FX 69-PR-281 (fx69pr281-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: FX 69-PR-281 (fx69pr281-il) Reynolds number: 1,000,000 Max Cl/Cd: 64.66 at α=4.75° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-fx69pr281-il-1000000.txt Download as CSV file: xf-fx69pr281-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: FX 69-PR-281
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
------ -------- --------- --------- -------- -------- --------
-19.750 -0.7236 0.11582 0.11248 -0.0701 1.0000 0.0748
-19.500 -0.7257 0.11296 0.10958 -0.0710 1.0000 0.0755
-19.250 -0.7195 0.11062 0.10725 -0.0722 0.9998 0.0765
-19.000 -0.7077 0.10759 0.10424 -0.0754 0.9992 0.0777
-18.750 -0.6988 0.10413 0.10077 -0.0788 0.9985 0.0788
-18.500 -0.6884 0.10080 0.09743 -0.0821 0.9975 0.0798
-18.250 -0.6811 0.09692 0.09349 -0.0860 0.9964 0.0810
-18.000 -0.6714 0.09345 0.09000 -0.0896 0.9952 0.0820
-17.750 -0.6584 0.09040 0.08697 -0.0931 0.9938 0.0833
-17.500 -0.6488 0.08682 0.08338 -0.0970 0.9924 0.0847
-17.250 -0.6428 0.08289 0.07942 -0.1010 0.9911 0.0860
-17.000 -0.6378 0.07963 0.07611 -0.1033 0.9886 0.0873
-16.750 -0.6344 0.07598 0.07247 -0.1065 0.9860 0.0888
-16.500 -0.6328 0.07194 0.06842 -0.1102 0.9833 0.0904
-16.250 -0.6283 0.06811 0.06456 -0.1140 0.9806 0.0922
-16.000 -0.6217 0.06437 0.06075 -0.1180 0.9781 0.0937
-15.750 -0.6300 0.06030 0.05667 -0.1205 0.9709 0.0955
-15.500 -0.6350 0.05587 0.05222 -0.1242 0.9639 0.0978
-15.250 -0.6370 0.05200 0.04828 -0.1274 0.9548 0.0996
-15.000 -0.6326 0.04754 0.04376 -0.1329 0.9476 0.1018
-14.750 -0.6246 0.04308 0.03924 -0.1394 0.9358 0.1044
-14.500 -0.6023 0.03968 0.03572 -0.1459 0.9193 0.1068
-14.250 -0.5934 0.03575 0.03163 -0.1521 0.8965 0.1093
-14.000 -0.5900 0.03259 0.02832 -0.1558 0.8719 0.1116
-13.750 -0.5792 0.03044 0.02603 -0.1583 0.8519 0.1136
-13.500 -0.5716 0.02809 0.02355 -0.1608 0.8351 0.1156
-13.000 -0.5429 0.02374 0.01904 -0.1672 0.8078 0.1201
-12.750 -0.5196 0.02251 0.01768 -0.1695 0.7934 0.1221
-12.500 -0.5110 0.02059 0.01570 -0.1711 0.7805 0.1242
-12.000 -0.4876 0.01804 0.01299 -0.1721 0.7517 0.1281
-11.750 -0.4751 0.01722 0.01205 -0.1717 0.7371 0.1297
-11.500 -0.4676 0.01618 0.01096 -0.1709 0.7268 0.1312
-11.250 -0.4741 0.01516 0.00987 -0.1680 0.7147 0.1327
-11.000 -0.4676 0.01468 0.00932 -0.1657 0.7039 0.1343
-10.750 -0.4509 0.01435 0.00895 -0.1643 0.6952 0.1362
-10.500 -0.4327 0.01413 0.00866 -0.1628 0.6852 0.1378
-10.250 -0.4133 0.01389 0.00836 -0.1615 0.6762 0.1394
-10.000 -0.3945 0.01354 0.00800 -0.1603 0.6673 0.1414
-9.750 -0.3752 0.01332 0.00773 -0.1589 0.6558 0.1433
-9.500 -0.3530 0.01313 0.00750 -0.1579 0.6457 0.1452
-9.250 -0.3294 0.01299 0.00730 -0.1570 0.6351 0.1469
-9.000 -0.3085 0.01285 0.00708 -0.1557 0.6227 0.1486
-8.750 -0.2851 0.01259 0.00682 -0.1549 0.6138 0.1509
-8.500 -0.2623 0.01244 0.00662 -0.1539 0.6034 0.1528
-8.250 -0.2384 0.01232 0.00645 -0.1530 0.5943 0.1548
-8.000 -0.2122 0.01221 0.00630 -0.1524 0.5868 0.1565
-7.750 -0.1879 0.01209 0.00613 -0.1515 0.5780 0.1583
-7.500 -0.1641 0.01194 0.00596 -0.1507 0.5691 0.1608
-7.250 -0.1372 0.01181 0.00582 -0.1502 0.5629 0.1630
-7.000 -0.1113 0.01173 0.00571 -0.1496 0.5549 0.1651
-6.750 -0.0869 0.01171 0.00561 -0.1486 0.5454 0.1669
-6.500 -0.0599 0.01156 0.00546 -0.1482 0.5397 0.1691
-6.250 -0.0332 0.01145 0.00534 -0.1477 0.5330 0.1715
-6.000 -0.0081 0.01139 0.00526 -0.1469 0.5255 0.1738
-5.750 0.0165 0.01137 0.00519 -0.1459 0.5179 0.1760
-5.500 0.0436 0.01132 0.00512 -0.1454 0.5129 0.1779
-5.250 0.0691 0.01121 0.00500 -0.1447 0.5067 0.1807
-5.000 0.0934 0.01117 0.00494 -0.1437 0.4996 0.1834
-4.750 0.1188 0.01116 0.00490 -0.1429 0.4931 0.1860
-4.500 0.1461 0.01114 0.00487 -0.1424 0.4884 0.1883
-4.250 0.1723 0.01115 0.00484 -0.1416 0.4826 0.1899
-4.000 0.1971 0.01108 0.00474 -0.1408 0.4757 0.1928
-3.750 0.2229 0.01105 0.00470 -0.1401 0.4692 0.1952
-3.500 0.2509 0.01100 0.00466 -0.1398 0.4642 0.1976
-3.250 0.2774 0.01101 0.00465 -0.1392 0.4573 0.1998
-3.000 0.3019 0.01107 0.00464 -0.1382 0.4494 0.2015
-2.750 0.3289 0.01110 0.00464 -0.1376 0.4433 0.2029
-2.500 0.3553 0.01104 0.00457 -0.1371 0.4349 0.2061
-2.250 0.3789 0.01110 0.00458 -0.1361 0.4251 0.2086
-2.000 0.4049 0.01112 0.00459 -0.1354 0.4171 0.2110
-1.750 0.4281 0.01123 0.00464 -0.1343 0.4078 0.2130
-1.500 0.4534 0.01131 0.00469 -0.1335 0.4001 0.2148
-1.250 0.4781 0.01143 0.00475 -0.1326 0.3915 0.2163
-1.000 0.5017 0.01155 0.00482 -0.1316 0.3829 0.2183
-0.750 0.5275 0.01159 0.00485 -0.1310 0.3756 0.2216
-0.500 0.5508 0.01173 0.00496 -0.1299 0.3675 0.2240
-0.250 0.5754 0.01184 0.00505 -0.1291 0.3615 0.2263
0.000 0.5995 0.01197 0.00516 -0.1282 0.3559 0.2284
0.250 0.6217 0.01216 0.00530 -0.1269 0.3498 0.2303
0.500 0.6448 0.01233 0.00543 -0.1259 0.3443 0.2319
0.750 0.6703 0.01241 0.00551 -0.1252 0.3401 0.2341
1.000 0.6943 0.01251 0.00561 -0.1244 0.3353 0.2376
1.250 0.7159 0.01270 0.00578 -0.1232 0.3302 0.2405
1.500 0.7384 0.01287 0.00595 -0.1221 0.3258 0.2431
1.750 0.7633 0.01299 0.00607 -0.1214 0.3227 0.2457
2.000 0.7867 0.01315 0.00622 -0.1204 0.3188 0.2478
2.250 0.8081 0.01338 0.00641 -0.1192 0.3146 0.2494
2.500 0.8276 0.01363 0.00664 -0.1178 0.3096 0.2536
2.750 0.8519 0.01375 0.00679 -0.1171 0.3072 0.2579
3.000 0.8754 0.01391 0.00697 -0.1162 0.3044 0.2616
3.250 0.8971 0.01413 0.00719 -0.1152 0.3015 0.2650
3.500 0.9171 0.01441 0.00745 -0.1139 0.2984 0.2677
3.750 0.9362 0.01472 0.00775 -0.1125 0.2949 0.2719
4.000 0.9559 0.01501 0.00806 -0.1112 0.2920 0.2778
4.250 0.9785 0.01521 0.00830 -0.1104 0.2904 0.2831
4.500 1.0002 0.01547 0.00857 -0.1094 0.2881 0.2877
4.750 1.0203 0.01578 0.00889 -0.1083 0.2856 0.2932
5.000 1.0392 0.01612 0.00926 -0.1070 0.2831 0.3012
5.250 1.0569 0.01654 0.00968 -0.1057 0.2804 0.3076
5.500 1.0715 0.01708 0.01021 -0.1039 0.2772 0.3121
5.750 1.0923 0.01740 0.01059 -0.1030 0.2757 0.3229
6.000 1.1138 0.01770 0.01095 -0.1022 0.2741 0.3320
6.250 1.1336 0.01809 0.01136 -0.1012 0.2721 0.3401
6.500 1.1515 0.01854 0.01186 -0.1001 0.2699 0.3514
6.750 1.1687 0.01906 0.01239 -0.0989 0.2677 0.3599
7.000 1.1837 0.01969 0.01302 -0.0975 0.2652 0.3662
7.250 1.1956 0.02046 0.01382 -0.0958 0.2623 0.3771
7.500 1.2149 0.02093 0.01434 -0.0949 0.2606 0.3865
7.750 1.2347 0.02139 0.01483 -0.0941 0.2590 0.3931
8.000 1.2522 0.02196 0.01547 -0.0932 0.2572 0.4066
8.250 1.2687 0.02260 0.01614 -0.0922 0.2551 0.4176
8.500 1.2843 0.02331 0.01686 -0.0911 0.2528 0.4267
8.750 1.2965 0.02420 0.01781 -0.0898 0.2505 0.4406
9.000 1.3059 0.02529 0.01890 -0.0883 0.2476 0.4512
9.250 1.3243 0.02590 0.01957 -0.0876 0.2461 0.4631
9.500 1.3416 0.02659 0.02033 -0.0868 0.2445 0.4776
9.750 1.3569 0.02742 0.02120 -0.0860 0.2425 0.4878
10.000 1.3718 0.02828 0.02211 -0.0851 0.2403 0.5012
10.250 1.3847 0.02929 0.02315 -0.0842 0.2381 0.5142
10.500 1.3927 0.03064 0.02453 -0.0830 0.2357 0.5253
10.750 1.4038 0.03181 0.02575 -0.0821 0.2334 0.5423
11.000 1.4201 0.03267 0.02669 -0.0815 0.2318 0.5596
11.250 1.4335 0.03376 0.02786 -0.0808 0.2299 0.5817
11.500 1.4467 0.03486 0.02903 -0.0802 0.2278 0.6066
11.750 1.4581 0.03610 0.03035 -0.0795 0.2257 0.6327
12.000 1.4642 0.03778 0.03211 -0.0786 0.2235 0.6613
12.250 1.4715 0.03936 0.03378 -0.0778 0.2211 0.7026
12.500 1.4853 0.04039 0.03502 -0.0772 0.2198 0.7644
12.750 1.4902 0.04140 0.03647 -0.0755 0.2182 1.0000
13.000 1.5014 0.04283 0.03792 -0.0751 0.2164 1.0000
13.250 1.5106 0.04446 0.03955 -0.0746 0.2144 1.0000
13.500 1.5147 0.04658 0.04167 -0.0742 0.2123 1.0000
13.750 1.5188 0.04866 0.04374 -0.0737 0.2099 1.0000
14.000 1.5271 0.05049 0.04560 -0.0734 0.2085 1.0000
14.250 1.5376 0.05212 0.04727 -0.0732 0.2071 1.0000
14.500 1.5481 0.05374 0.04892 -0.0731 0.2056 1.0000
14.750 1.5552 0.05574 0.05093 -0.0729 0.2040 1.0000
15.000 1.5592 0.05805 0.05326 -0.0728 0.2022 1.0000
15.250 1.5638 0.06031 0.05552 -0.0727 0.2003 1.0000
15.500 1.5629 0.06314 0.05835 -0.0727 0.1979 1.0000
15.750 1.5727 0.06499 0.06025 -0.0728 0.1969 1.0000
16.000 1.5824 0.06684 0.06214 -0.0729 0.1955 1.0000
16.250 1.5879 0.06916 0.06450 -0.0731 0.1940 1.0000
16.500 1.5930 0.07154 0.06691 -0.0734 0.1925 1.0000
16.750 1.5979 0.07394 0.06932 -0.0736 0.1908 1.0000
17.000 1.5967 0.07706 0.07246 -0.0740 0.1890 1.0000
17.250 1.6001 0.07963 0.07502 -0.0743 0.1869 1.0000
17.500 1.6083 0.08175 0.07719 -0.0748 0.1859 1.0000
17.750 1.6137 0.08421 0.07971 -0.0753 0.1845 1.0000
18.000 1.6169 0.08696 0.08250 -0.0759 0.1829 1.0000
18.250 1.6217 0.08948 0.08505 -0.0764 0.1813 1.0000
18.500 1.6233 0.09242 0.08800 -0.0771 0.1796 1.0000
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