GOE 459 AIRFOIL (goe459-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 459 AIRFOIL (goe459-il) Reynolds number: 1,000,000 Max Cl/Cd: 75.42 at α=9.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe459-il-1000000-n5.txt Download as CSV file: xf-goe459-il-1000000-n5.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 = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.500 -1.0567 0.12243 0.11951 -0.0134 1.0000 0.0060
-19.250 -1.1000 0.11053 0.10745 -0.0195 1.0000 0.0059
-19.000 -1.1400 0.09963 0.09638 -0.0251 1.0000 0.0058
-18.750 -1.1815 0.08878 0.08534 -0.0307 1.0000 0.0057
-18.500 -1.2124 0.07991 0.07632 -0.0352 1.0000 0.0057
-18.250 -1.2371 0.07233 0.06858 -0.0391 1.0000 0.0058
-18.000 -1.2578 0.06565 0.06176 -0.0424 1.0000 0.0057
-17.750 -1.2749 0.05985 0.05582 -0.0450 1.0000 0.0057
-17.500 -1.2888 0.05475 0.05059 -0.0472 1.0000 0.0058
-17.250 -1.2967 0.05066 0.04639 -0.0487 1.0000 0.0058
-17.000 -1.3036 0.04690 0.04251 -0.0498 1.0000 0.0059
-16.750 -1.3090 0.04350 0.03900 -0.0506 1.0000 0.0060
-16.500 -1.3116 0.04059 0.03599 -0.0510 1.0000 0.0060
-16.250 -1.3117 0.03809 0.03341 -0.0510 1.0000 0.0061
-16.000 -1.3116 0.03574 0.03096 -0.0508 1.0000 0.0063
-15.750 -1.3098 0.03368 0.02881 -0.0503 1.0000 0.0063
-15.500 -1.3058 0.03192 0.02697 -0.0496 1.0000 0.0065
-15.250 -1.3018 0.03027 0.02523 -0.0486 1.0000 0.0066
-15.000 -1.2971 0.02878 0.02366 -0.0473 1.0000 0.0067
-14.750 -1.2930 0.02733 0.02212 -0.0458 1.0000 0.0068
-14.500 -1.2889 0.02597 0.02069 -0.0440 1.0000 0.0070
-14.250 -1.2831 0.02482 0.01947 -0.0421 1.0000 0.0073
-14.000 -1.2768 0.02376 0.01835 -0.0400 1.0000 0.0075
-13.750 -1.2687 0.02289 0.01742 -0.0379 1.0000 0.0077
-13.500 -1.2605 0.02208 0.01655 -0.0356 1.0000 0.0078
-13.250 -1.2517 0.02135 0.01577 -0.0331 1.0000 0.0083
-13.000 -1.2427 0.02069 0.01505 -0.0305 1.0000 0.0083
-12.750 -1.2332 0.02012 0.01441 -0.0279 1.0000 0.0086
-12.500 -1.2234 0.01960 0.01385 -0.0251 1.0000 0.0089
-12.250 -1.2152 0.01907 0.01327 -0.0219 1.0000 0.0091
-12.000 -1.2090 0.01854 0.01270 -0.0183 1.0000 0.0096
-11.750 -1.2037 0.01807 0.01219 -0.0143 1.0000 0.0101
-11.500 -1.1952 0.01763 0.01170 -0.0108 1.0000 0.0105
-11.250 -1.1833 0.01717 0.01121 -0.0081 1.0000 0.0110
-11.000 -1.1703 0.01674 0.01074 -0.0055 1.0000 0.0117
-10.750 -1.1571 0.01632 0.01027 -0.0029 1.0000 0.0124
-10.500 -1.1445 0.01584 0.00977 -0.0001 1.0000 0.0135
-10.250 -1.1230 0.01536 0.00927 0.0007 0.9994 0.0150
-9.750 -1.0691 0.01418 0.00820 -0.0001 0.9965 0.0293
-9.500 -1.0398 0.01386 0.00793 -0.0008 0.9950 0.0343
-9.250 -1.0095 0.01361 0.00765 -0.0016 0.9938 0.0359
-9.000 -0.9829 0.01327 0.00732 -0.0017 0.9918 0.0378
-8.750 -0.9546 0.01298 0.00705 -0.0020 0.9897 0.0395
-8.500 -0.9250 0.01272 0.00679 -0.0026 0.9877 0.0413
-8.250 -0.8942 0.01250 0.00655 -0.0035 0.9861 0.0426
-8.000 -0.8621 0.01226 0.00629 -0.0046 0.9845 0.0434
-7.750 -0.8344 0.01204 0.00604 -0.0047 0.9810 0.0438
-7.500 -0.8061 0.01172 0.00570 -0.0050 0.9770 0.0451
-7.250 -0.7748 0.01139 0.00536 -0.0059 0.9739 0.0468
-7.000 -0.7494 0.01111 0.00508 -0.0055 0.9676 0.0482
-6.750 -0.7203 0.01083 0.00480 -0.0058 0.9622 0.0499
-6.500 -0.6914 0.01059 0.00455 -0.0061 0.9566 0.0512
-6.250 -0.6605 0.01035 0.00430 -0.0069 0.9508 0.0521
-6.000 -0.6244 0.01011 0.00404 -0.0088 0.9468 0.0529
-5.750 -0.5890 0.00989 0.00381 -0.0106 0.9409 0.0536
-5.500 -0.5491 0.00968 0.00358 -0.0133 0.9353 0.0542
-5.250 -0.5093 0.00942 0.00331 -0.0161 0.9279 0.0569
-5.000 -0.4707 0.00918 0.00307 -0.0185 0.9175 0.0605
-4.750 -0.4372 0.00898 0.00286 -0.0199 0.9046 0.0644
-4.500 -0.4082 0.00879 0.00266 -0.0202 0.8913 0.0732
-4.250 -0.3844 0.00846 0.00244 -0.0194 0.8772 0.1049
-4.000 -0.3608 0.00823 0.00228 -0.0186 0.8624 0.1322
-3.750 -0.3369 0.00808 0.00215 -0.0177 0.8471 0.1485
-3.500 -0.3135 0.00798 0.00202 -0.0167 0.8272 0.1607
-3.250 -0.2909 0.00788 0.00191 -0.0156 0.8064 0.1746
-3.000 -0.2687 0.00775 0.00179 -0.0143 0.7868 0.1950
-2.750 -0.2474 0.00755 0.00168 -0.0129 0.7690 0.2299
-2.500 -0.2248 0.00744 0.00160 -0.0118 0.7505 0.2543
-2.250 -0.2019 0.00735 0.00152 -0.0107 0.7324 0.2752
-2.000 -0.1787 0.00724 0.00145 -0.0097 0.7170 0.2986
-1.750 -0.1560 0.00716 0.00138 -0.0085 0.6976 0.3199
-1.500 -0.1336 0.00708 0.00131 -0.0073 0.6756 0.3439
-1.250 -0.1117 0.00695 0.00124 -0.0060 0.6538 0.3788
-1.000 -0.0902 0.00681 0.00119 -0.0047 0.6329 0.4230
-0.750 -0.0680 0.00676 0.00116 -0.0034 0.6064 0.4562
-0.500 -0.0456 0.00672 0.00115 -0.0022 0.5829 0.4864
-0.250 -0.0225 0.00667 0.00113 -0.0012 0.5642 0.5138
0.000 0.0001 0.00663 0.00112 0.0000 0.5432 0.5424
0.250 0.0229 0.00665 0.00113 0.0011 0.5183 0.5640
0.500 0.0456 0.00673 0.00115 0.0022 0.4846 0.5817
0.750 0.0684 0.00677 0.00116 0.0034 0.4566 0.6034
1.000 0.0904 0.00683 0.00119 0.0046 0.4221 0.6311
1.250 0.1117 0.00696 0.00124 0.0060 0.3783 0.6531
1.500 0.1337 0.00708 0.00131 0.0073 0.3444 0.6746
1.750 0.1558 0.00715 0.00138 0.0086 0.3198 0.6989
2.000 0.1787 0.00725 0.00145 0.0097 0.2976 0.7170
2.250 0.2021 0.00734 0.00152 0.0106 0.2757 0.7320
2.500 0.2249 0.00745 0.00160 0.0118 0.2538 0.7493
2.750 0.2475 0.00756 0.00168 0.0129 0.2293 0.7679
3.000 0.2685 0.00775 0.00180 0.0143 0.1947 0.7878
3.250 0.2907 0.00787 0.00191 0.0156 0.1746 0.8074
3.500 0.3135 0.00798 0.00203 0.0167 0.1605 0.8276
3.750 0.3369 0.00808 0.00215 0.0177 0.1482 0.8467
4.000 0.3608 0.00823 0.00228 0.0186 0.1319 0.8626
4.250 0.3846 0.00844 0.00243 0.0194 0.1062 0.8773
4.500 0.4084 0.00878 0.00266 0.0201 0.0736 0.8914
4.750 0.4373 0.00898 0.00285 0.0198 0.0648 0.9047
5.000 0.4704 0.00917 0.00306 0.0186 0.0609 0.9172
5.250 0.5092 0.00942 0.00331 0.0161 0.0569 0.9278
5.500 0.5490 0.00968 0.00358 0.0133 0.0544 0.9353
5.750 0.5890 0.00990 0.00381 0.0106 0.0537 0.9409
6.000 0.6244 0.01011 0.00404 0.0088 0.0530 0.9468
6.250 0.6606 0.01035 0.00430 0.0069 0.0521 0.9509
6.500 0.6913 0.01058 0.00455 0.0062 0.0513 0.9567
6.750 0.7204 0.01083 0.00482 0.0058 0.0502 0.9622
7.000 0.7495 0.01110 0.00508 0.0054 0.0484 0.9677
7.250 0.7750 0.01139 0.00536 0.0058 0.0465 0.9740
7.500 0.8062 0.01171 0.00569 0.0049 0.0452 0.9769
7.750 0.8345 0.01203 0.00604 0.0047 0.0439 0.9811
8.000 0.8623 0.01227 0.00629 0.0045 0.0434 0.9846
8.250 0.8944 0.01249 0.00654 0.0034 0.0426 0.9861
8.500 0.9252 0.01271 0.00677 0.0026 0.0411 0.9878
8.750 0.9546 0.01297 0.00704 0.0020 0.0394 0.9897
9.000 0.9829 0.01327 0.00732 0.0016 0.0374 0.9918
9.250 1.0097 0.01360 0.00764 0.0016 0.0359 0.9938
9.500 1.0400 0.01385 0.00792 0.0008 0.0341 0.9950
9.750 1.0695 0.01418 0.00820 0.0000 0.0292 0.9965
10.000 1.0962 0.01478 0.00869 -0.0003 0.0186 0.9981
10.250 1.1231 0.01537 0.00928 -0.0007 0.0149 0.9995
10.500 1.1444 0.01584 0.00977 0.0002 0.0135 1.0000
10.750 1.1573 0.01631 0.01026 0.0028 0.0124 1.0000
11.000 1.1704 0.01674 0.01073 0.0055 0.0116 1.0000
11.250 1.1836 0.01715 0.01119 0.0080 0.0111 1.0000
11.500 1.1958 0.01760 0.01168 0.0108 0.0106 1.0000
11.750 1.2043 0.01806 0.01217 0.0142 0.0102 1.0000
12.000 1.2096 0.01853 0.01268 0.0182 0.0096 1.0000
12.250 1.2156 0.01906 0.01326 0.0218 0.0091 1.0000
12.500 1.2241 0.01958 0.01382 0.0250 0.0089 1.0000
12.750 1.2334 0.02012 0.01442 0.0278 0.0086 1.0000
13.000 1.2429 0.02070 0.01506 0.0305 0.0084 1.0000
13.250 1.2525 0.02133 0.01575 0.0330 0.0081 1.0000
13.500 1.2607 0.02209 0.01657 0.0355 0.0079 1.0000
13.750 1.2695 0.02288 0.01740 0.0378 0.0077 1.0000
14.000 1.2768 0.02380 0.01839 0.0400 0.0075 1.0000
14.250 1.2837 0.02481 0.01946 0.0420 0.0072 1.0000
14.500 1.2904 0.02592 0.02063 0.0439 0.0072 1.0000
14.750 1.2933 0.02737 0.02216 0.0457 0.0068 1.0000
15.000 1.2970 0.02885 0.02374 0.0473 0.0067 1.0000
15.250 1.3029 0.03026 0.02522 0.0484 0.0066 1.0000
15.500 1.3075 0.03186 0.02690 0.0494 0.0065 1.0000
15.750 1.3102 0.03374 0.02887 0.0501 0.0064 1.0000
16.000 1.3129 0.03573 0.03095 0.0506 0.0064 1.0000
16.250 1.3125 0.03814 0.03346 0.0508 0.0062 1.0000
16.500 1.3107 0.04083 0.03625 0.0507 0.0061 1.0000
16.750 1.3101 0.04355 0.03906 0.0504 0.0060 1.0000
17.000 1.3059 0.04681 0.04242 0.0496 0.0059 1.0000
17.250 1.2978 0.05075 0.04648 0.0484 0.0058 1.0000
17.500 1.2910 0.05470 0.05053 0.0469 0.0058 1.0000
17.750 1.2800 0.05938 0.05533 0.0449 0.0057 1.0000
18.000 1.2610 0.06548 0.06158 0.0421 0.0057 1.0000
18.250 1.2406 0.07210 0.06834 0.0388 0.0056 1.0000
18.500 1.2202 0.07897 0.07534 0.0354 0.0056 1.0000
18.750 1.1841 0.08875 0.08530 0.0303 0.0057 1.0000
19.000 1.1494 0.09840 0.09512 0.0254 0.0057 1.0000
19.250 1.1040 0.11029 0.10719 0.0192 0.0058 1.0000
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