GOE 383 AIRFOIL (goe383-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 383 AIRFOIL (goe383-il) Reynolds number: 1,000,000 Max Cl/Cd: 106.06 at α=6.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe383-il-1000000-n5.txt Download as CSV file: xf-goe383-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: GOE 383 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
------ -------- --------- --------- -------- -------- --------
-19.250 -0.7552 0.11558 0.11284 -0.0549 1.0000 0.0254
-19.000 -0.8162 0.10111 0.09812 -0.0637 1.0000 0.0255
-18.750 -0.8510 0.09158 0.08843 -0.0697 0.9913 0.0255
-18.500 -0.8768 0.08368 0.08038 -0.0749 0.9784 0.0256
-18.250 -0.9007 0.07646 0.07301 -0.0794 0.9690 0.0256
-18.000 -0.9210 0.07014 0.06655 -0.0831 0.9613 0.0257
-17.750 -0.9392 0.06425 0.06052 -0.0865 0.9537 0.0257
-17.500 -0.9536 0.05889 0.05503 -0.0896 0.9473 0.0258
-17.250 -0.9655 0.05397 0.04998 -0.0925 0.9399 0.0258
-17.000 -0.9739 0.04954 0.04542 -0.0951 0.9331 0.0259
-16.750 -0.9796 0.04558 0.04134 -0.0974 0.9246 0.0259
-16.500 -0.9827 0.04210 0.03773 -0.0992 0.9160 0.0260
-16.250 -0.9835 0.03908 0.03458 -0.1006 0.9044 0.0260
-16.000 -0.9819 0.03643 0.03181 -0.1017 0.8909 0.0261
-15.750 -0.9789 0.03412 0.02935 -0.1023 0.8742 0.0261
-15.500 -0.9737 0.03212 0.02720 -0.1027 0.8554 0.0262
-15.250 -0.9668 0.03035 0.02528 -0.1028 0.8362 0.0262
-15.000 -0.9585 0.02880 0.02358 -0.1028 0.8177 0.0263
-14.750 -0.9488 0.02744 0.02207 -0.1025 0.7998 0.0263
-14.500 -0.9380 0.02624 0.02074 -0.1021 0.7822 0.0264
-14.250 -0.9260 0.02519 0.01956 -0.1015 0.7652 0.0264
-14.000 -0.9130 0.02426 0.01852 -0.1007 0.7485 0.0265
-13.750 -0.8990 0.02345 0.01757 -0.0998 0.7323 0.0265
-13.500 -0.8842 0.02270 0.01672 -0.0988 0.7173 0.0266
-13.250 -0.8684 0.02202 0.01594 -0.0977 0.7046 0.0266
-13.000 -0.8557 0.02125 0.01507 -0.0961 0.6921 0.0267
-12.750 -0.8436 0.02060 0.01434 -0.0941 0.6823 0.0269
-12.250 -0.8070 0.01944 0.01305 -0.0919 0.6653 0.0271
-12.000 -0.7865 0.01894 0.01249 -0.0911 0.6582 0.0272
-11.750 -0.7650 0.01849 0.01197 -0.0903 0.6515 0.0274
-11.500 -0.7428 0.01806 0.01149 -0.0896 0.6461 0.0275
-11.250 -0.7197 0.01765 0.01105 -0.0890 0.6418 0.0276
-11.000 -0.6962 0.01726 0.01062 -0.0884 0.6371 0.0278
-10.750 -0.6723 0.01690 0.01021 -0.0878 0.6323 0.0279
-10.250 -0.6234 0.01622 0.00944 -0.0869 0.6239 0.0282
-10.000 -0.5983 0.01588 0.00908 -0.0864 0.6207 0.0284
-9.750 -0.5730 0.01557 0.00872 -0.0860 0.6168 0.0286
-9.500 -0.5476 0.01527 0.00838 -0.0857 0.6125 0.0287
-9.250 -0.5220 0.01499 0.00805 -0.0853 0.6081 0.0289
-8.750 -0.4698 0.01444 0.00743 -0.0847 0.6012 0.0293
-8.500 -0.4433 0.01417 0.00714 -0.0844 0.5983 0.0295
-8.250 -0.4166 0.01392 0.00686 -0.0842 0.5952 0.0297
-8.000 -0.3898 0.01368 0.00659 -0.0839 0.5916 0.0299
-7.750 -0.3628 0.01348 0.00635 -0.0837 0.5877 0.0301
-7.500 -0.3360 0.01326 0.00610 -0.0835 0.5842 0.0303
-7.250 -0.3095 0.01300 0.00581 -0.0833 0.5813 0.0307
-7.000 -0.2821 0.01275 0.00557 -0.0831 0.5799 0.0310
-6.750 -0.2545 0.01253 0.00535 -0.0830 0.5781 0.0313
-6.500 -0.2268 0.01233 0.00514 -0.0829 0.5759 0.0316
-6.250 -0.1989 0.01215 0.00495 -0.0828 0.5732 0.0319
-6.000 -0.1710 0.01198 0.00477 -0.0828 0.5702 0.0323
-5.750 -0.1431 0.01183 0.00459 -0.0827 0.5671 0.0327
-5.500 -0.1152 0.01168 0.00443 -0.0826 0.5641 0.0331
-5.250 -0.0872 0.01156 0.00427 -0.0826 0.5611 0.0335
-5.000 -0.0588 0.01141 0.00413 -0.0826 0.5591 0.0338
-4.750 -0.0305 0.01125 0.00397 -0.0826 0.5570 0.0343
-4.500 -0.0022 0.01109 0.00382 -0.0826 0.5543 0.0349
-4.250 0.0262 0.01096 0.00369 -0.0826 0.5510 0.0356
-4.000 0.0546 0.01085 0.00358 -0.0826 0.5472 0.0363
-3.750 0.0828 0.01077 0.00347 -0.0826 0.5431 0.0371
-3.500 0.1113 0.01068 0.00337 -0.0826 0.5396 0.0378
-3.250 0.1399 0.01056 0.00326 -0.0827 0.5366 0.0390
-3.000 0.1686 0.01046 0.00318 -0.0828 0.5327 0.0405
-2.750 0.1971 0.01038 0.00310 -0.0828 0.5282 0.0420
-2.500 0.2252 0.01031 0.00302 -0.0828 0.5233 0.0442
-2.250 0.2538 0.01024 0.00295 -0.0829 0.5190 0.0466
-2.000 0.2823 0.01016 0.00288 -0.0830 0.5135 0.0499
-1.750 0.3103 0.01010 0.00282 -0.0829 0.5062 0.0543
-1.500 0.3382 0.01003 0.00275 -0.0829 0.4991 0.0620
-1.250 0.3645 0.00980 0.00268 -0.0827 0.4900 0.1086
-1.000 0.3919 0.00976 0.00266 -0.0826 0.4816 0.1271
-0.750 0.4193 0.00971 0.00264 -0.0826 0.4722 0.1446
-0.500 0.4464 0.00969 0.00264 -0.0825 0.4636 0.1627
-0.250 0.4731 0.00960 0.00264 -0.0823 0.4548 0.1973
0.000 0.4992 0.00950 0.00266 -0.0821 0.4467 0.2484
0.250 0.5263 0.00948 0.00270 -0.0820 0.4388 0.2776
0.500 0.5527 0.00950 0.00276 -0.0818 0.4311 0.3051
0.750 0.5800 0.00944 0.00279 -0.0818 0.4261 0.3413
1.250 0.6305 0.00905 0.00291 -0.0812 0.4156 0.5208
1.500 0.6562 0.00893 0.00300 -0.0809 0.4111 0.5957
1.750 0.6834 0.00893 0.00309 -0.0808 0.4069 0.6310
2.000 0.7102 0.00898 0.00319 -0.0806 0.4018 0.6581
2.250 0.7361 0.00909 0.00331 -0.0803 0.3955 0.6835
2.500 0.7632 0.00915 0.00341 -0.0802 0.3907 0.7046
2.750 0.7899 0.00921 0.00351 -0.0800 0.3857 0.7255
3.000 0.8159 0.00930 0.00364 -0.0797 0.3809 0.7486
3.250 0.8417 0.00941 0.00377 -0.0794 0.3767 0.7686
3.500 0.8684 0.00947 0.00388 -0.0793 0.3741 0.7870
3.750 0.8949 0.00951 0.00400 -0.0790 0.3716 0.8092
4.000 0.9206 0.00958 0.00413 -0.0787 0.3685 0.8344
4.250 0.9455 0.00966 0.00428 -0.0782 0.3650 0.8593
4.500 0.9692 0.00978 0.00445 -0.0774 0.3613 0.8866
4.750 0.9920 0.00992 0.00463 -0.0765 0.3578 0.9124
5.000 1.0166 0.01001 0.00479 -0.0758 0.3558 0.9387
5.250 1.0450 0.01015 0.00495 -0.0760 0.3529 0.9656
5.500 1.0791 0.01034 0.00514 -0.0776 0.3491 0.9830
5.750 1.1122 0.01057 0.00534 -0.0790 0.3448 0.9936
6.000 1.1423 0.01082 0.00556 -0.0799 0.3407 1.0000
6.250 1.1596 0.01095 0.00570 -0.0781 0.3384 1.0000
6.500 1.1794 0.01112 0.00587 -0.0767 0.3355 1.0000
6.750 1.1995 0.01134 0.00608 -0.0756 0.3313 1.0000
7.000 1.2180 0.01165 0.00635 -0.0742 0.3256 1.0000
7.250 1.2387 0.01192 0.00661 -0.0733 0.3204 1.0000
7.500 1.2594 0.01221 0.00689 -0.0724 0.3146 1.0000
7.750 1.2781 0.01261 0.00725 -0.0713 0.3086 1.0000
8.000 1.2987 0.01294 0.00757 -0.0704 0.3030 1.0000
8.250 1.3172 0.01337 0.00798 -0.0694 0.2956 1.0000
8.500 1.3355 0.01384 0.00842 -0.0683 0.2890 1.0000
8.750 1.3525 0.01439 0.00894 -0.0672 0.2803 1.0000
9.000 1.3680 0.01502 0.00953 -0.0659 0.2710 1.0000
9.250 1.3812 0.01581 0.01026 -0.0644 0.2607 1.0000
9.500 1.3939 0.01665 0.01106 -0.0629 0.2500 1.0000
9.750 1.4071 0.01751 0.01188 -0.0616 0.2411 1.0000
10.250 1.4323 0.01940 0.01373 -0.0591 0.2262 1.0000
10.750 1.4546 0.02160 0.01590 -0.0567 0.2120 1.0000
11.000 1.4621 0.02302 0.01729 -0.0554 0.2043 1.0000
11.250 1.4739 0.02418 0.01844 -0.0544 0.1987 1.0000
11.500 1.4828 0.02556 0.01981 -0.0534 0.1932 1.0000
11.750 1.4932 0.02688 0.02115 -0.0525 0.1894 1.0000
12.000 1.5051 0.02812 0.02241 -0.0518 0.1858 1.0000
12.250 1.5144 0.02958 0.02389 -0.0510 0.1819 1.0000
12.500 1.5212 0.03128 0.02559 -0.0501 0.1779 1.0000
12.750 1.5321 0.03266 0.02701 -0.0495 0.1746 1.0000
13.000 1.5384 0.03448 0.02883 -0.0487 0.1695 1.0000
13.250 1.5426 0.03649 0.03085 -0.0479 0.1647 1.0000
13.500 1.5491 0.03830 0.03267 -0.0472 0.1595 1.0000
13.750 1.5506 0.04062 0.03499 -0.0464 0.1543 1.0000
14.000 1.5559 0.04259 0.03699 -0.0457 0.1492 1.0000
14.250 1.5546 0.04522 0.03961 -0.0449 0.1428 1.0000
14.500 1.5536 0.04783 0.04222 -0.0442 0.1351 1.0000
14.750 1.5452 0.05118 0.04553 -0.0432 0.1234 1.0000
15.000 1.5148 0.05681 0.05105 -0.0417 0.0980 1.0000
15.250 1.4884 0.06223 0.05642 -0.0406 0.0808 1.0000
15.500 1.4780 0.06614 0.06033 -0.0401 0.0743 1.0000
15.750 1.4730 0.06954 0.06377 -0.0398 0.0709 1.0000
16.000 1.4697 0.07277 0.06704 -0.0397 0.0681 1.0000
16.250 1.4685 0.07584 0.07015 -0.0396 0.0661 1.0000
16.500 1.4665 0.07903 0.07340 -0.0396 0.0640 1.0000
16.750 1.4634 0.08237 0.07678 -0.0397 0.0621 1.0000
17.000 1.4627 0.08546 0.07992 -0.0398 0.0605 1.0000
17.250 1.4622 0.08853 0.08304 -0.0400 0.0587 1.0000
17.500 1.4577 0.09213 0.08669 -0.0403 0.0569 1.0000
17.750 1.4573 0.09524 0.08985 -0.0407 0.0553 1.0000
18.000 1.4542 0.09873 0.09339 -0.0411 0.0535 1.0000
18.250 1.4521 0.10205 0.09674 -0.0415 0.0515 1.0000
18.500 1.4482 0.10567 0.10042 -0.0421 0.0498 1.0000
18.750 1.4473 0.10889 0.10368 -0.0427 0.0478 1.0000
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