GOE 650 AIRFOIL (goe650-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: GOE 650 AIRFOIL (goe650-il) Reynolds number: 1,000,000 Max Cl/Cd: 109.58 at α=5.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-goe650-il-1000000.txt Download as CSV file: xf-goe650-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: GOE 650 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
------ -------- --------- --------- -------- -------- --------
-18.500 -0.7347 0.12697 0.12461 -0.0498 1.0000 0.0230
-18.250 -0.7560 0.11930 0.11684 -0.0539 1.0000 0.0233
-18.000 -0.7740 0.11244 0.10989 -0.0575 1.0000 0.0235
-17.750 -0.7891 0.10627 0.10364 -0.0608 1.0000 0.0239
-17.500 -0.8017 0.10077 0.09806 -0.0636 1.0000 0.0240
-17.250 -0.8146 0.09522 0.09244 -0.0665 1.0000 0.0242
-17.000 -0.8241 0.09047 0.08762 -0.0689 1.0000 0.0243
-16.750 -0.8356 0.08540 0.08248 -0.0714 1.0000 0.0245
-16.500 -0.8470 0.08048 0.07749 -0.0739 1.0000 0.0246
-16.250 -0.8563 0.07608 0.07301 -0.0760 1.0000 0.0247
-16.000 -0.8668 0.07157 0.06844 -0.0782 1.0000 0.0248
-15.750 -0.8803 0.06726 0.06407 -0.0799 1.0000 0.0250
-15.500 -0.8933 0.06328 0.06005 -0.0813 1.0000 0.0253
-15.250 -0.9093 0.05909 0.05582 -0.0828 1.0000 0.0254
-15.000 -0.9283 0.05483 0.05151 -0.0840 1.0000 0.0255
-14.750 -0.9512 0.05050 0.04712 -0.0849 1.0000 0.0256
-14.500 -0.9811 0.04611 0.04268 -0.0850 1.0000 0.0256
-14.250 -1.0023 0.04095 0.03744 -0.0885 0.9987 0.0257
-14.000 -1.0002 0.03449 0.03085 -0.0990 0.9939 0.0259
-13.750 -0.9825 0.02872 0.02492 -0.1094 0.9893 0.0262
-13.500 -0.9559 0.02570 0.02176 -0.1156 0.9863 0.0266
-13.250 -0.9271 0.02424 0.02022 -0.1186 0.9845 0.0272
-13.000 -0.8978 0.02289 0.01877 -0.1214 0.9831 0.0276
-12.750 -0.8671 0.02177 0.01756 -0.1239 0.9821 0.0281
-12.500 -0.8475 0.02090 0.01661 -0.1235 0.9769 0.0284
-12.250 -0.8183 0.02017 0.01581 -0.1248 0.9747 0.0287
-12.000 -0.7916 0.01872 0.01426 -0.1266 0.9726 0.0294
-11.750 -0.7618 0.01762 0.01311 -0.1284 0.9712 0.0300
-11.500 -0.7298 0.01681 0.01224 -0.1301 0.9702 0.0306
-11.250 -0.7037 0.01615 0.01153 -0.1304 0.9668 0.0311
-11.000 -0.6771 0.01555 0.01088 -0.1307 0.9630 0.0317
-10.750 -0.6452 0.01498 0.01025 -0.1319 0.9609 0.0323
-10.500 -0.6127 0.01445 0.00967 -0.1332 0.9590 0.0329
-10.250 -0.5797 0.01396 0.00911 -0.1346 0.9571 0.0333
-10.000 -0.5525 0.01318 0.00827 -0.1350 0.9531 0.0343
-9.750 -0.5272 0.01264 0.00769 -0.1348 0.9474 0.0351
-9.500 -0.4962 0.01217 0.00716 -0.1357 0.9437 0.0360
-9.250 -0.4638 0.01176 0.00670 -0.1367 0.9402 0.0370
-9.000 -0.4398 0.01145 0.00634 -0.1359 0.9329 0.0377
-8.750 -0.4100 0.01105 0.00588 -0.1364 0.9276 0.0389
-8.500 -0.3832 0.01064 0.00543 -0.1362 0.9213 0.0405
-8.250 -0.3567 0.01031 0.00507 -0.1360 0.9140 0.0423
-8.000 -0.3281 0.01000 0.00470 -0.1361 0.9075 0.0448
-7.750 -0.3037 0.00966 0.00435 -0.1353 0.8991 0.0494
-7.500 -0.2771 0.00922 0.00395 -0.1352 0.8918 0.0648
-7.250 -0.2527 0.00892 0.00372 -0.1344 0.8838 0.0794
-7.000 -0.2253 0.00874 0.00354 -0.1342 0.8765 0.0883
-6.750 -0.1986 0.00861 0.00339 -0.1338 0.8689 0.0935
-6.500 -0.1717 0.00847 0.00324 -0.1334 0.8611 0.0991
-6.250 -0.1445 0.00840 0.00312 -0.1331 0.8538 0.1027
-6.000 -0.1178 0.00826 0.00297 -0.1326 0.8460 0.1072
-5.750 -0.0906 0.00817 0.00285 -0.1323 0.8391 0.1116
-5.500 -0.0636 0.00810 0.00275 -0.1319 0.8315 0.1149
-5.250 -0.0367 0.00800 0.00261 -0.1315 0.8240 0.1197
-5.000 -0.0098 0.00790 0.00252 -0.1311 0.8170 0.1244
-4.750 0.0175 0.00785 0.00242 -0.1307 0.8102 0.1278
-4.500 0.0447 0.00777 0.00231 -0.1304 0.8044 0.1326
-4.250 0.0718 0.00767 0.00223 -0.1301 0.7985 0.1377
-4.000 0.0993 0.00762 0.00215 -0.1297 0.7928 0.1417
-3.750 0.1266 0.00756 0.00206 -0.1294 0.7874 0.1469
-3.500 0.1537 0.00746 0.00199 -0.1291 0.7816 0.1529
-3.250 0.1808 0.00743 0.00192 -0.1286 0.7746 0.1576
-3.000 0.2076 0.00735 0.00184 -0.1282 0.7680 0.1652
-2.750 0.2346 0.00729 0.00179 -0.1278 0.7613 0.1724
-2.500 0.2614 0.00725 0.00172 -0.1274 0.7543 0.1797
-2.250 0.2884 0.00717 0.00167 -0.1270 0.7478 0.1881
-2.000 0.3151 0.00711 0.00162 -0.1265 0.7407 0.1982
-1.750 0.3418 0.00707 0.00158 -0.1260 0.7338 0.2100
-1.250 0.3949 0.00697 0.00153 -0.1250 0.7193 0.2420
-0.750 0.4486 0.00687 0.00151 -0.1242 0.7059 0.2757
-0.500 0.4751 0.00685 0.00152 -0.1237 0.6990 0.2927
-0.250 0.5018 0.00681 0.00152 -0.1232 0.6907 0.3084
0.000 0.5279 0.00682 0.00154 -0.1226 0.6827 0.3220
0.250 0.5545 0.00680 0.00155 -0.1221 0.6734 0.3355
0.750 0.6056 0.00685 0.00159 -0.1207 0.6502 0.3601
1.000 0.6309 0.00689 0.00162 -0.1199 0.6349 0.3712
1.250 0.6548 0.00697 0.00165 -0.1189 0.6154 0.3823
1.500 0.6781 0.00707 0.00171 -0.1177 0.5918 0.3940
1.750 0.7000 0.00725 0.00178 -0.1163 0.5655 0.4039
2.000 0.7225 0.00741 0.00188 -0.1150 0.5439 0.4159
2.250 0.7454 0.00756 0.00199 -0.1139 0.5249 0.4273
2.500 0.7685 0.00772 0.00209 -0.1127 0.5070 0.4385
2.750 0.7916 0.00787 0.00221 -0.1116 0.4898 0.4508
3.000 0.8145 0.00802 0.00232 -0.1104 0.4716 0.4638
3.250 0.8370 0.00819 0.00245 -0.1092 0.4503 0.4783
3.500 0.8583 0.00839 0.00258 -0.1077 0.4262 0.4934
3.750 0.8786 0.00862 0.00274 -0.1061 0.3969 0.5127
4.000 0.8975 0.00888 0.00293 -0.1043 0.3670 0.5370
4.250 0.9161 0.00915 0.00314 -0.1024 0.3418 0.5659
4.500 0.9358 0.00934 0.00335 -0.1006 0.3243 0.5974
4.750 0.9548 0.00947 0.00353 -0.0988 0.3104 0.6402
5.000 0.9715 0.00948 0.00371 -0.0964 0.2992 0.7187
5.250 1.0421 0.00951 0.00416 -0.1060 0.2798 1.0000
5.500 1.0626 0.00977 0.00435 -0.1045 0.2673 1.0000
5.750 1.0814 0.01004 0.00455 -0.1026 0.2555 1.0000
6.000 1.1015 0.01024 0.00472 -0.1009 0.2464 1.0000
6.250 1.1204 0.01050 0.00492 -0.0991 0.2362 1.0000
6.500 1.1402 0.01073 0.00512 -0.0974 0.2278 1.0000
6.750 1.1597 0.01099 0.00534 -0.0957 0.2196 1.0000
7.000 1.1791 0.01126 0.00557 -0.0941 0.2110 1.0000
7.250 1.1987 0.01153 0.00580 -0.0925 0.2026 1.0000
7.500 1.2174 0.01185 0.00607 -0.0907 0.1933 1.0000
7.750 1.2372 0.01212 0.00633 -0.0892 0.1856 1.0000
8.000 1.2554 0.01248 0.00663 -0.0875 0.1768 1.0000
8.250 1.2753 0.01277 0.00691 -0.0860 0.1701 1.0000
8.500 1.2928 0.01317 0.00726 -0.0842 0.1612 1.0000
8.750 1.3121 0.01350 0.00758 -0.0828 0.1541 1.0000
9.000 1.3295 0.01393 0.00796 -0.0810 0.1461 1.0000
9.250 1.3482 0.01429 0.00832 -0.0795 0.1401 1.0000
9.500 1.3652 0.01476 0.00875 -0.0778 0.1330 1.0000
9.750 1.3834 0.01516 0.00914 -0.0763 0.1272 1.0000
10.000 1.3999 0.01567 0.00962 -0.0746 0.1210 1.0000
10.250 1.4180 0.01610 0.01006 -0.0732 0.1164 1.0000
10.500 1.4341 0.01665 0.01058 -0.0715 0.1107 1.0000
10.750 1.4510 0.01716 0.01109 -0.0700 0.1059 1.0000
11.000 1.4671 0.01772 0.01164 -0.0684 0.1007 1.0000
11.250 1.4821 0.01837 0.01227 -0.0667 0.0938 1.0000
11.500 1.4958 0.01909 0.01296 -0.0650 0.0870 1.0000
11.750 1.5094 0.01985 0.01369 -0.0633 0.0788 1.0000
12.000 1.5157 0.02109 0.01479 -0.0608 0.0610 1.0000
12.250 1.5134 0.02294 0.01647 -0.0576 0.0397 1.0000
12.500 1.5205 0.02421 0.01773 -0.0554 0.0352 1.0000
12.750 1.5312 0.02526 0.01881 -0.0538 0.0333 1.0000
13.000 1.5415 0.02637 0.01995 -0.0521 0.0319 1.0000
13.250 1.5501 0.02763 0.02125 -0.0505 0.0306 1.0000
13.500 1.5570 0.02904 0.02270 -0.0487 0.0295 1.0000
13.750 1.5674 0.03020 0.02393 -0.0474 0.0288 1.0000
14.000 1.5771 0.03147 0.02525 -0.0461 0.0281 1.0000
14.250 1.5850 0.03289 0.02672 -0.0447 0.0274 1.0000
14.500 1.5917 0.03445 0.02834 -0.0434 0.0268 1.0000
14.750 1.5960 0.03626 0.03022 -0.0421 0.0261 1.0000
15.000 1.5975 0.03840 0.03242 -0.0407 0.0255 1.0000
15.250 1.6016 0.04034 0.03443 -0.0396 0.0249 1.0000
15.500 1.6077 0.04215 0.03631 -0.0387 0.0246 1.0000
15.750 1.6127 0.04411 0.03835 -0.0379 0.0242 1.0000
16.000 1.6161 0.04629 0.04060 -0.0371 0.0237 1.0000
16.250 1.6185 0.04860 0.04298 -0.0365 0.0232 1.0000
16.500 1.6189 0.05120 0.04566 -0.0359 0.0229 1.0000
16.750 1.6170 0.05415 0.04868 -0.0355 0.0225 1.0000
17.000 1.6120 0.05756 0.05218 -0.0353 0.0221 1.0000
17.250 1.6035 0.06151 0.05623 -0.0353 0.0218 1.0000
17.500 1.5917 0.06602 0.06085 -0.0356 0.0214 1.0000
17.750 1.5898 0.06937 0.06429 -0.0360 0.0212 1.0000
18.000 1.5860 0.07304 0.06805 -0.0364 0.0210 1.0000
18.250 1.5818 0.07677 0.07188 -0.0370 0.0207 1.0000
18.500 1.5763 0.08072 0.07593 -0.0377 0.0204 1.0000
18.750 1.5656 0.08550 0.08081 -0.0388 0.0202 1.0000
19.000 1.5538 0.09051 0.08593 -0.0400 0.0200 1.0000
19.250 1.5409 0.09572 0.09124 -0.0415 0.0198 1.0000
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