FX 76-MP-160 (fx76mp160-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: FX 76-MP-160 (fx76mp160-il) Reynolds number: 1,000,000 Max Cl/Cd: 152.53 at α=3° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-fx76mp160-il-1000000.txt Download as CSV file: xf-fx76mp160-il-1000000.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 = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-16.000 -0.4663 0.08011 0.07687 -0.1259 0.8261 0.0221
-15.750 -0.4946 0.07050 0.06710 -0.1342 0.8242 0.0220
-15.500 -0.5166 0.06155 0.05798 -0.1437 0.8221 0.0220
-15.250 -0.5270 0.05485 0.05116 -0.1510 0.8202 0.0219
-15.000 -0.5367 0.04870 0.04490 -0.1574 0.8186 0.0219
-14.750 -0.5428 0.04274 0.03880 -0.1643 0.8166 0.0218
-14.500 -0.5518 0.03587 0.03173 -0.1728 0.8143 0.0219
-14.250 -0.5509 0.03111 0.02682 -0.1792 0.8119 0.0220
-14.000 -0.5439 0.02806 0.02363 -0.1833 0.8095 0.0221
-13.750 -0.5359 0.02576 0.02121 -0.1857 0.8070 0.0220
-13.500 -0.5334 0.02342 0.01873 -0.1874 0.8040 0.0223
-13.250 -0.5287 0.02189 0.01711 -0.1873 0.8017 0.0224
-13.000 -0.5254 0.02085 0.01601 -0.1857 0.8002 0.0223
-12.750 -0.5225 0.01987 0.01496 -0.1838 0.7985 0.0224
-12.500 -0.5099 0.01908 0.01412 -0.1827 0.7967 0.0228
-12.250 -0.4943 0.01838 0.01337 -0.1818 0.7950 0.0232
-12.000 -0.4768 0.01771 0.01264 -0.1811 0.7933 0.0233
-11.750 -0.4575 0.01712 0.01198 -0.1805 0.7917 0.0235
-11.500 -0.4368 0.01658 0.01139 -0.1800 0.7901 0.0238
-11.250 -0.4154 0.01606 0.01080 -0.1795 0.7885 0.0240
-11.000 -0.3928 0.01559 0.01026 -0.1792 0.7867 0.0241
-10.750 -0.3692 0.01516 0.00975 -0.1790 0.7845 0.0243
-10.500 -0.3454 0.01474 0.00929 -0.1787 0.7829 0.0246
-10.250 -0.3215 0.01431 0.00881 -0.1784 0.7819 0.0248
-10.000 -0.2970 0.01391 0.00837 -0.1782 0.7807 0.0251
-9.750 -0.2718 0.01355 0.00797 -0.1780 0.7794 0.0253
-9.500 -0.2463 0.01319 0.00757 -0.1779 0.7781 0.0255
-9.250 -0.2207 0.01281 0.00715 -0.1778 0.7767 0.0260
-9.000 -0.1943 0.01250 0.00682 -0.1777 0.7752 0.0266
-8.750 -0.1674 0.01224 0.00655 -0.1777 0.7736 0.0272
-8.500 -0.1404 0.01198 0.00627 -0.1777 0.7718 0.0278
-8.250 -0.1131 0.01176 0.00601 -0.1777 0.7700 0.0286
-8.000 -0.0856 0.01155 0.00576 -0.1778 0.7680 0.0294
-7.750 -0.0575 0.01139 0.00559 -0.1780 0.7658 0.0307
-7.500 -0.0294 0.01127 0.00546 -0.1781 0.7640 0.0322
-7.250 -0.0016 0.01114 0.00532 -0.1781 0.7630 0.0339
-7.000 0.0255 0.01087 0.00505 -0.1781 0.7615 0.0355
-6.750 0.0531 0.01069 0.00487 -0.1781 0.7598 0.0374
-6.500 0.0813 0.01058 0.00472 -0.1782 0.7581 0.0389
-6.250 0.1088 0.01031 0.00444 -0.1783 0.7562 0.0407
-6.000 0.1368 0.01010 0.00422 -0.1784 0.7544 0.0424
-5.750 0.1651 0.00995 0.00404 -0.1785 0.7526 0.0438
-5.500 0.1933 0.00979 0.00385 -0.1786 0.7506 0.0451
-5.250 0.2217 0.00964 0.00369 -0.1788 0.7483 0.0468
-5.000 0.2508 0.00956 0.00360 -0.1791 0.7456 0.0487
-4.750 0.2791 0.00945 0.00351 -0.1793 0.7441 0.0509
-4.500 0.3071 0.00932 0.00342 -0.1793 0.7429 0.0536
-4.000 0.3635 0.00910 0.00323 -0.1795 0.7394 0.0600
-3.750 0.3919 0.00901 0.00314 -0.1795 0.7372 0.0631
-3.500 0.4201 0.00885 0.00299 -0.1796 0.7345 0.0667
-3.250 0.4485 0.00874 0.00286 -0.1797 0.7321 0.0698
-3.000 0.4770 0.00862 0.00274 -0.1798 0.7296 0.0741
-2.750 0.5058 0.00854 0.00267 -0.1801 0.7264 0.0818
-2.500 0.5336 0.00842 0.00262 -0.1801 0.7241 0.0958
-2.250 0.5612 0.00830 0.00254 -0.1800 0.7213 0.1042
-2.000 0.5892 0.00820 0.00246 -0.1801 0.7183 0.1110
-1.750 0.6170 0.00807 0.00240 -0.1801 0.7151 0.1242
-1.500 0.6450 0.00799 0.00233 -0.1801 0.7117 0.1410
-1.250 0.6733 0.00794 0.00227 -0.1802 0.7079 0.1499
-1.000 0.7011 0.00788 0.00225 -0.1802 0.7051 0.1587
-0.750 0.7286 0.00779 0.00225 -0.1802 0.7020 0.1765
-0.500 0.7563 0.00774 0.00223 -0.1802 0.6985 0.1923
-0.250 0.7837 0.00768 0.00218 -0.1801 0.6941 0.2015
0.000 0.8107 0.00765 0.00215 -0.1799 0.6890 0.2150
0.250 0.8377 0.00757 0.00216 -0.1798 0.6846 0.2423
0.500 0.8649 0.00752 0.00217 -0.1797 0.6796 0.2608
0.750 0.8916 0.00745 0.00218 -0.1795 0.6745 0.2953
1.000 0.9176 0.00744 0.00218 -0.1792 0.6690 0.3174
1.250 0.9445 0.00735 0.00222 -0.1791 0.6639 0.3621
1.500 0.9705 0.00730 0.00225 -0.1788 0.6575 0.3948
1.750 0.9949 0.00726 0.00229 -0.1782 0.6505 0.4481
2.000 1.0203 0.00711 0.00237 -0.1779 0.6441 0.5319
2.250 1.0434 0.00702 0.00247 -0.1770 0.6358 0.6327
2.500 1.0662 0.00704 0.00261 -0.1760 0.6264 0.6967
2.750 1.0880 0.00715 0.00274 -0.1747 0.6144 0.7220
3.000 1.1104 0.00728 0.00284 -0.1736 0.6015 0.7381
3.250 1.1302 0.00746 0.00297 -0.1720 0.5880 0.7467
3.500 1.1472 0.00769 0.00313 -0.1698 0.5739 0.7558
3.750 1.1654 0.00787 0.00329 -0.1679 0.5599 0.7644
4.000 1.1796 0.00807 0.00345 -0.1651 0.5457 0.7711
4.250 1.1915 0.00835 0.00367 -0.1619 0.5302 0.7769
4.750 1.2165 0.00897 0.00418 -0.1560 0.5029 0.7908
5.000 1.2292 0.00928 0.00445 -0.1531 0.4920 0.7974
5.250 1.2402 0.00965 0.00476 -0.1500 0.4765 0.8037
5.500 1.2524 0.00997 0.00507 -0.1472 0.4639 0.8090
5.750 1.2616 0.01040 0.00546 -0.1439 0.4519 0.8158
6.000 1.2715 0.01085 0.00588 -0.1408 0.4402 0.8211
6.250 1.2831 0.01127 0.00630 -0.1381 0.4298 0.8276
6.500 1.2897 0.01190 0.00687 -0.1347 0.4140 0.8355
6.750 1.2986 0.01251 0.00743 -0.1318 0.3990 0.8432
7.000 1.3086 0.01311 0.00801 -0.1291 0.3875 0.8509
7.250 1.3156 0.01387 0.00872 -0.1261 0.3749 0.8581
7.500 1.3314 0.01433 0.00921 -0.1245 0.3668 0.8639
7.750 1.3405 0.01508 0.00993 -0.1219 0.3538 0.8711
8.000 1.3548 0.01564 0.01051 -0.1202 0.3436 0.8829
8.250 1.3669 0.01636 0.01121 -0.1183 0.3329 0.8990
8.500 1.3964 0.01703 0.01194 -0.1200 0.3236 0.9317
8.750 1.4478 0.01786 0.01277 -0.1264 0.3124 0.9479
9.000 1.4656 0.01856 0.01346 -0.1256 0.3048 1.0000
9.250 1.4806 0.01948 0.01434 -0.1245 0.2960 1.0000
9.500 1.5005 0.02010 0.01497 -0.1241 0.2892 1.0000
9.750 1.5149 0.02106 0.01587 -0.1230 0.2779 1.0000
10.000 1.5312 0.02191 0.01670 -0.1221 0.2709 1.0000
10.250 1.5452 0.02288 0.01764 -0.1210 0.2635 1.0000
10.500 1.5612 0.02373 0.01849 -0.1202 0.2573 1.0000
10.750 1.5779 0.02455 0.01932 -0.1194 0.2515 1.0000
11.000 1.5907 0.02563 0.02038 -0.1182 0.2442 1.0000
11.250 1.6057 0.02654 0.02129 -0.1173 0.2372 1.0000
11.500 1.6205 0.02748 0.02221 -0.1163 0.2283 1.0000
11.750 1.6307 0.02875 0.02344 -0.1150 0.2194 1.0000
12.000 1.6435 0.02984 0.02452 -0.1139 0.2130 1.0000
12.250 1.6548 0.03103 0.02568 -0.1126 0.2064 1.0000
12.500 1.6685 0.03207 0.02675 -0.1117 0.2013 1.0000
12.750 1.6785 0.03337 0.02804 -0.1104 0.1932 1.0000
13.000 1.6879 0.03474 0.02938 -0.1091 0.1862 1.0000
13.250 1.7031 0.03568 0.03036 -0.1083 0.1816 1.0000
13.500 1.7110 0.03720 0.03186 -0.1070 0.1724 1.0000
13.750 1.7187 0.03872 0.03335 -0.1056 0.1645 1.0000
14.000 1.7256 0.04031 0.03491 -0.1043 0.1575 1.0000
14.250 1.7333 0.04191 0.03652 -0.1030 0.1517 1.0000
14.500 1.7423 0.04338 0.03801 -0.1019 0.1456 1.0000
14.750 1.7475 0.04517 0.03978 -0.1006 0.1389 1.0000
15.000 1.7555 0.04679 0.04143 -0.0995 0.1337 1.0000
15.250 1.7604 0.04863 0.04326 -0.0982 0.1258 1.0000
15.500 1.7627 0.05077 0.04537 -0.0969 0.1188 1.0000
15.750 1.7661 0.05282 0.04742 -0.0956 0.1142 1.0000
16.000 1.7681 0.05502 0.04962 -0.0944 0.1083 1.0000
16.250 1.7739 0.05692 0.05157 -0.0935 0.1051 1.0000
16.500 1.7770 0.05902 0.05369 -0.0923 0.1004 1.0000
16.750 1.7750 0.06168 0.05636 -0.0911 0.0951 1.0000
17.000 1.7800 0.06366 0.05839 -0.0902 0.0913 1.0000
17.250 1.7788 0.06630 0.06103 -0.0892 0.0856 1.0000
17.500 1.7763 0.06906 0.06380 -0.0881 0.0808 1.0000
17.750 1.7738 0.07187 0.06663 -0.0872 0.0775 1.0000
18.000 1.7706 0.07474 0.06952 -0.0862 0.0740 1.0000
18.250 1.7684 0.07761 0.07245 -0.0855 0.0713 1.0000
18.500 1.7696 0.08010 0.07500 -0.0849 0.0690 1.0000
18.750 1.7659 0.08320 0.07814 -0.0843 0.0662 1.0000
19.000 1.7596 0.08656 0.08154 -0.0837 0.0629 1.0000
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