GOE 8K AIRFOIL (goe08k-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 8K AIRFOIL (goe08k-il) Reynolds number: 500,000 Max Cl/Cd: 96.16 at α=4.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe08k-il-500000-n5.txt Download as CSV file: xf-goe08k-il-500000-n5.csv |
XFOIL Version 6.96
Calculated polar for: GOE 8K AIRFOIL
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.500 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-12.250 -0.2508 0.03569 0.03235 -0.2165 0.9070 0.0093
-12.000 -0.3006 0.03198 0.02838 -0.2086 0.8987 0.0093
-11.750 -0.3113 0.02898 0.02507 -0.2060 0.8954 0.0093
-11.500 -0.3270 0.02767 0.02360 -0.1994 0.8908 0.0095
-11.250 -0.3432 0.02650 0.02228 -0.1921 0.8855 0.0095
-11.000 -0.3396 0.02482 0.02037 -0.1893 0.8825 0.0098
-10.750 -0.3249 0.02321 0.01851 -0.1885 0.8806 0.0100
-10.500 -0.3248 0.02221 0.01731 -0.1839 0.8771 0.0103
-10.250 -0.3370 0.02175 0.01677 -0.1762 0.8718 0.0103
-10.000 -0.3265 0.02080 0.01563 -0.1735 0.8691 0.0108
-9.750 -0.3099 0.01988 0.01457 -0.1722 0.8672 0.0111
-9.500 -0.2863 0.01903 0.01358 -0.1722 0.8657 0.0116
-9.250 -0.2583 0.01824 0.01263 -0.1732 0.8645 0.0122
-9.000 -0.2826 0.01825 0.01262 -0.1621 0.8577 0.0123
-8.750 -0.2686 0.01767 0.01190 -0.1597 0.8549 0.0128
-8.500 -0.2483 0.01700 0.01108 -0.1586 0.8528 0.0132
-8.250 -0.2228 0.01633 0.01029 -0.1588 0.8514 0.0141
-8.000 -0.1937 0.01576 0.00960 -0.1596 0.8501 0.0149
-7.750 -0.2057 0.01578 0.00960 -0.1511 0.8446 0.0153
-7.500 -0.1925 0.01545 0.00918 -0.1483 0.8414 0.0162
-7.250 -0.1722 0.01502 0.00864 -0.1471 0.8392 0.0171
-7.000 -0.1465 0.01457 0.00814 -0.1470 0.8375 0.0190
-6.750 -0.1175 0.01413 0.00758 -0.1477 0.8361 0.0204
-6.500 -0.1075 0.01397 0.00739 -0.1440 0.8326 0.0222
-6.250 -0.1033 0.01390 0.00731 -0.1390 0.8280 0.0234
-6.000 -0.0830 0.01372 0.00708 -0.1377 0.8253 0.0260
-5.750 -0.0561 0.01352 0.00685 -0.1378 0.8234 0.0284
-5.500 -0.0246 0.01347 0.00677 -0.1389 0.8220 0.0316
-5.250 0.0082 0.01329 0.00650 -0.1402 0.8208 0.0346
-5.000 0.0030 0.01344 0.00666 -0.1332 0.8154 0.0356
-4.750 0.0217 0.01355 0.00677 -0.1314 0.8123 0.0375
-4.500 0.0467 0.01357 0.00675 -0.1310 0.8101 0.0400
-4.250 0.0749 0.01340 0.00650 -0.1314 0.8084 0.0422
-4.000 0.1056 0.01327 0.00628 -0.1323 0.8070 0.0439
-3.750 0.1217 0.01338 0.00635 -0.1299 0.8040 0.0447
-3.500 0.1276 0.01318 0.00614 -0.1254 0.7996 0.0462
-3.250 0.1468 0.01300 0.00594 -0.1238 0.7968 0.0475
-3.000 0.1733 0.01286 0.00578 -0.1238 0.7947 0.0493
-2.750 0.2017 0.01264 0.00551 -0.1242 0.7932 0.0508
-2.500 0.2328 0.01243 0.00526 -0.1252 0.7919 0.0526
-2.250 0.2370 0.01250 0.00531 -0.1202 0.7878 0.0534
-2.000 0.2521 0.01246 0.00524 -0.1177 0.7846 0.0542
-1.750 0.2734 0.01237 0.00512 -0.1165 0.7823 0.0550
-1.500 0.2991 0.01225 0.00497 -0.1163 0.7805 0.0556
-1.250 0.3273 0.01211 0.00479 -0.1167 0.7790 0.0561
-1.000 0.3565 0.01186 0.00451 -0.1173 0.7777 0.0570
-0.750 0.3707 0.01187 0.00451 -0.1145 0.7748 0.0572
-0.500 0.3809 0.01192 0.00456 -0.1110 0.7713 0.0582
-0.250 0.4000 0.01188 0.00451 -0.1094 0.7686 0.0592
0.000 0.4243 0.01182 0.00443 -0.1089 0.7668 0.0600
0.250 0.4518 0.01172 0.00433 -0.1091 0.7653 0.0611
0.500 0.4816 0.01163 0.00422 -0.1098 0.7640 0.0631
0.750 0.5133 0.01154 0.00412 -0.1111 0.7628 0.0648
1.000 0.5272 0.01167 0.00427 -0.1083 0.7602 0.0649
1.250 0.5408 0.01181 0.00442 -0.1055 0.7573 0.0675
1.500 0.5597 0.01189 0.00450 -0.1040 0.7545 0.0684
1.750 0.5837 0.01188 0.00449 -0.1034 0.7517 0.0724
2.000 0.6144 0.01177 0.00441 -0.1044 0.7496 0.0830
2.500 0.9493 0.01065 0.00583 -0.1714 0.7535 1.0000
2.750 0.9723 0.01071 0.00588 -0.1708 0.7509 1.0000
3.000 1.0019 0.01069 0.00583 -0.1715 0.7484 1.0000
3.250 1.0171 0.01086 0.00602 -0.1691 0.7455 1.0000
3.500 1.0250 0.01112 0.00631 -0.1651 0.7409 1.0000
3.750 1.0433 0.01124 0.00643 -0.1634 0.7370 1.0000
4.000 1.0705 0.01125 0.00643 -0.1637 0.7339 1.0000
4.250 1.0924 0.01136 0.00657 -0.1628 0.7314 1.0000
4.500 1.0915 0.01176 0.00700 -0.1569 0.7235 1.0000
4.750 1.1175 0.01174 0.00695 -0.1568 0.7172 1.0000
5.000 1.1215 0.01215 0.00741 -0.1521 0.7113 1.0000
5.250 1.1377 0.01233 0.00761 -0.1500 0.7051 1.0000
5.500 1.1508 0.01260 0.00791 -0.1472 0.6982 1.0000
5.750 1.1624 0.01290 0.00821 -0.1442 0.6890 1.0000
6.000 1.1718 0.01330 0.00864 -0.1408 0.6807 1.0000
6.250 1.1822 0.01366 0.00900 -0.1375 0.6691 1.0000
6.500 1.1853 0.01425 0.00958 -0.1329 0.6509 1.0000
6.750 1.1810 0.01509 0.01030 -0.1268 0.6152 1.0000
7.000 1.1835 0.01585 0.01096 -0.1222 0.5878 1.0000
7.250 1.1703 0.01725 0.01213 -0.1149 0.5458 1.0000
7.500 1.1531 0.01900 0.01360 -0.1071 0.5022 1.0000
7.750 1.1450 0.02051 0.01494 -0.1012 0.4645 1.0000
8.000 1.1405 0.02195 0.01622 -0.0962 0.4288 1.0000
8.250 1.1375 0.02341 0.01751 -0.0915 0.3929 1.0000
8.500 1.1345 0.02494 0.01887 -0.0871 0.3532 1.0000
8.750 1.1336 0.02641 0.02015 -0.0831 0.3139 1.0000
9.000 1.1259 0.02832 0.02176 -0.0782 0.2581 1.0000
9.250 1.1225 0.03005 0.02322 -0.0741 0.2111 1.0000
9.500 1.1234 0.03157 0.02453 -0.0708 0.1702 1.0000
10.000 1.1248 0.03477 0.02727 -0.0644 0.0854 1.0000
10.250 1.1325 0.03598 0.02841 -0.0622 0.0690 1.0000
10.500 1.1417 0.03712 0.02951 -0.0603 0.0557 1.0000
11.000 1.1573 0.03962 0.03189 -0.0563 0.0272 1.0000
11.250 1.1674 0.04075 0.03303 -0.0546 0.0224 1.0000
11.500 1.1777 0.04187 0.03418 -0.0529 0.0198 1.0000
11.750 1.1881 0.04300 0.03536 -0.0514 0.0181 1.0000
12.000 1.1982 0.04417 0.03656 -0.0498 0.0161 1.0000
12.250 1.2074 0.04543 0.03784 -0.0482 0.0147 1.0000
12.500 1.2179 0.04659 0.03907 -0.0468 0.0139 1.0000
12.750 1.2271 0.04787 0.04042 -0.0453 0.0133 1.0000
13.000 1.2362 0.04917 0.04178 -0.0438 0.0124 1.0000
13.250 1.2441 0.05058 0.04323 -0.0422 0.0118 1.0000
13.500 1.2512 0.05209 0.04480 -0.0407 0.0113 1.0000
13.750 1.2606 0.05341 0.04619 -0.0394 0.0106 1.0000
14.000 1.2676 0.05498 0.04783 -0.0379 0.0101 1.0000
14.250 1.2752 0.05649 0.04938 -0.0366 0.0095 1.0000
14.500 1.2786 0.05841 0.05136 -0.0350 0.0090 1.0000
14.750 1.2845 0.06012 0.05319 -0.0336 0.0086 1.0000
15.000 1.2922 0.06167 0.05481 -0.0325 0.0083 1.0000
15.250 1.2955 0.06369 0.05692 -0.0311 0.0081 1.0000
15.500 1.3006 0.06555 0.05884 -0.0299 0.0078 1.0000
15.750 1.3038 0.06763 0.06101 -0.0286 0.0076 1.0000
16.000 1.3073 0.06971 0.06315 -0.0275 0.0074 1.0000
16.250 1.3071 0.07222 0.06574 -0.0262 0.0069 1.0000
16.500 1.3120 0.07418 0.06778 -0.0254 0.0069 1.0000
16.750 1.3127 0.07665 0.07036 -0.0243 0.0068 1.0000
17.000 1.3134 0.07919 0.07301 -0.0234 0.0065 1.0000
17.250 1.3162 0.08149 0.07542 -0.0227 0.0062 1.0000
17.500 1.3147 0.08434 0.07837 -0.0219 0.0061 1.0000
17.750 1.3150 0.08700 0.08113 -0.0213 0.0060 1.0000
18.000 1.3176 0.08945 0.08366 -0.0209 0.0059 1.0000
18.250 1.3174 0.09223 0.08652 -0.0206 0.0056 1.0000
18.500 1.3162 0.09517 0.08956 -0.0203 0.0056 1.0000
18.750 1.3120 0.09856 0.09304 -0.0201 0.0054 1.0000
19.000 1.3094 0.10178 0.09635 -0.0201 0.0053 1.0000
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