FX 76-MP-160 (fx76mp160-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: FX 76-MP-160 (fx76mp160-il) Reynolds number: 1,000,000 Max Cl/Cd: 110.62 at α=2.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx76mp160-il-1000000-n5.txt Download as CSV file: xf-fx76mp160-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: FX 76-MP-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
------ -------- --------- --------- -------- -------- --------
-16.750 -0.4095 0.10466 0.10135 -0.1076 0.7983 0.0173
-16.500 -0.4303 0.09688 0.09349 -0.1124 0.7971 0.0173
-16.250 -0.4507 0.08935 0.08587 -0.1174 0.7957 0.0174
-16.000 -0.4735 0.08140 0.07782 -0.1230 0.7942 0.0175
-15.750 -0.4908 0.07449 0.07082 -0.1284 0.7925 0.0174
-15.500 -0.5185 0.06599 0.06220 -0.1357 0.7910 0.0175
-15.250 -0.5449 0.05712 0.05320 -0.1445 0.7894 0.0174
-15.000 -0.5808 0.04648 0.04238 -0.1553 0.7874 0.0173
-14.750 -0.6035 0.03640 0.03204 -0.1670 0.7851 0.0172
-14.500 -0.6056 0.03034 0.02578 -0.1753 0.7829 0.0173
-14.250 -0.5994 0.02734 0.02267 -0.1791 0.7813 0.0173
-14.000 -0.5914 0.02521 0.02044 -0.1811 0.7795 0.0174
-13.750 -0.5855 0.02334 0.01848 -0.1821 0.7776 0.0174
-13.500 -0.5786 0.02197 0.01702 -0.1820 0.7756 0.0175
-13.250 -0.5754 0.02091 0.01588 -0.1806 0.7735 0.0176
-13.000 -0.5644 0.02003 0.01492 -0.1797 0.7718 0.0176
-12.750 -0.5489 0.01931 0.01412 -0.1790 0.7701 0.0177
-12.500 -0.5302 0.01875 0.01350 -0.1785 0.7685 0.0179
-12.250 -0.5104 0.01822 0.01289 -0.1780 0.7669 0.0181
-12.000 -0.4905 0.01766 0.01225 -0.1775 0.7651 0.0181
-11.750 -0.4692 0.01713 0.01167 -0.1772 0.7639 0.0182
-11.500 -0.4481 0.01657 0.01106 -0.1768 0.7629 0.0183
-11.250 -0.4269 0.01596 0.01039 -0.1764 0.7619 0.0185
-11.000 -0.4041 0.01544 0.00982 -0.1761 0.7607 0.0186
-10.750 -0.3808 0.01494 0.00927 -0.1758 0.7594 0.0187
-10.500 -0.3569 0.01447 0.00875 -0.1756 0.7580 0.0189
-10.250 -0.3322 0.01405 0.00830 -0.1755 0.7565 0.0191
-10.000 -0.3072 0.01365 0.00784 -0.1754 0.7550 0.0193
-9.750 -0.2816 0.01328 0.00743 -0.1753 0.7535 0.0195
-9.500 -0.2556 0.01295 0.00706 -0.1752 0.7521 0.0196
-9.250 -0.2293 0.01263 0.00670 -0.1752 0.7508 0.0198
-9.000 -0.2028 0.01233 0.00637 -0.1752 0.7494 0.0200
-8.750 -0.1759 0.01206 0.00605 -0.1752 0.7478 0.0202
-8.500 -0.1488 0.01182 0.00576 -0.1753 0.7458 0.0204
-8.250 -0.1215 0.01157 0.00548 -0.1753 0.7442 0.0206
-8.000 -0.0943 0.01132 0.00521 -0.1753 0.7428 0.0208
-7.750 -0.0669 0.01108 0.00496 -0.1754 0.7411 0.0211
-7.500 -0.0392 0.01087 0.00473 -0.1755 0.7396 0.0213
-7.250 -0.0113 0.01066 0.00451 -0.1756 0.7381 0.0217
-7.000 0.0166 0.01047 0.00431 -0.1757 0.7364 0.0222
-6.750 0.0444 0.01026 0.00410 -0.1758 0.7343 0.0235
-6.500 0.0721 0.01006 0.00392 -0.1758 0.7319 0.0251
-6.250 0.1000 0.00990 0.00378 -0.1759 0.7297 0.0299
-6.000 0.1282 0.00979 0.00365 -0.1760 0.7277 0.0327
-5.750 0.1565 0.00971 0.00354 -0.1761 0.7256 0.0340
-5.500 0.1848 0.00956 0.00340 -0.1762 0.7239 0.0351
-5.250 0.2131 0.00942 0.00326 -0.1763 0.7217 0.0363
-5.000 0.2415 0.00930 0.00314 -0.1765 0.7192 0.0376
-4.750 0.2700 0.00920 0.00303 -0.1766 0.7171 0.0386
-4.500 0.2984 0.00910 0.00292 -0.1767 0.7151 0.0393
-4.250 0.3267 0.00898 0.00279 -0.1769 0.7131 0.0402
-4.000 0.3548 0.00887 0.00267 -0.1769 0.7108 0.0412
-3.750 0.3828 0.00877 0.00256 -0.1770 0.7081 0.0422
-3.500 0.4110 0.00868 0.00247 -0.1771 0.7053 0.0430
-3.250 0.4395 0.00859 0.00239 -0.1772 0.7022 0.0439
-3.000 0.4676 0.00851 0.00231 -0.1773 0.6986 0.0453
-2.750 0.4954 0.00841 0.00224 -0.1773 0.6947 0.0486
-2.500 0.5228 0.00833 0.00217 -0.1772 0.6905 0.0578
-2.250 0.5505 0.00829 0.00213 -0.1772 0.6864 0.0624
-2.000 0.5787 0.00822 0.00208 -0.1773 0.6821 0.0659
-1.750 0.6063 0.00817 0.00203 -0.1772 0.6766 0.0695
-1.500 0.6330 0.00813 0.00198 -0.1770 0.6705 0.0740
-1.250 0.6605 0.00807 0.00195 -0.1769 0.6649 0.0802
-1.000 0.6877 0.00801 0.00194 -0.1768 0.6588 0.0976
-0.750 0.7141 0.00801 0.00192 -0.1765 0.6525 0.1042
-0.500 0.7410 0.00801 0.00191 -0.1764 0.6470 0.1087
-0.250 0.7671 0.00802 0.00192 -0.1760 0.6385 0.1138
0.000 0.7919 0.00804 0.00195 -0.1755 0.6295 0.1251
0.250 0.8173 0.00808 0.00198 -0.1750 0.6177 0.1391
0.500 0.8415 0.00815 0.00202 -0.1743 0.6056 0.1448
0.750 0.8647 0.00826 0.00208 -0.1734 0.5925 0.1497
1.000 0.8880 0.00836 0.00215 -0.1725 0.5800 0.1545
1.250 0.9108 0.00846 0.00223 -0.1715 0.5690 0.1638
1.500 0.9327 0.00856 0.00234 -0.1704 0.5563 0.1850
1.750 0.9548 0.00870 0.00244 -0.1693 0.5425 0.1925
2.000 0.9746 0.00887 0.00257 -0.1678 0.5285 0.2002
2.500 1.0111 0.00914 0.00285 -0.1641 0.5042 0.2485
3.000 1.0414 0.00944 0.00319 -0.1592 0.4766 0.3117
3.250 1.0569 0.00969 0.00340 -0.1569 0.4620 0.3229
3.500 1.0715 0.00991 0.00365 -0.1545 0.4501 0.3593
3.750 1.0864 0.01016 0.00390 -0.1521 0.4393 0.3817
4.000 1.1023 0.01033 0.00415 -0.1500 0.4302 0.4332
4.250 1.1141 0.01061 0.00448 -0.1472 0.4154 0.4732
4.500 1.1286 0.01086 0.00478 -0.1449 0.4039 0.5173
4.750 1.1394 0.01118 0.00518 -0.1420 0.3917 0.5769
5.000 1.1531 0.01143 0.00557 -0.1397 0.3838 0.6439
5.250 1.1636 0.01188 0.00605 -0.1368 0.3726 0.6872
5.500 1.1787 0.01225 0.00645 -0.1348 0.3634 0.7029
5.750 1.1904 0.01274 0.00697 -0.1323 0.3542 0.7324
6.000 1.2053 0.01321 0.00741 -0.1304 0.3438 0.7420
6.250 1.2170 0.01379 0.00797 -0.1281 0.3331 0.7540
6.500 1.2283 0.01443 0.00858 -0.1257 0.3221 0.7626
6.750 1.2410 0.01503 0.00917 -0.1236 0.3128 0.7707
7.000 1.2561 0.01555 0.00970 -0.1219 0.3050 0.7820
7.250 1.2672 0.01629 0.01039 -0.1197 0.2931 0.7899
7.500 1.2808 0.01693 0.01101 -0.1180 0.2815 0.7963
7.750 1.2910 0.01777 0.01177 -0.1158 0.2688 0.8003
8.000 1.3043 0.01848 0.01245 -0.1141 0.2611 0.8040
8.250 1.3197 0.01908 0.01307 -0.1127 0.2557 0.8071
8.500 1.3360 0.01965 0.01365 -0.1114 0.2511 0.8113
8.750 1.3499 0.02035 0.01435 -0.1098 0.2441 0.8163
9.000 1.3643 0.02104 0.01506 -0.1084 0.2394 0.8220
9.250 1.3808 0.02164 0.01569 -0.1073 0.2343 0.8267
9.750 1.4079 0.02319 0.01722 -0.1044 0.2191 0.8456
10.000 1.4220 0.02397 0.01802 -0.1031 0.2141 0.8514
10.250 1.4363 0.02475 0.01883 -0.1019 0.2093 0.8613
10.500 1.4530 0.02553 0.01968 -0.1011 0.2038 0.8896
10.750 1.4974 0.02644 0.02069 -0.1062 0.1984 0.9192
11.000 1.5528 0.02781 0.02208 -0.1141 0.1900 0.9913
11.250 1.5694 0.02894 0.02320 -0.1136 0.1837 1.0000
11.500 1.5811 0.03012 0.02434 -0.1124 0.1722 1.0000
11.750 1.5926 0.03131 0.02549 -0.1112 0.1644 1.0000
12.000 1.6022 0.03266 0.02680 -0.1098 0.1570 1.0000
12.250 1.6146 0.03382 0.02797 -0.1088 0.1520 1.0000
12.500 1.6281 0.03491 0.02908 -0.1079 0.1473 1.0000
12.750 1.6347 0.03652 0.03064 -0.1064 0.1376 1.0000
13.000 1.6460 0.03781 0.03195 -0.1054 0.1317 1.0000
13.250 1.6528 0.03942 0.03351 -0.1040 0.1223 1.0000
13.500 1.6621 0.04087 0.03495 -0.1028 0.1175 1.0000
13.750 1.6670 0.04272 0.03678 -0.1014 0.1107 1.0000
14.000 1.6777 0.04408 0.03817 -0.1004 0.1074 1.0000
14.250 1.6869 0.04560 0.03970 -0.0994 0.1029 1.0000
14.500 1.6906 0.04759 0.04169 -0.0981 0.0970 1.0000
14.750 1.6988 0.04919 0.04331 -0.0971 0.0930 1.0000
15.000 1.7040 0.05112 0.04524 -0.0959 0.0869 1.0000
15.250 1.7059 0.05333 0.04744 -0.0946 0.0809 1.0000
15.500 1.7097 0.05542 0.04953 -0.0935 0.0767 1.0000
15.750 1.7129 0.05757 0.05171 -0.0924 0.0737 1.0000
16.000 1.7183 0.05950 0.05366 -0.0915 0.0708 1.0000
16.250 1.7226 0.06162 0.05584 -0.0906 0.0684 1.0000
16.500 1.7246 0.06393 0.05817 -0.0896 0.0650 1.0000
17.000 1.7275 0.06878 0.06309 -0.0878 0.0586 1.0000
17.500 1.7174 0.07499 0.06931 -0.0858 0.0476 1.0000
17.750 1.7122 0.07822 0.07257 -0.0850 0.0444 1.0000
18.000 1.7118 0.08095 0.07534 -0.0844 0.0425 1.0000
18.250 1.7084 0.08410 0.07855 -0.0839 0.0409 1.0000
18.500 1.7028 0.08749 0.08198 -0.0834 0.0389 1.0000
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