GOE 459 AIRFOIL (goe459-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: GOE 459 AIRFOIL (goe459-il) Reynolds number: 1,000,000 Max Cl/Cd: 75.59 at α=10.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-goe459-il-1000000.txt Download as CSV file: xf-goe459-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: GOE 459 AIRFOIL
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
------ -------- --------- --------- -------- -------- --------
-18.250 -1.1544 0.08600 0.08258 -0.0319 1.0000 0.0098
-18.000 -1.1773 0.07854 0.07498 -0.0357 1.0000 0.0099
-17.750 -1.1963 0.07189 0.06820 -0.0390 1.0000 0.0099
-17.500 -1.2134 0.06576 0.06194 -0.0419 1.0000 0.0099
-17.250 -1.2240 0.06082 0.05688 -0.0442 1.0000 0.0100
-17.000 -1.2402 0.05532 0.05125 -0.0466 1.0000 0.0099
-16.750 -1.2503 0.05086 0.04667 -0.0483 1.0000 0.0100
-16.500 -1.2606 0.04660 0.04229 -0.0496 1.0000 0.0102
-16.250 -1.2713 0.04257 0.03812 -0.0506 1.0000 0.0102
-16.000 -1.2824 0.03878 0.03422 -0.0511 1.0000 0.0104
-15.750 -1.2890 0.03572 0.03104 -0.0509 1.0000 0.0106
-15.500 -1.2904 0.03336 0.02859 -0.0504 1.0000 0.0107
-15.250 -1.2907 0.03125 0.02639 -0.0495 1.0000 0.0109
-15.000 -1.2909 0.02931 0.02436 -0.0482 1.0000 0.0113
-14.750 -1.2870 0.02780 0.02278 -0.0467 1.0000 0.0115
-14.500 -1.2818 0.02650 0.02139 -0.0451 1.0000 0.0117
-14.250 -1.2770 0.02525 0.02006 -0.0432 1.0000 0.0119
-14.000 -1.2693 0.02426 0.01901 -0.0413 1.0000 0.0122
-13.750 -1.2630 0.02326 0.01792 -0.0390 1.0000 0.0125
-13.500 -1.2561 0.02237 0.01695 -0.0366 1.0000 0.0128
-13.250 -1.2522 0.02137 0.01588 -0.0336 1.0000 0.0132
-13.000 -1.2474 0.02050 0.01495 -0.0304 1.0000 0.0138
-12.750 -1.2413 0.01975 0.01416 -0.0272 1.0000 0.0145
-12.500 -1.2332 0.01917 0.01353 -0.0241 1.0000 0.0149
-12.250 -1.2260 0.01864 0.01292 -0.0207 1.0000 0.0155
-12.000 -1.2205 0.01813 0.01236 -0.0168 1.0000 0.0161
-11.750 -1.2174 0.01755 0.01176 -0.0124 1.0000 0.0172
-11.500 -1.2078 0.01703 0.01121 -0.0092 1.0000 0.0183
-11.250 -1.1976 0.01645 0.01062 -0.0062 1.0000 0.0206
-11.000 -1.1865 0.01591 0.01012 -0.0032 1.0000 0.0248
-10.750 -1.1720 0.01552 0.00979 -0.0009 1.0000 0.0307
-10.500 -1.1539 0.01534 0.00961 0.0009 1.0000 0.0340
-10.250 -1.1374 0.01507 0.00937 0.0030 1.0000 0.0367
-10.000 -1.1186 0.01493 0.00924 0.0046 1.0000 0.0388
-9.750 -1.0992 0.01483 0.00912 0.0062 1.0000 0.0403
-9.500 -1.0791 0.01479 0.00905 0.0077 1.0000 0.0411
-9.250 -1.0673 0.01431 0.00854 0.0106 1.0000 0.0428
-9.000 -1.0516 0.01405 0.00829 0.0128 1.0000 0.0443
-8.750 -1.0230 0.01383 0.00806 0.0124 0.9991 0.0457
-8.500 -0.9899 0.01363 0.00785 0.0110 0.9977 0.0472
-8.250 -0.9564 0.01344 0.00764 0.0096 0.9961 0.0483
-8.000 -0.9217 0.01330 0.00749 0.0080 0.9947 0.0492
-7.750 -0.8897 0.01285 0.00700 0.0068 0.9929 0.0504
-7.500 -0.8593 0.01237 0.00650 0.0059 0.9900 0.0527
-7.250 -0.8255 0.01203 0.00616 0.0045 0.9875 0.0543
-7.000 -0.7904 0.01173 0.00586 0.0027 0.9854 0.0559
-6.750 -0.7547 0.01148 0.00559 0.0009 0.9839 0.0577
-6.500 -0.7193 0.01124 0.00533 -0.0009 0.9828 0.0588
-6.250 -0.6937 0.01093 0.00501 -0.0005 0.9777 0.0598
-6.000 -0.6627 0.01056 0.00462 -0.0012 0.9748 0.0624
-5.750 -0.6297 0.01023 0.00430 -0.0025 0.9727 0.0652
-5.500 -0.5954 0.00995 0.00403 -0.0039 0.9711 0.0678
-5.250 -0.5681 0.00970 0.00377 -0.0038 0.9658 0.0705
-5.000 -0.5390 0.00930 0.00346 -0.0042 0.9615 0.0834
-4.750 -0.5095 0.00866 0.00311 -0.0048 0.9583 0.1375
-4.500 -0.4800 0.00831 0.00287 -0.0053 0.9531 0.1631
-4.250 -0.4491 0.00798 0.00266 -0.0060 0.9469 0.1870
-4.000 -0.4114 0.00761 0.00244 -0.0084 0.9431 0.2222
-3.750 -0.3791 0.00731 0.00226 -0.0095 0.9350 0.2565
-3.500 -0.3418 0.00700 0.00208 -0.0117 0.9278 0.2892
-3.250 -0.3087 0.00675 0.00190 -0.0129 0.9152 0.3190
-3.000 -0.2791 0.00646 0.00174 -0.0133 0.9003 0.3582
-2.750 -0.2542 0.00618 0.00161 -0.0127 0.8848 0.4103
-2.500 -0.2302 0.00599 0.00153 -0.0119 0.8694 0.4545
-2.250 -0.2063 0.00587 0.00146 -0.0109 0.8535 0.4860
-2.000 -0.1820 0.00579 0.00140 -0.0100 0.8371 0.5087
-1.750 -0.1585 0.00573 0.00134 -0.0089 0.8193 0.5290
-1.500 -0.1357 0.00566 0.00129 -0.0077 0.8005 0.5523
-1.250 -0.1128 0.00563 0.00125 -0.0065 0.7804 0.5725
-1.000 -0.0905 0.00558 0.00122 -0.0051 0.7606 0.5953
-0.750 -0.0679 0.00555 0.00120 -0.0038 0.7419 0.6196
-0.500 -0.0451 0.00553 0.00118 -0.0026 0.7242 0.6413
-0.250 -0.0227 0.00549 0.00118 -0.0013 0.7072 0.6682
0.000 0.0000 0.00548 0.00118 0.0000 0.6898 0.6895
0.250 0.0227 0.00550 0.00118 0.0013 0.6676 0.7071
0.500 0.0454 0.00552 0.00118 0.0025 0.6427 0.7239
0.750 0.0680 0.00555 0.00119 0.0038 0.6188 0.7409
1.000 0.0902 0.00559 0.00121 0.0052 0.5938 0.7607
1.250 0.1127 0.00563 0.00125 0.0065 0.5722 0.7810
1.500 0.1357 0.00567 0.00129 0.0077 0.5515 0.8004
1.750 0.1585 0.00572 0.00134 0.0089 0.5295 0.8196
2.000 0.1820 0.00579 0.00140 0.0100 0.5085 0.8373
2.250 0.2061 0.00587 0.00146 0.0110 0.4844 0.8536
2.500 0.2303 0.00599 0.00153 0.0118 0.4549 0.8687
2.750 0.2542 0.00618 0.00161 0.0127 0.4107 0.8843
3.000 0.2793 0.00646 0.00174 0.0133 0.3584 0.9007
3.250 0.3087 0.00675 0.00191 0.0129 0.3179 0.9153
3.500 0.3415 0.00700 0.00207 0.0117 0.2893 0.9277
3.750 0.3791 0.00731 0.00226 0.0095 0.2565 0.9350
4.000 0.4113 0.00761 0.00244 0.0084 0.2218 0.9431
4.250 0.4491 0.00798 0.00266 0.0060 0.1870 0.9469
4.500 0.4799 0.00831 0.00287 0.0053 0.1625 0.9531
4.750 0.5094 0.00868 0.00311 0.0048 0.1360 0.9583
5.000 0.5390 0.00931 0.00346 0.0042 0.0830 0.9615
5.250 0.5682 0.00970 0.00377 0.0038 0.0706 0.9658
5.500 0.5953 0.00994 0.00402 0.0040 0.0678 0.9711
5.750 0.6297 0.01024 0.00431 0.0025 0.0649 0.9727
6.000 0.6628 0.01056 0.00461 0.0012 0.0625 0.9748
6.250 0.6938 0.01093 0.00500 0.0004 0.0598 0.9777
6.500 0.7193 0.01123 0.00532 0.0009 0.0587 0.9828
6.750 0.7548 0.01147 0.00558 -0.0009 0.0577 0.9839
7.000 0.7905 0.01175 0.00588 -0.0027 0.0562 0.9855
7.250 0.8257 0.01203 0.00616 -0.0045 0.0544 0.9875
7.500 0.8594 0.01236 0.00650 -0.0059 0.0528 0.9900
7.750 0.8900 0.01282 0.00696 -0.0068 0.0508 0.9928
8.000 0.9218 0.01331 0.00751 -0.0080 0.0492 0.9947
8.250 0.9566 0.01344 0.00765 -0.0096 0.0484 0.9961
8.500 0.9901 0.01362 0.00784 -0.0111 0.0471 0.9977
8.750 1.0230 0.01383 0.00807 -0.0124 0.0457 0.9991
9.000 1.0516 0.01404 0.00828 -0.0128 0.0443 1.0000
9.250 1.0673 0.01430 0.00853 -0.0106 0.0430 1.0000
9.500 1.0791 0.01478 0.00904 -0.0077 0.0411 1.0000
9.750 1.0993 0.01483 0.00912 -0.0062 0.0403 1.0000
10.000 1.1190 0.01491 0.00921 -0.0047 0.0387 1.0000
10.250 1.1377 0.01505 0.00935 -0.0030 0.0366 1.0000
10.500 1.1542 0.01532 0.00959 -0.0010 0.0339 1.0000
10.750 1.1721 0.01552 0.00978 0.0009 0.0304 1.0000
11.000 1.1866 0.01590 0.01011 0.0032 0.0251 1.0000
11.250 1.1979 0.01644 0.01061 0.0061 0.0208 1.0000
11.500 1.2085 0.01699 0.01117 0.0091 0.0187 1.0000
11.750 1.2173 0.01757 0.01178 0.0124 0.0172 1.0000
12.000 1.2204 0.01814 0.01238 0.0168 0.0161 1.0000
12.250 1.2265 0.01863 0.01291 0.0206 0.0154 1.0000
12.500 1.2342 0.01914 0.01349 0.0240 0.0149 1.0000
12.750 1.2416 0.01975 0.01416 0.0272 0.0143 1.0000
13.000 1.2486 0.02045 0.01490 0.0302 0.0138 1.0000
13.250 1.2548 0.02125 0.01575 0.0332 0.0134 1.0000
13.500 1.2556 0.02242 0.01700 0.0366 0.0127 1.0000
13.750 1.2630 0.02329 0.01794 0.0390 0.0126 1.0000
14.000 1.2715 0.02416 0.01889 0.0410 0.0123 1.0000
14.250 1.2772 0.02527 0.02008 0.0431 0.0120 1.0000
14.500 1.2836 0.02642 0.02131 0.0449 0.0117 1.0000
14.750 1.2882 0.02776 0.02274 0.0466 0.0115 1.0000
15.000 1.2933 0.02917 0.02422 0.0479 0.0112 1.0000
15.250 1.2937 0.03106 0.02620 0.0492 0.0110 1.0000
15.500 1.2937 0.03314 0.02836 0.0502 0.0108 1.0000
15.750 1.2920 0.03551 0.03083 0.0507 0.0106 1.0000
16.000 1.2846 0.03866 0.03409 0.0509 0.0104 1.0000
16.250 1.2764 0.04213 0.03767 0.0505 0.0103 1.0000
16.500 1.2549 0.04746 0.04317 0.0491 0.0101 1.0000
16.750 1.2478 0.05136 0.04718 0.0478 0.0100 1.0000
17.000 1.2386 0.05572 0.05166 0.0461 0.0100 1.0000
17.250 1.2363 0.05932 0.05535 0.0446 0.0099 1.0000
17.500 1.2188 0.06521 0.06138 0.0419 0.0099 1.0000
17.750 1.1989 0.07176 0.06807 0.0387 0.0099 1.0000
18.000 1.1840 0.07778 0.07421 0.0357 0.0098 1.0000
18.250 1.1626 0.08500 0.08156 0.0321 0.0098 1.0000
18.500 1.1356 0.09321 0.08991 0.0280 0.0098 1.0000
18.750 1.1118 0.10105 0.09786 0.0241 0.0098 1.0000
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