GOE 775 AIRFOIL (goe775-il) Xfoil prediction polar at RE=100,000 Ncrit=9
| Details | Polar file |
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Airfoil: GOE 775 AIRFOIL (goe775-il) Reynolds number: 100,000 Max Cl/Cd: 36.87 at α=7.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-goe775-il-100000.txt Download as CSV file: xf-goe775-il-100000.csv |
XFOIL Version 6.96
Calculated polar for: GOE 775 AIRFOIL
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.100 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-15.750 -0.5089 0.17275 0.16616 -0.0063 1.0000 0.1966
-15.500 -1.0643 0.06879 0.06112 -0.0567 1.0000 0.1531
-15.250 -1.1278 0.06117 0.05310 -0.0566 1.0000 0.1537
-15.000 -1.0553 0.06439 0.05673 -0.0562 1.0000 0.1592
-14.750 -1.0820 0.05984 0.05198 -0.0559 1.0000 0.1615
-14.500 -1.1151 0.05537 0.04724 -0.0545 1.0000 0.1637
-14.250 -1.1501 0.05149 0.04304 -0.0517 1.0000 0.1657
-14.000 -1.1380 0.05000 0.04158 -0.0509 1.0000 0.1695
-13.750 -1.1234 0.04905 0.04069 -0.0500 1.0000 0.1736
-13.500 -1.1374 0.04684 0.03830 -0.0471 1.0000 0.1769
-13.250 -1.1617 0.04460 0.03577 -0.0425 1.0000 0.1796
-13.000 -1.1325 0.04384 0.03520 -0.0429 1.0000 0.1847
-12.750 -1.1292 0.04273 0.03406 -0.0404 1.0000 0.1889
-12.500 -1.1447 0.04124 0.03238 -0.0355 1.0000 0.1924
-12.250 -1.1543 0.03995 0.03095 -0.0308 1.0000 0.1959
-12.000 -1.1253 0.03940 0.03063 -0.0311 1.0000 0.2017
-11.750 -1.1349 0.03850 0.02963 -0.0259 1.0000 0.2057
-11.500 -1.1540 0.03749 0.02840 -0.0191 1.0000 0.2092
-11.250 -1.1284 0.03677 0.02790 -0.0189 1.0000 0.2151
-11.000 -1.1264 0.03607 0.02717 -0.0151 1.0000 0.2202
-10.750 -1.1388 0.03518 0.02607 -0.0090 1.0000 0.2248
-10.500 -1.1188 0.03449 0.02557 -0.0079 1.0000 0.2309
-10.250 -1.1147 0.03387 0.02495 -0.0043 1.0000 0.2369
-10.000 -1.1238 0.03305 0.02389 0.0014 1.0000 0.2424
-9.750 -1.1015 0.03251 0.02362 0.0022 1.0000 0.2494
-9.500 -1.1003 0.03187 0.02288 0.0064 1.0000 0.2563
-9.250 -1.0904 0.03119 0.02226 0.0091 1.0000 0.2634
-9.000 -1.0808 0.03073 0.02184 0.0120 1.0000 0.2711
-8.750 -1.0766 0.03004 0.02105 0.0156 1.0000 0.2789
-8.500 -1.0621 0.02967 0.02083 0.0177 1.0000 0.2871
-8.250 -1.0589 0.02906 0.02007 0.0215 1.0000 0.2958
-8.000 -1.0421 0.02874 0.01995 0.0231 1.0000 0.3042
-7.750 -1.0380 0.02824 0.01927 0.0267 1.0000 0.3137
-7.500 -1.0203 0.02795 0.01921 0.0282 1.0000 0.3223
-7.250 -1.0139 0.02755 0.01864 0.0313 1.0000 0.3323
-7.000 -0.9970 0.02730 0.01861 0.0328 1.0000 0.3410
-6.750 -0.9885 0.02698 0.01815 0.0355 1.0000 0.3514
-6.500 -0.9720 0.02677 0.01813 0.0370 1.0000 0.3601
-6.250 -0.9619 0.02652 0.01776 0.0393 1.0000 0.3710
-6.000 -0.9149 0.02651 0.01792 0.0351 0.9926 0.3846
-5.750 -0.8729 0.02637 0.01782 0.0318 0.9836 0.3986
-5.500 -0.8301 0.02626 0.01767 0.0283 0.9748 0.4141
-5.250 -0.7875 0.02619 0.01771 0.0251 0.9653 0.4285
-5.000 -0.7484 0.02606 0.01768 0.0227 0.9551 0.4424
-4.750 -0.7033 0.02592 0.01757 0.0191 0.9468 0.4586
-4.500 -0.6724 0.02577 0.01738 0.0182 0.9345 0.4742
-4.250 -0.6216 0.02572 0.01751 0.0141 0.9280 0.4904
-4.000 -0.5930 0.02557 0.01744 0.0139 0.9151 0.5038
-3.750 -0.5434 0.02535 0.01724 0.0099 0.9090 0.5208
-3.500 -0.5175 0.02526 0.01721 0.0103 0.8954 0.5342
-3.250 -0.4648 0.02501 0.01707 0.0061 0.8896 0.5497
-3.000 -0.4411 0.02484 0.01689 0.0069 0.8762 0.5636
-2.750 -0.3909 0.02453 0.01662 0.0033 0.8701 0.5799
-2.500 -0.3593 0.02441 0.01662 0.0031 0.8583 0.5924
-2.250 -0.3191 0.02401 0.01623 0.0014 0.8501 0.6080
-2.000 -0.2860 0.02380 0.01608 0.0010 0.8395 0.6223
-1.750 -0.2479 0.02349 0.01585 0.0000 0.8298 0.6360
-1.500 -0.2169 0.02315 0.01550 0.0000 0.8196 0.6514
-1.250 -0.1815 0.02290 0.01533 -0.0004 0.8086 0.6654
-1.000 -0.1473 0.02264 0.01512 -0.0007 0.7982 0.6793
-0.750 -0.1181 0.02228 0.01474 -0.0001 0.7866 0.6955
-0.500 -0.0830 0.02223 0.01478 -0.0003 0.7745 0.7083
-0.250 -0.0467 0.02195 0.01451 -0.0007 0.7636 0.7225
0.000 -0.0249 0.02187 0.01441 0.0009 0.7493 0.7386
0.250 0.0241 0.02187 0.01441 -0.0012 0.7390 0.7489
0.500 0.0456 0.02195 0.01451 0.0005 0.7230 0.7633
0.750 0.0829 0.02222 0.01478 0.0000 0.7091 0.7740
1.000 0.1169 0.02227 0.01474 -0.0001 0.6960 0.7864
1.250 0.1469 0.02264 0.01513 0.0004 0.6801 0.7978
1.500 0.1813 0.02288 0.01530 0.0001 0.6665 0.8085
1.750 0.2160 0.02314 0.01550 -0.0002 0.6521 0.8195
2.000 0.2472 0.02348 0.01584 -0.0002 0.6369 0.8297
2.250 0.2864 0.02378 0.01605 -0.0014 0.6235 0.8393
2.500 0.3182 0.02400 0.01623 -0.0016 0.6089 0.8501
2.750 0.3587 0.02440 0.01662 -0.0033 0.5935 0.8583
3.000 0.3914 0.02450 0.01657 -0.0037 0.5813 0.8700
3.250 0.4402 0.02483 0.01690 -0.0071 0.5646 0.8763
3.500 0.4646 0.02500 0.01706 -0.0064 0.5509 0.8897
3.750 0.5178 0.02523 0.01717 -0.0107 0.5357 0.8954
4.000 0.5430 0.02534 0.01725 -0.0102 0.5219 0.9090
4.250 0.5927 0.02556 0.01744 -0.0142 0.5050 0.9152
4.500 0.6221 0.02569 0.01747 -0.0145 0.4919 0.9281
4.750 0.6725 0.02573 0.01735 -0.0186 0.4755 0.9347
5.000 0.7034 0.02591 0.01757 -0.0195 0.4599 0.9469
5.250 0.7484 0.02604 0.01766 -0.0231 0.4438 0.9553
5.500 0.7882 0.02615 0.01764 -0.0256 0.4301 0.9654
5.750 0.8296 0.02623 0.01767 -0.0287 0.4153 0.9752
6.000 0.8732 0.02634 0.01780 -0.0323 0.3999 0.9839
6.250 0.9157 0.02646 0.01786 -0.0357 0.3860 0.9928
6.500 0.9616 0.02646 0.01769 -0.0397 0.3724 1.0000
6.750 0.9715 0.02674 0.01810 -0.0373 0.3616 1.0000
7.000 0.9881 0.02691 0.01808 -0.0359 0.3527 1.0000
7.250 0.9965 0.02727 0.01857 -0.0332 0.3424 1.0000
7.500 1.0129 0.02747 0.01860 -0.0316 0.3336 1.0000
7.750 1.0200 0.02791 0.01917 -0.0286 0.3237 1.0000
8.000 1.0360 0.02817 0.01925 -0.0268 0.3150 1.0000
8.250 1.0420 0.02869 0.01990 -0.0236 0.3057 1.0000
8.500 1.0569 0.02900 0.02006 -0.0216 0.2971 1.0000
8.750 1.0624 0.02961 0.02077 -0.0182 0.2885 1.0000
9.000 1.0748 0.03000 0.02106 -0.0158 0.2802 1.0000
9.250 1.0818 0.03066 0.02175 -0.0126 0.2724 1.0000
9.500 1.0892 0.03117 0.02226 -0.0094 0.2646 1.0000
9.750 1.1026 0.03179 0.02275 -0.0072 0.2575 1.0000
10.000 1.1015 0.03247 0.02358 -0.0027 0.2506 1.0000
10.250 1.1187 0.03295 0.02387 -0.0010 0.2438 1.0000
10.500 1.1167 0.03380 0.02485 0.0035 0.2380 1.0000
10.750 1.1180 0.03446 0.02556 0.0076 0.2321 1.0000
11.000 1.1433 0.03509 0.02593 0.0079 0.2256 1.0000
11.250 1.1290 0.03599 0.02707 0.0142 0.2212 1.0000
11.500 1.1278 0.03674 0.02788 0.0185 0.2162 1.0000
11.750 1.1593 0.03740 0.02825 0.0178 0.2099 1.0000
12.000 1.1394 0.03842 0.02952 0.0247 0.2065 1.0000
12.250 1.1272 0.03935 0.03057 0.0303 0.2026 1.0000
12.500 1.1425 0.03998 0.03109 0.0320 0.1976 1.0000
12.750 1.1506 0.04111 0.03221 0.0343 0.1931 1.0000
13.000 1.1331 0.04261 0.03393 0.0395 0.1897 1.0000
13.250 1.1319 0.04387 0.03525 0.0424 0.1856 1.0000
13.500 1.1693 0.04439 0.03550 0.0412 0.1801 1.0000
13.750 1.1434 0.04661 0.03803 0.0460 0.1776 1.0000
14.000 1.1270 0.04890 0.04053 0.0492 0.1744 1.0000
14.250 1.1325 0.05029 0.04193 0.0505 0.1705 1.0000
14.500 1.1588 0.05109 0.04258 0.0506 0.1662 1.0000
14.750 1.1233 0.05489 0.04672 0.0535 0.1642 1.0000
15.000 1.0891 0.05937 0.05149 0.0551 0.1621 1.0000
15.250 1.0586 0.06421 0.05654 0.0555 0.1598 1.0000
15.500 1.1392 0.06044 0.05231 0.0557 0.1541 1.0000
15.750 1.0785 0.06760 0.05987 0.0561 0.1533 1.0000
16.000 0.9527 0.08421 0.07704 0.0513 0.1538 1.0000
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