GOE 627 AIRFOIL (goe627-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 627 AIRFOIL (goe627-il) Reynolds number: 1,000,000 Max Cl/Cd: 90.53 at α=7.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe627-il-1000000-n5.txt Download as CSV file: xf-goe627-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: GOE 627 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
------ -------- --------- --------- -------- -------- --------
-18.250 -0.9957 0.06578 0.06273 -0.0874 1.0000 0.0135
-18.000 -1.0261 0.05689 0.05367 -0.0938 0.9996 0.0137
-17.750 -1.0442 0.04945 0.04604 -0.1002 0.9989 0.0137
-17.500 -1.0511 0.04421 0.04065 -0.1048 0.9980 0.0138
-17.250 -1.0539 0.03995 0.03624 -0.1084 0.9968 0.0140
-17.000 -1.0510 0.03671 0.03288 -0.1110 0.9953 0.0141
-16.750 -1.0453 0.03400 0.03004 -0.1130 0.9937 0.0143
-16.500 -1.0404 0.03185 0.02781 -0.1136 0.9919 0.0144
-16.250 -1.0309 0.03017 0.02607 -0.1140 0.9901 0.0146
-16.000 -1.0188 0.02869 0.02452 -0.1145 0.9882 0.0148
-15.750 -1.0028 0.02753 0.02331 -0.1148 0.9867 0.0150
-15.500 -0.9857 0.02649 0.02222 -0.1151 0.9855 0.0153
-15.250 -0.9678 0.02544 0.02112 -0.1155 0.9844 0.0155
-15.000 -0.9476 0.02455 0.02016 -0.1159 0.9834 0.0157
-14.750 -0.9327 0.02375 0.01931 -0.1150 0.9812 0.0160
-14.500 -0.9183 0.02292 0.01841 -0.1140 0.9784 0.0162
-14.250 -0.8997 0.02215 0.01757 -0.1136 0.9764 0.0165
-14.000 -0.8793 0.02143 0.01677 -0.1134 0.9749 0.0168
-13.750 -0.8566 0.02076 0.01603 -0.1134 0.9736 0.0170
-13.500 -0.8338 0.02005 0.01525 -0.1134 0.9725 0.0172
-13.250 -0.8084 0.01950 0.01468 -0.1137 0.9715 0.0176
-13.000 -0.7873 0.01906 0.01422 -0.1130 0.9692 0.0178
-12.750 -0.7682 0.01863 0.01376 -0.1118 0.9660 0.0180
-12.500 -0.7425 0.01829 0.01339 -0.1118 0.9640 0.0183
-12.250 -0.7160 0.01781 0.01287 -0.1120 0.9623 0.0186
-12.000 -0.6883 0.01733 0.01235 -0.1124 0.9606 0.0189
-11.750 -0.6574 0.01680 0.01177 -0.1135 0.9588 0.0192
-11.500 -0.6332 0.01638 0.01129 -0.1131 0.9546 0.0196
-11.250 -0.6146 0.01598 0.01083 -0.1114 0.9487 0.0198
-11.000 -0.5881 0.01557 0.01036 -0.1114 0.9457 0.0201
-10.750 -0.5596 0.01516 0.00990 -0.1118 0.9434 0.0204
-10.500 -0.5406 0.01479 0.00950 -0.1102 0.9395 0.0207
-10.250 -0.5230 0.01447 0.00917 -0.1083 0.9346 0.0210
-10.000 -0.4984 0.01422 0.00890 -0.1077 0.9309 0.0213
-9.750 -0.4716 0.01391 0.00855 -0.1076 0.9278 0.0216
-9.500 -0.4494 0.01363 0.00825 -0.1065 0.9238 0.0219
-9.250 -0.4305 0.01337 0.00796 -0.1046 0.9185 0.0223
-9.000 -0.4065 0.01309 0.00765 -0.1039 0.9139 0.0226
-8.750 -0.3799 0.01278 0.00728 -0.1036 0.9100 0.0230
-8.500 -0.3608 0.01255 0.00702 -0.1018 0.9038 0.0233
-8.250 -0.3375 0.01227 0.00670 -0.1008 0.8974 0.0235
-8.000 -0.3133 0.01206 0.00644 -0.0999 0.8894 0.0238
-7.750 -0.2914 0.01169 0.00600 -0.0987 0.8787 0.0241
-7.500 -0.2706 0.01137 0.00565 -0.0972 0.8663 0.0245
-7.250 -0.2480 0.01113 0.00535 -0.0960 0.8545 0.0248
-7.000 -0.2256 0.01093 0.00509 -0.0947 0.8394 0.0251
-6.750 -0.2034 0.01079 0.00488 -0.0934 0.8235 0.0255
-6.500 -0.1824 0.01065 0.00466 -0.0918 0.8043 0.0259
-6.250 -0.1620 0.01052 0.00443 -0.0901 0.7854 0.0263
-6.000 -0.1416 0.01041 0.00424 -0.0884 0.7669 0.0266
-5.750 -0.1218 0.01033 0.00406 -0.0866 0.7466 0.0269
-5.500 -0.1030 0.01027 0.00389 -0.0845 0.7238 0.0272
-5.250 -0.0833 0.01022 0.00374 -0.0826 0.7021 0.0275
-5.000 -0.0645 0.01021 0.00361 -0.0806 0.6771 0.0277
-4.750 -0.0463 0.01015 0.00343 -0.0784 0.6534 0.0282
-4.500 -0.0272 0.01008 0.00327 -0.0765 0.6307 0.0288
-4.250 -0.0064 0.01001 0.00314 -0.0748 0.6139 0.0293
-4.000 0.0148 0.00996 0.00302 -0.0733 0.5985 0.0297
-3.750 0.0360 0.00992 0.00291 -0.0718 0.5816 0.0302
-3.500 0.0574 0.00989 0.00282 -0.0703 0.5650 0.0308
-3.250 0.0794 0.00986 0.00272 -0.0689 0.5493 0.0314
-3.000 0.1012 0.00984 0.00264 -0.0675 0.5332 0.0319
-2.750 0.1226 0.00984 0.00256 -0.0661 0.5153 0.0325
-2.500 0.1432 0.00984 0.00249 -0.0644 0.4957 0.0336
-2.250 0.1639 0.00987 0.00244 -0.0628 0.4752 0.0349
-2.000 0.1849 0.00990 0.00239 -0.0613 0.4556 0.0364
-1.750 0.2060 0.00992 0.00235 -0.0598 0.4390 0.0392
-1.500 0.2271 0.00993 0.00232 -0.0583 0.4241 0.0452
-1.250 0.2474 0.00985 0.00229 -0.0566 0.4102 0.0702
-1.000 0.2668 0.00973 0.00224 -0.0549 0.3983 0.1077
-0.750 0.2849 0.00961 0.00221 -0.0528 0.3869 0.1550
-0.500 0.3031 0.00951 0.00219 -0.0508 0.3753 0.1912
-0.250 0.3206 0.00937 0.00219 -0.0486 0.3656 0.2483
0.000 0.3383 0.00929 0.00220 -0.0465 0.3542 0.2980
0.250 0.3568 0.00920 0.00222 -0.0445 0.3433 0.3477
0.500 0.3739 0.00908 0.00225 -0.0423 0.3336 0.4097
0.750 0.3904 0.00893 0.00229 -0.0400 0.3252 0.4854
1.000 0.4058 0.00878 0.00236 -0.0374 0.3176 0.5675
1.250 0.4208 0.00863 0.00243 -0.0346 0.3107 0.6475
1.500 0.4370 0.00860 0.00252 -0.0321 0.3034 0.7010
1.750 0.4487 0.00843 0.00262 -0.0285 0.2981 0.7837
2.000 0.4656 0.00842 0.00273 -0.0261 0.2916 0.8329
2.250 0.4897 0.00842 0.00289 -0.0252 0.2848 0.8928
2.500 0.5253 0.00855 0.00303 -0.0269 0.2779 0.9160
2.750 0.5770 0.00880 0.00324 -0.0323 0.2685 0.9383
3.000 0.6327 0.00905 0.00345 -0.0385 0.2608 0.9503
3.250 0.6784 0.00930 0.00364 -0.0425 0.2542 0.9586
3.500 0.7157 0.00950 0.00380 -0.0447 0.2499 0.9643
3.750 0.7463 0.00968 0.00395 -0.0454 0.2458 0.9710
4.000 0.7799 0.00990 0.00413 -0.0468 0.2410 0.9753
4.250 0.8080 0.01013 0.00432 -0.0470 0.2363 0.9810
4.500 0.8403 0.01030 0.00448 -0.0481 0.2331 0.9842
4.750 0.8720 0.01048 0.00463 -0.0492 0.2296 0.9864
5.000 0.9022 0.01069 0.00480 -0.0500 0.2253 0.9891
5.250 0.9310 0.01092 0.00499 -0.0505 0.2214 0.9919
5.500 0.9605 0.01110 0.00517 -0.0511 0.2189 0.9944
5.750 0.9920 0.01128 0.00534 -0.0521 0.2164 0.9965
6.000 1.0234 0.01147 0.00552 -0.0532 0.2135 0.9982
6.250 1.0546 0.01169 0.00571 -0.0543 0.2104 0.9995
6.500 1.0759 0.01189 0.00590 -0.0533 0.2072 1.0000
6.750 1.0889 0.01208 0.00607 -0.0505 0.2042 1.0000
7.000 1.1047 0.01222 0.00623 -0.0483 0.2029 1.0000
7.250 1.1207 0.01238 0.00640 -0.0462 0.2014 1.0000
7.500 1.1371 0.01256 0.00660 -0.0441 0.1998 1.0000
7.750 1.1539 0.01276 0.00680 -0.0422 0.1977 1.0000
8.000 1.1703 0.01299 0.00702 -0.0403 0.1948 1.0000
8.250 1.1864 0.01326 0.00728 -0.0383 0.1920 1.0000
8.500 1.2031 0.01352 0.00754 -0.0365 0.1895 1.0000
8.750 1.2217 0.01374 0.00778 -0.0350 0.1882 1.0000
9.000 1.2400 0.01398 0.00804 -0.0336 0.1866 1.0000
9.250 1.2581 0.01424 0.00833 -0.0321 0.1846 1.0000
9.500 1.2762 0.01452 0.00862 -0.0307 0.1824 1.0000
9.750 1.2940 0.01483 0.00894 -0.0293 0.1802 1.0000
10.000 1.3111 0.01518 0.00929 -0.0278 0.1777 1.0000
10.250 1.3282 0.01555 0.00967 -0.0263 0.1752 1.0000
10.500 1.3470 0.01585 0.01001 -0.0252 0.1737 1.0000
10.750 1.3650 0.01620 0.01038 -0.0240 0.1708 1.0000
11.000 1.3810 0.01665 0.01082 -0.0225 0.1653 1.0000
11.250 1.3975 0.01710 0.01128 -0.0212 0.1625 1.0000
11.500 1.4141 0.01755 0.01174 -0.0199 0.1580 1.0000
11.750 1.4291 0.01810 0.01228 -0.0185 0.1522 1.0000
12.000 1.4429 0.01873 0.01289 -0.0170 0.1454 1.0000
12.250 1.4571 0.01934 0.01350 -0.0155 0.1404 1.0000
12.500 1.4676 0.02018 0.01430 -0.0138 0.1310 1.0000
12.750 1.4757 0.02119 0.01526 -0.0118 0.1206 1.0000
13.000 1.4851 0.02215 0.01620 -0.0101 0.1141 1.0000
13.250 1.4913 0.02333 0.01735 -0.0081 0.1048 1.0000
13.500 1.5012 0.02434 0.01836 -0.0067 0.1007 1.0000
13.750 1.5081 0.02556 0.01958 -0.0051 0.0950 1.0000
14.000 1.5163 0.02674 0.02079 -0.0037 0.0914 1.0000
14.250 1.5263 0.02784 0.02193 -0.0025 0.0890 1.0000
14.500 1.5339 0.02916 0.02327 -0.0013 0.0862 1.0000
14.750 1.5402 0.03062 0.02475 -0.0002 0.0834 1.0000
15.000 1.5467 0.03211 0.02629 0.0009 0.0805 1.0000
15.250 1.5541 0.03358 0.02781 0.0017 0.0784 1.0000
15.500 1.5592 0.03529 0.02955 0.0026 0.0760 1.0000
15.750 1.5626 0.03721 0.03151 0.0034 0.0738 1.0000
16.000 1.5665 0.03914 0.03349 0.0040 0.0713 1.0000
16.250 1.5709 0.04108 0.03550 0.0045 0.0693 1.0000
16.500 1.5686 0.04372 0.03816 0.0051 0.0652 1.0000
16.750 1.5683 0.04625 0.04075 0.0054 0.0629 1.0000
17.000 1.5615 0.04953 0.04406 0.0056 0.0573 1.0000
17.250 1.5492 0.05350 0.04806 0.0057 0.0509 1.0000
17.500 1.5267 0.05884 0.05341 0.0053 0.0431 1.0000
17.750 1.5023 0.06462 0.05926 0.0046 0.0364 1.0000
18.000 1.4688 0.07181 0.06653 0.0033 0.0289 1.0000
18.250 1.4351 0.07935 0.07416 0.0016 0.0231 1.0000
18.500 1.4073 0.08632 0.08124 -0.0002 0.0202 1.0000
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