GOE 604 AIRFOIL (goe604-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: GOE 604 AIRFOIL (goe604-il) Reynolds number: 1,000,000 Max Cl/Cd: 112.97 at α=7° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-goe604-il-1000000.txt Download as CSV file: xf-goe604-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: GOE 604 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
------ -------- --------- --------- -------- -------- --------
-19.000 -0.6750 0.12238 0.12006 -0.0473 1.0000 0.0202
-18.750 -0.7020 0.11355 0.11113 -0.0524 1.0000 0.0206
-18.500 -0.7304 0.10487 0.10233 -0.0575 1.0000 0.0207
-18.250 -0.7540 0.09724 0.09460 -0.0620 1.0000 0.0209
-18.000 -0.7756 0.09013 0.08738 -0.0663 1.0000 0.0210
-17.750 -0.7965 0.08333 0.08048 -0.0703 1.0000 0.0212
-17.500 -0.8173 0.07678 0.07384 -0.0743 1.0000 0.0213
-17.250 -0.8416 0.07020 0.06715 -0.0783 1.0000 0.0214
-17.000 -0.8663 0.06358 0.06042 -0.0824 1.0000 0.0216
-16.750 -0.8877 0.05748 0.05421 -0.0861 1.0000 0.0217
-16.500 -0.9084 0.05151 0.04813 -0.0898 1.0000 0.0217
-16.250 -0.9256 0.04585 0.04234 -0.0935 1.0000 0.0218
-16.000 -0.9386 0.04058 0.03695 -0.0972 1.0000 0.0219
-15.750 -0.9462 0.03629 0.03253 -0.1003 1.0000 0.0220
-15.500 -0.9509 0.03302 0.02915 -0.1020 1.0000 0.0221
-15.250 -0.9693 0.02964 0.02566 -0.1022 1.0000 0.0223
-15.000 -0.9886 0.02754 0.02349 -0.0994 1.0000 0.0225
-14.750 -0.9860 0.02593 0.02181 -0.0987 0.9986 0.0228
-14.500 -0.9619 0.02470 0.02054 -0.1005 0.9948 0.0231
-14.250 -0.9396 0.02374 0.01954 -0.1012 0.9892 0.0235
-14.000 -0.9139 0.02285 0.01859 -0.1022 0.9840 0.0240
-13.750 -0.8857 0.02205 0.01774 -0.1034 0.9804 0.0244
-13.500 -0.8619 0.02128 0.01690 -0.1036 0.9731 0.0249
-13.250 -0.8274 0.02060 0.01614 -0.1056 0.9693 0.0254
-13.000 -0.7963 0.01974 0.01519 -0.1072 0.9629 0.0259
-12.750 -0.7653 0.01866 0.01408 -0.1091 0.9539 0.0265
-12.500 -0.7367 0.01808 0.01346 -0.1098 0.9418 0.0270
-12.250 -0.7114 0.01760 0.01291 -0.1096 0.9275 0.0275
-12.000 -0.6892 0.01720 0.01242 -0.1088 0.9112 0.0280
-11.750 -0.6697 0.01679 0.01191 -0.1073 0.8921 0.0285
-11.500 -0.6501 0.01648 0.01147 -0.1058 0.8698 0.0289
-11.250 -0.6304 0.01625 0.01109 -0.1041 0.8441 0.0293
-11.000 -0.6163 0.01573 0.01042 -0.1018 0.8136 0.0299
-10.750 -0.6004 0.01533 0.00988 -0.0996 0.7814 0.0305
-10.500 -0.5819 0.01510 0.00951 -0.0978 0.7491 0.0310
-10.250 -0.5621 0.01490 0.00917 -0.0962 0.7197 0.0316
-10.000 -0.5414 0.01468 0.00883 -0.0947 0.6954 0.0321
-9.750 -0.5195 0.01447 0.00850 -0.0935 0.6756 0.0327
-9.500 -0.4967 0.01429 0.00820 -0.0924 0.6590 0.0333
-9.000 -0.4539 0.01356 0.00731 -0.0899 0.6324 0.0348
-8.750 -0.4306 0.01331 0.00701 -0.0890 0.6216 0.0355
-8.500 -0.4064 0.01310 0.00674 -0.0881 0.6114 0.0362
-8.250 -0.3819 0.01291 0.00648 -0.0873 0.6019 0.0371
-8.000 -0.3569 0.01274 0.00624 -0.0866 0.5925 0.0378
-7.750 -0.3328 0.01248 0.00591 -0.0857 0.5844 0.0386
-7.500 -0.3090 0.01215 0.00555 -0.0848 0.5770 0.0397
-7.250 -0.2843 0.01197 0.00531 -0.0840 0.5695 0.0407
-7.000 -0.2582 0.01178 0.00510 -0.0835 0.5637 0.0419
-6.750 -0.2321 0.01164 0.00491 -0.0829 0.5574 0.0429
-6.500 -0.2076 0.01141 0.00462 -0.0821 0.5511 0.0443
-6.250 -0.1817 0.01118 0.00439 -0.0816 0.5464 0.0458
-6.000 -0.1554 0.01103 0.00420 -0.0810 0.5408 0.0475
-5.750 -0.1293 0.01093 0.00404 -0.0805 0.5349 0.0490
-5.500 -0.1038 0.01070 0.00381 -0.0798 0.5300 0.0519
-5.250 -0.0770 0.01055 0.00365 -0.0794 0.5253 0.0546
-5.000 -0.0512 0.01037 0.00346 -0.0788 0.5204 0.0585
-4.750 -0.0254 0.01024 0.00330 -0.0782 0.5152 0.0632
-4.500 0.0008 0.01004 0.00313 -0.0777 0.5111 0.0710
-4.250 0.0263 0.00979 0.00295 -0.0771 0.5065 0.0870
-4.000 0.0509 0.00952 0.00283 -0.0764 0.5014 0.1239
-3.750 0.0770 0.00946 0.00279 -0.0759 0.4960 0.1395
-3.500 0.1047 0.00939 0.00274 -0.0756 0.4923 0.1489
-3.250 0.1319 0.00932 0.00268 -0.0753 0.4878 0.1565
-3.000 0.1588 0.00929 0.00263 -0.0749 0.4830 0.1631
-2.750 0.1855 0.00929 0.00259 -0.0745 0.4779 0.1686
-2.500 0.2129 0.00921 0.00254 -0.0742 0.4741 0.1761
-2.250 0.2402 0.00918 0.00249 -0.0739 0.4694 0.1814
-2.000 0.2666 0.00914 0.00245 -0.0735 0.4644 0.1901
-1.750 0.2932 0.00912 0.00243 -0.0731 0.4593 0.1995
-1.500 0.3201 0.00904 0.00240 -0.0727 0.4546 0.2141
-1.250 0.3463 0.00898 0.00238 -0.0723 0.4493 0.2348
-1.000 0.3715 0.00893 0.00239 -0.0716 0.4435 0.2627
-0.750 0.3980 0.00883 0.00238 -0.0713 0.4394 0.2940
-0.500 0.4241 0.00876 0.00239 -0.0708 0.4342 0.3230
-0.250 0.4496 0.00875 0.00240 -0.0702 0.4284 0.3472
0.000 0.4757 0.00871 0.00242 -0.0698 0.4235 0.3725
0.250 0.5016 0.00865 0.00244 -0.0693 0.4182 0.4028
0.500 0.5262 0.00862 0.00247 -0.0686 0.4123 0.4398
0.750 0.5505 0.00853 0.00251 -0.0678 0.4071 0.4899
1.000 0.5738 0.00839 0.00255 -0.0669 0.4009 0.5599
1.250 0.5943 0.00827 0.00262 -0.0654 0.3936 0.6433
1.500 0.6141 0.00806 0.00269 -0.0636 0.3882 0.7360
1.750 0.6327 0.00790 0.00279 -0.0615 0.3824 0.8262
2.000 0.6596 0.00789 0.00295 -0.0611 0.3759 0.9065
2.250 0.7160 0.00805 0.00313 -0.0670 0.3701 0.9507
2.500 0.7638 0.00826 0.00328 -0.0713 0.3639 0.9644
2.750 0.8042 0.00846 0.00342 -0.0740 0.3582 0.9722
3.000 0.8381 0.00861 0.00354 -0.0752 0.3537 0.9810
3.250 0.8792 0.00881 0.00368 -0.0780 0.3484 0.9859
3.500 0.9157 0.00903 0.00385 -0.0800 0.3429 0.9909
3.750 0.9546 0.00916 0.00396 -0.0824 0.3398 0.9943
4.000 0.9970 0.00931 0.00407 -0.0855 0.3361 0.9975
4.250 1.0365 0.00948 0.00420 -0.0881 0.3323 0.9997
4.500 1.0584 0.00965 0.00434 -0.0871 0.3286 1.0000
4.750 1.0774 0.00978 0.00445 -0.0854 0.3261 1.0000
5.000 1.0975 0.00987 0.00455 -0.0840 0.3242 1.0000
5.250 1.1172 0.00999 0.00467 -0.0824 0.3218 1.0000
5.500 1.1364 0.01012 0.00479 -0.0808 0.3193 1.0000
5.750 1.1549 0.01028 0.00494 -0.0790 0.3164 1.0000
6.000 1.1722 0.01048 0.00511 -0.0771 0.3131 1.0000
6.250 1.1906 0.01065 0.00527 -0.0753 0.3102 1.0000
6.500 1.2111 0.01076 0.00540 -0.0740 0.3083 1.0000
6.750 1.2307 0.01090 0.00555 -0.0725 0.3061 1.0000
7.000 1.2483 0.01105 0.00570 -0.0706 0.3038 1.0000
7.250 1.2637 0.01122 0.00587 -0.0683 0.3015 1.0000
7.500 1.2791 0.01141 0.00606 -0.0660 0.2992 1.0000
7.750 1.2940 0.01166 0.00629 -0.0637 0.2964 1.0000
8.000 1.3121 0.01185 0.00650 -0.0621 0.2945 1.0000
8.250 1.3325 0.01199 0.00667 -0.0609 0.2926 1.0000
8.500 1.3524 0.01217 0.00687 -0.0596 0.2901 1.0000
8.750 1.3713 0.01239 0.00710 -0.0583 0.2875 1.0000
9.000 1.3895 0.01265 0.00737 -0.0568 0.2848 1.0000
9.250 1.4063 0.01297 0.00768 -0.0553 0.2818 1.0000
9.500 1.4241 0.01328 0.00801 -0.0539 0.2790 1.0000
9.750 1.4450 0.01349 0.00826 -0.0530 0.2770 1.0000
10.000 1.4647 0.01376 0.00855 -0.0520 0.2743 1.0000
10.250 1.4830 0.01409 0.00889 -0.0509 0.2708 1.0000
10.500 1.4987 0.01454 0.00933 -0.0494 0.2666 1.0000
10.750 1.5169 0.01490 0.00972 -0.0484 0.2619 1.0000
11.000 1.5348 0.01530 0.01013 -0.0473 0.2569 1.0000
11.250 1.5475 0.01595 0.01075 -0.0457 0.2498 1.0000
11.500 1.5643 0.01644 0.01126 -0.0447 0.2424 1.0000
11.750 1.5754 0.01724 0.01203 -0.0431 0.2347 1.0000
12.000 1.5823 0.01832 0.01304 -0.0412 0.2196 1.0000
12.250 1.5822 0.01987 0.01450 -0.0388 0.2004 1.0000
12.500 1.5810 0.02164 0.01621 -0.0366 0.1870 1.0000
12.750 1.5809 0.02345 0.01800 -0.0349 0.1782 1.0000
13.000 1.5829 0.02526 0.01981 -0.0335 0.1723 1.0000
13.250 1.5829 0.02732 0.02189 -0.0323 0.1671 1.0000
13.500 1.5895 0.02894 0.02355 -0.0316 0.1647 1.0000
13.750 1.5945 0.03075 0.02542 -0.0309 0.1626 1.0000
14.000 1.5957 0.03295 0.02765 -0.0302 0.1600 1.0000
14.250 1.5944 0.03544 0.03019 -0.0296 0.1575 1.0000
14.500 1.5907 0.03823 0.03303 -0.0290 0.1547 1.0000
14.750 1.5941 0.04038 0.03525 -0.0287 0.1534 1.0000
15.000 1.5992 0.04238 0.03731 -0.0284 0.1521 1.0000
15.250 1.6006 0.04476 0.03975 -0.0282 0.1502 1.0000
15.500 1.5996 0.04742 0.04247 -0.0279 0.1486 1.0000
15.750 1.5959 0.05039 0.04549 -0.0277 0.1469 1.0000
16.000 1.5907 0.05355 0.04872 -0.0276 0.1453 1.0000
16.250 1.5831 0.05702 0.05224 -0.0275 0.1433 1.0000
16.500 1.5753 0.06055 0.05583 -0.0275 0.1415 1.0000
16.750 1.5775 0.06303 0.05838 -0.0276 0.1407 1.0000
17.000 1.5819 0.06529 0.06071 -0.0277 0.1394 1.0000
17.250 1.5827 0.06798 0.06347 -0.0279 0.1379 1.0000
17.500 1.5808 0.07099 0.06654 -0.0281 0.1361 1.0000
17.750 1.5769 0.07422 0.06982 -0.0284 0.1341 1.0000
18.000 1.5693 0.07796 0.07362 -0.0288 0.1322 1.0000
18.250 1.5604 0.08189 0.07758 -0.0293 0.1300 1.0000
18.500 1.5592 0.08492 0.08069 -0.0297 0.1281 1.0000
18.750 1.5613 0.08753 0.08336 -0.0301 0.1259 1.0000
19.000 1.5580 0.09084 0.08673 -0.0307 0.1238 1.0000
19.250 1.5499 0.09479 0.09071 -0.0314 0.1205 1.0000
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