.1365 0.6381 0.5410
2.000 0.7328 0.00701 0.00191 -0.1347 0.6221 0.5452
2.250 0.7542 0.00709 0.00197 -0.1333 0.6115 0.5482
2.500 0.7754 0.00719 0.00203 -0.1318 0.6015 0.5508
2.750 0.7971 0.00729 0.00210 -0.1305 0.5893 0.5533
3.000 0.8156 0.00744 0.00221 -0.1285 0.5713 0.5568
3.250 0.8285 0.00773 0.00239 -0.1254 0.5421 0.5603
3.500 0.8422 0.00806 0.00259 -0.1226 0.5123 0.5636
3.750 0.8527 0.00849 0.00286 -0.1191 0.4744 0.5666
4.000 0.8637 0.00895 0.00315 -0.1158 0.4370 0.5691
4.250 0.8753 0.00941 0.00345 -0.1127 0.4032 0.5723
4.500 0.8844 0.00995 0.00382 -0.1091 0.3627 0.5754
4.750 0.8982 0.01036 0.00413 -0.1065 0.3357 0.5784
5.000 0.9112 0.01081 0.00446 -0.1038 0.3077 0.5812
5.250 0.9243 0.01127 0.00480 -0.1012 0.2808 0.5842
5.500 0.9378 0.01173 0.00516 -0.0987 0.2572 0.5873
5.750 0.9507 0.01223 0.00554 -0.0961 0.2311 0.5903
6.000 0.9634 0.01273 0.00595 -0.0935 0.2092 0.5941
6.250 0.9770 0.01322 0.00636 -0.0912 0.1877 0.5984
6.500 0.9920 0.01367 0.00676 -0.0891 0.1729 0.6027
6.750 1.0079 0.01411 0.00714 -0.0872 0.1611 0.6062
7.000 1.0256 0.01447 0.00750 -0.0856 0.1533 0.6099
7.250 1.0413 0.01491 0.00792 -0.0837 0.1443 0.6141
7.500 1.0586 0.01531 0.00832 -0.0821 0.1363 0.6186
7.750 1.0746 0.01577 0.00876 -0.0804 0.1286 0.6231
8.000 1.0907 0.01624 0.00921 -0.0787 0.1210 0.6276
8.250 1.1066 0.01672 0.00969 -0.0770 0.1133 0.6335
8.500 1.1229 0.01719 0.01017 -0.0754 0.1081 0.6398
8.750 1.1381 0.01773 0.01070 -0.0737 0.1007 0.6462
9.000 1.1534 0.01827 0.01124 -0.0720 0.0939 0.6544
9.500 1.1845 0.01936 0.01236 -0.0688 0.0839 0.6711
10.000 1.2148 0.02052 0.01358 -0.0657 0.0755 0.6940
10.250 1.2292 0.02115 0.01424 -0.0640 0.0715 0.7097
10.500 1.2441 0.02174 0.01490 -0.0625 0.0682 0.7291
10.750 1.2581 0.02237 0.01560 -0.0609 0.0644 0.7554
11.000 1.2705 0.02300 0.01635 -0.0590 0.0609 0.8031
11.500 1.3254 0.02450 0.01818 -0.0618 0.0525 1.0000
11.750 1.3406 0.02527 0.01896 -0.0607 0.0500 1.0000
12.000 1.3539 0.02619 0.01986 -0.0593 0.0470 1.0000
12.250 1.3681 0.02705 0.02074 -0.0581 0.0450 1.0000
12.500 1.3823 0.02793 0.02163 -0.0569 0.0428 1.0000
12.750 1.3943 0.02898 0.02268 -0.0556 0.0405 1.0000
13.000 1.4083 0.02991 0.02364 -0.0545 0.0390 1.0000
13.250 1.4214 0.03091 0.02466 -0.0533 0.0370 1.0000
13.500 1.4328 0.03204 0.02580 -0.0521 0.0349 1.0000
13.750 1.4456 0.03310 0.02688 -0.0510 0.0336 1.0000
14.000 1.4577 0.03423 0.02803 -0.0499 0.0321 1.0000
14.250 1.4691 0.03542 0.02924 -0.0488 0.0303 1.0000
14.500 1.4799 0.03668 0.03053 -0.0477 0.0291 1.0000
14.750 1.4910 0.03794 0.03182 -0.0467 0.0276 1.0000
15.000 1.5013 0.03925 0.03316 -0.0456 0.0263 1.0000
15.250 1.5108 0.04069 0.03462 -0.0446 0.0254 1.0000
15.500 1.5208 0.04208 0.03605 -0.0437 0.0243 1.0000
15.750 1.5300 0.04359 0.03760 -0.0428 0.0235 1.0000
16.000 1.5389 0.04513 0.03918 -0.0419 0.0227 1.0000
16.250 1.5463 0.04684 0.04092 -0.0410 0.0219 1.0000
16.500 1.5535 0.04857 0.04270 -0.0401 0.0212 1.0000
16.750 1.5612 0.05030 0.04448 -0.0394 0.0207 1.0000
17.000 1.5685 0.05210 0.04633 -0.0387 0.0202 1.0000
17.250 1.5746 0.05404 0.04833 -0.0380 0.0196 1.0000
17.500 1.5800 0.05608 0.05042 -0.0374 0.0190 1.0000
17.750 1.5844 0.05827 0.05266 -0.0368 0.0186 1.0000
18.000 1.5875 0.06059 0.05504 -0.0363 0.0180 1.0000
18.250 1.5914 0.06290 0.05742 -0.0359 0.0176 1.0000
18.500 1.5955 0.06523 0.05982 -0.0356 0.0172 1.0000
18.750 1.5985 0.06772 0.06238 -0.0354 0.0170 1.0000
19.000 1.6001 0.07043 0.06516 -0.0353 0.0164 1.0000
19.250 1.6011 0.07323 0.06804 -0.0352 0.0161 1.0000
|
Polar data table (+)
Polar graphs
<< Back to FX 83-W-160 (fx83w160-il)