GOE 460 AIRFOIL (goe460-il) Xfoil prediction polar at RE=200,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 460 AIRFOIL (goe460-il) Reynolds number: 200,000 Max Cl/Cd: 39.42 at α=10.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe460-il-200000-n5.txt Download as CSV file: xf-goe460-il-200000-n5.csv |
XFOIL Version 6.96
Calculated polar for: GOE 460 AIRFOIL
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.200 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-18.750 -0.9935 0.08905 0.08273 -0.0573 1.0000 0.0706
-18.500 -0.9999 0.08518 0.07883 -0.0585 1.0000 0.0722
-18.250 -1.0044 0.08161 0.07520 -0.0596 1.0000 0.0740
-18.000 -1.0084 0.07815 0.07166 -0.0605 1.0000 0.0763
-17.750 -1.0128 0.07470 0.06816 -0.0614 1.0000 0.0784
-17.500 -1.0172 0.07134 0.06475 -0.0621 1.0000 0.0806
-17.250 -1.0197 0.06825 0.06159 -0.0627 1.0000 0.0834
-17.000 -1.0204 0.06545 0.05870 -0.0631 1.0000 0.0863
-16.750 -1.0240 0.06238 0.05560 -0.0635 1.0000 0.0888
-16.500 -1.0252 0.05965 0.05279 -0.0638 1.0000 0.0922
-16.250 -1.0231 0.05734 0.05036 -0.0638 1.0000 0.0955
-16.000 -1.0266 0.05455 0.04756 -0.0637 1.0000 0.0983
-15.750 -1.0272 0.05213 0.04508 -0.0636 1.0000 0.1017
-15.500 -1.0243 0.05009 0.04294 -0.0632 1.0000 0.1049
-15.250 -1.0248 0.04784 0.04065 -0.0627 1.0000 0.1078
-15.000 -1.0258 0.04563 0.03842 -0.0621 1.0000 0.1106
-14.750 -1.0244 0.04370 0.03643 -0.0613 1.0000 0.1139
-14.500 -1.0204 0.04206 0.03471 -0.0604 1.0000 0.1170
-14.250 -1.0212 0.04013 0.03277 -0.0592 1.0000 0.1200
-14.000 -1.0215 0.03833 0.03096 -0.0579 1.0000 0.1235
-13.750 -1.0193 0.03681 0.02940 -0.0565 1.0000 0.1269
-13.500 -1.0166 0.03541 0.02796 -0.0549 1.0000 0.1304
-13.250 -1.0173 0.03390 0.02646 -0.0529 1.0000 0.1341
-13.000 -1.0159 0.03262 0.02517 -0.0509 1.0000 0.1381
-12.750 -1.0131 0.03151 0.02403 -0.0487 1.0000 0.1424
-12.500 -1.0135 0.03034 0.02288 -0.0462 1.0000 0.1470
-12.250 -1.0119 0.02938 0.02192 -0.0436 1.0000 0.1525
-12.000 -1.0114 0.02847 0.02101 -0.0406 1.0000 0.1580
-11.750 -1.0107 0.02769 0.02022 -0.0375 1.0000 0.1640
-11.500 -1.0089 0.02703 0.01953 -0.0344 1.0000 0.1696
-11.250 -1.0105 0.02636 0.01887 -0.0307 1.0000 0.1747
-11.000 -1.0102 0.02585 0.01832 -0.0270 1.0000 0.1807
-10.750 -0.9873 0.02508 0.01754 -0.0278 0.9969 0.1881
-10.500 -0.9590 0.02445 0.01684 -0.0293 0.9927 0.1962
-10.250 -0.9328 0.02371 0.01609 -0.0304 0.9873 0.2032
-10.000 -0.9036 0.02307 0.01541 -0.0320 0.9823 0.2103
-9.750 -0.8718 0.02252 0.01479 -0.0339 0.9784 0.2170
-9.500 -0.8508 0.02186 0.01416 -0.0338 0.9716 0.2232
-9.000 -0.7941 0.02082 0.01305 -0.0359 0.9637 0.2363
-8.750 -0.7737 0.02029 0.01254 -0.0353 0.9564 0.2420
-8.500 -0.7445 0.01982 0.01203 -0.0363 0.9524 0.2482
-8.250 -0.7123 0.01933 0.01153 -0.0379 0.9495 0.2535
-8.000 -0.6940 0.01889 0.01110 -0.0367 0.9409 0.2585
-7.750 -0.6644 0.01843 0.01063 -0.0377 0.9364 0.2650
-7.500 -0.6305 0.01795 0.01015 -0.0395 0.9331 0.2722
-7.250 -0.6137 0.01755 0.00979 -0.0379 0.9234 0.2797
-7.000 -0.5837 0.01712 0.00935 -0.0388 0.9180 0.2884
-6.750 -0.5631 0.01671 0.00899 -0.0379 0.9096 0.2979
-6.500 -0.5395 0.01630 0.00861 -0.0375 0.9016 0.3095
-6.250 -0.5141 0.01592 0.00825 -0.0373 0.8942 0.3218
-6.000 -0.4944 0.01557 0.00793 -0.0360 0.8844 0.3338
-5.750 -0.4699 0.01521 0.00759 -0.0356 0.8762 0.3472
-5.500 -0.4500 0.01493 0.00732 -0.0341 0.8659 0.3608
-5.250 -0.4273 0.01464 0.00703 -0.0332 0.8571 0.3755
-5.000 -0.4092 0.01440 0.00681 -0.0313 0.8466 0.3880
-4.750 -0.3882 0.01419 0.00660 -0.0300 0.8373 0.4003
-4.500 -0.3695 0.01403 0.00643 -0.0282 0.8269 0.4130
-4.250 -0.3502 0.01385 0.00627 -0.0265 0.8172 0.4252
-4.000 -0.3313 0.01370 0.00613 -0.0246 0.8067 0.4382
-3.500 -0.2929 0.01344 0.00588 -0.0211 0.7856 0.4648
-3.250 -0.2735 0.01334 0.00579 -0.0193 0.7750 0.4761
-3.000 -0.2520 0.01324 0.00566 -0.0179 0.7640 0.4870
-2.750 -0.2327 0.01315 0.00559 -0.0161 0.7520 0.4964
-2.500 -0.2103 0.01307 0.00546 -0.0149 0.7410 0.5067
-2.250 -0.1905 0.01299 0.00540 -0.0132 0.7281 0.5160
-2.000 -0.1696 0.01293 0.00530 -0.0117 0.7151 0.5260
-1.750 -0.1479 0.01285 0.00520 -0.0103 0.7011 0.5353
-1.500 -0.1267 0.01281 0.00510 -0.0088 0.6862 0.5453
-1.250 -0.1056 0.01276 0.00504 -0.0073 0.6720 0.5544
-1.000 -0.0840 0.01274 0.00497 -0.0060 0.6598 0.5645
-0.750 -0.0622 0.01271 0.00492 -0.0046 0.6476 0.5746
-0.500 -0.0421 0.01271 0.00489 -0.0030 0.6351 0.5869
-0.250 -0.0208 0.01269 0.00488 -0.0015 0.6236 0.5995
0.000 0.0000 0.01268 0.00488 0.0000 0.6116 0.6117
0.250 0.0207 0.01269 0.00488 0.0016 0.5993 0.6235
0.500 0.0422 0.01271 0.00489 0.0030 0.5868 0.6350
0.750 0.0622 0.01272 0.00492 0.0046 0.5746 0.6474
1.000 0.0841 0.01274 0.00497 0.0060 0.5645 0.6596
1.250 0.1057 0.01276 0.00504 0.0073 0.5545 0.6720
1.500 0.1268 0.01281 0.00510 0.0088 0.5453 0.6862
1.750 0.1479 0.01285 0.00520 0.0103 0.5353 0.7011
2.000 0.1697 0.01293 0.00530 0.0117 0.5261 0.7149
2.250 0.1905 0.01299 0.00540 0.0132 0.5160 0.7281
2.500 0.2104 0.01307 0.00546 0.0149 0.5067 0.7409
2.750 0.2328 0.01315 0.00559 0.0161 0.4964 0.7519
3.000 0.2520 0.01323 0.00566 0.0179 0.4869 0.7640
3.250 0.2735 0.01333 0.00579 0.0193 0.4761 0.7750
3.500 0.2928 0.01344 0.00588 0.0211 0.4646 0.7856
3.750 0.3118 0.01358 0.00599 0.0229 0.4521 0.7965
4.000 0.3314 0.01370 0.00613 0.0246 0.4384 0.8066
4.250 0.3505 0.01385 0.00627 0.0264 0.4259 0.8173
4.500 0.3695 0.01403 0.00643 0.0282 0.4130 0.8269
4.750 0.3884 0.01418 0.00660 0.0300 0.4005 0.8373
5.000 0.4094 0.01439 0.00681 0.0313 0.3883 0.8465
5.250 0.4274 0.01464 0.00703 0.0332 0.3755 0.8571
5.500 0.4505 0.01492 0.00732 0.0340 0.3611 0.8660
5.750 0.4699 0.01521 0.00759 0.0355 0.3470 0.8761
6.000 0.4943 0.01557 0.00793 0.0360 0.3337 0.8843
6.250 0.5143 0.01592 0.00824 0.0373 0.3219 0.8942
6.500 0.5395 0.01630 0.00861 0.0374 0.3091 0.9018
6.750 0.5632 0.01671 0.00899 0.0379 0.2978 0.9098
7.000 0.5838 0.01713 0.00935 0.0388 0.2881 0.9181
7.250 0.6138 0.01756 0.00979 0.0379 0.2793 0.9235
7.500 0.6305 0.01796 0.01015 0.0395 0.2718 0.9332
7.750 0.6646 0.01843 0.01063 0.0376 0.2647 0.9364
8.000 0.6942 0.01888 0.01110 0.0367 0.2584 0.9410
8.250 0.7127 0.01933 0.01152 0.0378 0.2533 0.9495
8.500 0.7450 0.01981 0.01203 0.0363 0.2480 0.9524
8.750 0.7742 0.02028 0.01253 0.0352 0.2419 0.9565
9.000 0.7937 0.02082 0.01305 0.0359 0.2358 0.9641
9.500 0.8513 0.02185 0.01415 0.0337 0.2230 0.9717
9.750 0.8727 0.02250 0.01477 0.0337 0.2173 0.9785
10.000 0.9044 0.02305 0.01539 0.0319 0.2105 0.9824
10.250 0.9338 0.02370 0.01607 0.0303 0.2032 0.9875
10.500 0.9598 0.02444 0.01682 0.0292 0.1963 0.9927
10.750 0.9882 0.02507 0.01752 0.0276 0.1879 0.9970
11.000 1.0103 0.02583 0.01829 0.0270 0.1806 1.0000
11.250 1.0106 0.02634 0.01884 0.0307 0.1746 1.0000
11.500 1.0089 0.02701 0.01950 0.0344 0.1694 1.0000
11.750 1.0110 0.02765 0.02018 0.0375 0.1638 1.0000
12.000 1.0117 0.02844 0.02098 0.0406 0.1578 1.0000
12.250 1.0124 0.02934 0.02187 0.0435 0.1524 1.0000
12.500 1.0138 0.03031 0.02285 0.0461 0.1468 1.0000
12.750 1.0134 0.03149 0.02400 0.0487 0.1421 1.0000
13.000 1.0166 0.03258 0.02512 0.0508 0.1380 1.0000
13.250 1.0181 0.03386 0.02641 0.0529 0.1340 1.0000
13.500 1.0174 0.03537 0.02791 0.0548 0.1303 1.0000
13.750 1.0204 0.03675 0.02934 0.0564 0.1268 1.0000
14.000 1.0224 0.03829 0.03091 0.0578 0.1231 1.0000
14.250 1.0223 0.04007 0.03271 0.0591 0.1199 1.0000
14.500 1.0219 0.04198 0.03463 0.0603 0.1169 1.0000
14.750 1.0260 0.04362 0.03635 0.0612 0.1138 1.0000
15.000 1.0274 0.04555 0.03834 0.0619 0.1106 1.0000
15.250 1.0262 0.04779 0.04059 0.0626 0.1076 1.0000
15.500 1.0262 0.04999 0.04283 0.0631 0.1049 1.0000
15.750 1.0289 0.05206 0.04501 0.0634 0.1012 1.0000
16.000 1.0282 0.05451 0.04751 0.0635 0.0980 1.0000
16.250 1.0249 0.05728 0.05028 0.0636 0.0954 1.0000
16.500 1.0274 0.05957 0.05270 0.0635 0.0920 1.0000
16.750 1.0263 0.06228 0.05549 0.0633 0.0888 1.0000
17.000 1.0225 0.06537 0.05861 0.0629 0.0862 1.0000
17.250 1.0219 0.06817 0.06151 0.0625 0.0832 1.0000
17.500 1.0194 0.07128 0.06469 0.0619 0.0803 1.0000
17.750 1.0149 0.07467 0.06812 0.0611 0.0782 1.0000
18.000 1.0110 0.07806 0.07157 0.0602 0.0760 1.0000
18.250 1.0074 0.08148 0.07506 0.0593 0.0739 1.0000
18.500 1.0023 0.08514 0.07878 0.0582 0.0720 1.0000
18.750 0.9963 0.08897 0.08265 0.0570 0.0705 1.0000
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