GOE 15K AIRFOIL (goe15k-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 15K AIRFOIL (goe15k-il) Reynolds number: 500,000 Max Cl/Cd: 67.7 at α=4° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe15k-il-500000-n5.txt Download as CSV file: xf-goe15k-il-500000-n5.csv |
XFOIL Version 6.96
Calculated polar for: GOE 15K 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
------ -------- --------- --------- -------- -------- --------
-18.000 -0.5038 0.12727 0.12433 -0.1054 0.9700 0.0127
-17.750 -0.5406 0.11581 0.11272 -0.1109 0.9695 0.0125
-17.500 -0.5705 0.10609 0.10290 -0.1160 0.9691 0.0124
-17.250 -0.6106 0.09505 0.09175 -0.1220 0.9686 0.0123
-17.000 -0.6527 0.08404 0.08058 -0.1282 0.9681 0.0122
-16.750 -0.6990 0.07496 0.07138 -0.1308 0.9647 0.0120
-16.500 -0.7516 0.06385 0.06012 -0.1363 0.9619 0.0115
-16.250 -0.7824 0.05483 0.05090 -0.1425 0.9600 0.0115
-16.000 -0.7949 0.04831 0.04416 -0.1481 0.9587 0.0119
-15.750 -0.8060 0.04270 0.03836 -0.1527 0.9576 0.0118
-15.500 -0.8278 0.03931 0.03482 -0.1508 0.9519 0.0120
-15.250 -0.8356 0.03648 0.03185 -0.1505 0.9489 0.0120
-15.000 -0.8336 0.03435 0.02955 -0.1501 0.9472 0.0124
-14.750 -0.8326 0.03224 0.02731 -0.1494 0.9459 0.0128
-14.500 -0.8436 0.03097 0.02593 -0.1446 0.9395 0.0127
-14.250 -0.8412 0.02953 0.02438 -0.1425 0.9364 0.0129
-14.000 -0.8321 0.02831 0.02307 -0.1411 0.9347 0.0136
-13.750 -0.8238 0.02700 0.02163 -0.1394 0.9332 0.0138
-13.500 -0.8236 0.02632 0.02087 -0.1353 0.9279 0.0141
-13.250 -0.8173 0.02542 0.01986 -0.1324 0.9244 0.0149
-13.000 -0.8045 0.02461 0.01893 -0.1306 0.9223 0.0153
-12.750 -0.7915 0.02370 0.01791 -0.1289 0.9207 0.0156
-12.500 -0.7777 0.02272 0.01686 -0.1273 0.9195 0.0164
-12.250 -0.7720 0.02215 0.01622 -0.1237 0.9148 0.0170
-12.000 -0.7612 0.02154 0.01551 -0.1210 0.9113 0.0178
-11.750 -0.7448 0.02088 0.01475 -0.1195 0.9091 0.0186
-11.500 -0.7252 0.02019 0.01399 -0.1186 0.9075 0.0200
-11.250 -0.7032 0.01951 0.01325 -0.1182 0.9063 0.0213
-11.000 -0.6789 0.01889 0.01254 -0.1182 0.9053 0.0229
-10.750 -0.6532 0.01828 0.01187 -0.1185 0.9044 0.0244
-10.500 -0.6507 0.01810 0.01166 -0.1135 0.8979 0.0260
-10.250 -0.6300 0.01768 0.01118 -0.1125 0.8956 0.0280
-10.000 -0.6050 0.01728 0.01075 -0.1125 0.8940 0.0305
-9.750 -0.5770 0.01697 0.01042 -0.1130 0.8927 0.0332
-9.500 -0.5477 0.01664 0.01001 -0.1138 0.8916 0.0357
-9.250 -0.5176 0.01627 0.00961 -0.1149 0.8906 0.0378
-9.000 -0.4855 0.01600 0.00932 -0.1163 0.8897 0.0401
-8.750 -0.4795 0.01599 0.00926 -0.1118 0.8848 0.0418
-8.500 -0.4598 0.01588 0.00909 -0.1103 0.8818 0.0438
-8.250 -0.4347 0.01569 0.00882 -0.1101 0.8799 0.0449
-8.000 -0.4084 0.01533 0.00840 -0.1102 0.8783 0.0463
-7.750 -0.3807 0.01494 0.00799 -0.1106 0.8770 0.0484
-7.500 -0.3510 0.01461 0.00761 -0.1115 0.8758 0.0496
-7.250 -0.3188 0.01434 0.00730 -0.1129 0.8748 0.0516
-7.000 -0.3003 0.01422 0.00714 -0.1112 0.8721 0.0535
-6.750 -0.2929 0.01412 0.00699 -0.1068 0.8681 0.0544
-6.500 -0.2728 0.01400 0.00683 -0.1054 0.8658 0.0554
-6.250 -0.2491 0.01382 0.00660 -0.1048 0.8640 0.0560
-6.000 -0.2232 0.01349 0.00622 -0.1047 0.8625 0.0574
-5.750 -0.1952 0.01315 0.00585 -0.1051 0.8613 0.0589
-5.500 -0.1651 0.01288 0.00554 -0.1060 0.8602 0.0599
-5.250 -0.1332 0.01262 0.00527 -0.1073 0.8593 0.0622
-5.000 -0.0998 0.01240 0.00500 -0.1089 0.8584 0.0632
-4.750 -0.0994 0.01242 0.00503 -0.1028 0.8550 0.0643
-4.500 -0.0856 0.01237 0.00495 -0.0999 0.8524 0.0653
-4.250 -0.0657 0.01228 0.00483 -0.0983 0.8504 0.0665
-4.000 -0.0420 0.01216 0.00469 -0.0976 0.8487 0.0680
-3.750 -0.0160 0.01203 0.00454 -0.0975 0.8472 0.0691
-3.500 0.0122 0.01185 0.00437 -0.0978 0.8460 0.0743
-3.250 0.0421 0.01169 0.00423 -0.0986 0.8450 0.0808
-3.000 0.0739 0.01139 0.00407 -0.0999 0.8442 0.1118
-2.750 0.1065 0.01105 0.00395 -0.1015 0.8434 0.1695
-2.500 0.1400 0.01083 0.00385 -0.1032 0.8427 0.2051
-2.250 0.1428 0.01088 0.00397 -0.0977 0.8399 0.2213
-2.000 0.1511 0.01085 0.00407 -0.0935 0.8373 0.2531
-1.750 0.1681 0.01078 0.00410 -0.0914 0.8350 0.2820
-1.500 0.1900 0.01069 0.00412 -0.0903 0.8333 0.3105
-1.250 0.2144 0.01061 0.00411 -0.0898 0.8320 0.3381
-1.000 0.2405 0.01051 0.00411 -0.0897 0.8308 0.3661
-0.750 0.2681 0.01036 0.00408 -0.0900 0.8297 0.4023
-0.500 0.3014 0.01014 0.00398 -0.0915 0.8280 0.4405
-0.250 0.3339 0.00982 0.00388 -0.0929 0.8262 0.5034
0.000 0.3109 0.00995 0.00418 -0.0814 0.8201 0.5428
0.500 0.5290 0.01022 0.00573 -0.1184 0.8229 0.9158
0.750 0.5471 0.01053 0.00606 -0.1161 0.8195 0.9266
1.000 0.5750 0.01070 0.00622 -0.1162 0.8166 0.9322
1.250 0.6062 0.01089 0.00641 -0.1171 0.8147 0.9387
1.500 0.6358 0.01101 0.00653 -0.1176 0.8128 0.9436
1.750 0.6739 0.01104 0.00655 -0.1201 0.8094 0.9455
2.000 0.6776 0.01139 0.00694 -0.1147 0.8045 0.9526
2.250 0.7030 0.01149 0.00703 -0.1142 0.7987 0.9558
2.500 0.7467 0.01142 0.00696 -0.1180 0.7953 0.9570
2.750 0.7501 0.01172 0.00731 -0.1126 0.7868 0.9619
3.000 0.7739 0.01176 0.00731 -0.1117 0.7793 0.9656
3.250 0.7924 0.01197 0.00758 -0.1098 0.7699 0.9683
3.500 0.8094 0.01215 0.00775 -0.1075 0.7536 0.9723
3.750 0.8217 0.01239 0.00798 -0.1042 0.7373 0.9762
4.000 0.8449 0.01248 0.00800 -0.1033 0.7077 0.9783
4.250 0.8457 0.01309 0.00823 -0.0976 0.6365 0.9826
4.500 0.8438 0.01396 0.00883 -0.0916 0.5841 0.9865
4.750 0.8367 0.01500 0.00953 -0.0849 0.5099 0.9891
5.000 0.8292 0.01634 0.01050 -0.0785 0.4376 0.9927
5.250 0.8399 0.01706 0.01109 -0.0757 0.4073 0.9947
5.500 0.8547 0.01757 0.01147 -0.0738 0.3784 0.9959
5.750 0.8709 0.01805 0.01185 -0.0722 0.3494 0.9973
6.000 0.8867 0.01865 0.01229 -0.0706 0.3121 0.9989
6.250 0.8993 0.01942 0.01282 -0.0685 0.2610 1.0000
6.500 0.9044 0.02018 0.01339 -0.0646 0.2229 1.0000
6.750 0.9111 0.02090 0.01394 -0.0612 0.1891 1.0000
7.000 0.9246 0.02134 0.01435 -0.0589 0.1774 1.0000
7.250 0.9340 0.02199 0.01487 -0.0560 0.1531 1.0000
7.500 0.9466 0.02250 0.01533 -0.0536 0.1382 1.0000
7.750 0.9577 0.02312 0.01582 -0.0510 0.1145 1.0000
8.000 0.9709 0.02363 0.01630 -0.0488 0.1020 1.0000
8.250 0.9839 0.02418 0.01680 -0.0466 0.0911 1.0000
8.750 1.0114 0.02520 0.01779 -0.0426 0.0777 1.0000
9.000 1.0247 0.02577 0.01833 -0.0405 0.0703 1.0000
9.250 1.0389 0.02629 0.01886 -0.0386 0.0659 1.0000
9.500 1.0520 0.02689 0.01944 -0.0365 0.0608 1.0000
9.750 1.0665 0.02740 0.01999 -0.0347 0.0570 1.0000
10.000 1.0807 0.02796 0.02057 -0.0329 0.0534 1.0000
10.250 1.0942 0.02856 0.02118 -0.0310 0.0482 1.0000
10.500 1.1070 0.02921 0.02181 -0.0291 0.0416 1.0000
10.750 1.1199 0.02987 0.02247 -0.0272 0.0367 1.0000
11.000 1.1321 0.03059 0.02317 -0.0252 0.0319 1.0000
11.250 1.1441 0.03132 0.02391 -0.0233 0.0282 1.0000
11.500 1.1547 0.03216 0.02476 -0.0211 0.0243 1.0000
11.750 1.1669 0.03290 0.02555 -0.0193 0.0232 1.0000
12.000 1.1786 0.03369 0.02636 -0.0174 0.0215 1.0000
12.250 1.1888 0.03461 0.02731 -0.0154 0.0200 1.0000
12.500 1.2003 0.03543 0.02818 -0.0136 0.0185 1.0000
12.750 1.2105 0.03637 0.02917 -0.0116 0.0178 1.0000
13.000 1.2192 0.03744 0.03028 -0.0096 0.0163 1.0000
13.250 1.2289 0.03843 0.03133 -0.0077 0.0162 1.0000
13.500 1.2388 0.03942 0.03240 -0.0059 0.0152 1.0000
13.750 1.2482 0.04047 0.03350 -0.0041 0.0142 1.0000
14.000 1.2563 0.04163 0.03473 -0.0022 0.0140 1.0000
14.250 1.2645 0.04281 0.03597 -0.0004 0.0138 1.0000
14.500 1.2699 0.04424 0.03745 0.0016 0.0131 1.0000
14.750 1.2756 0.04567 0.03896 0.0035 0.0130 1.0000
15.000 1.2830 0.04700 0.04037 0.0052 0.0122 1.0000
15.250 1.2888 0.04845 0.04192 0.0069 0.0120 1.0000
15.500 1.2937 0.05002 0.04357 0.0086 0.0116 1.0000
15.750 1.3012 0.05137 0.04497 0.0099 0.0109 1.0000
16.000 1.2998 0.05361 0.04729 0.0119 0.0107 1.0000
16.250 1.3022 0.05554 0.04931 0.0134 0.0105 1.0000
16.500 1.3054 0.05743 0.05129 0.0147 0.0104 1.0000
16.750 1.3056 0.05968 0.05366 0.0162 0.0100 1.0000
17.000 1.3109 0.06144 0.05550 0.0172 0.0092 1.0000
17.250 1.3074 0.06418 0.05836 0.0185 0.0097 1.0000
17.500 1.3045 0.06697 0.06127 0.0195 0.0095 1.0000
17.750 1.3079 0.06907 0.06346 0.0201 0.0092 1.0000
18.000 1.2981 0.07283 0.06735 0.0209 0.0094 1.0000
18.250 1.2943 0.07599 0.07062 0.0214 0.0089 1.0000
18.500 1.2885 0.07945 0.07420 0.0216 0.0092 1.0000
18.750 1.2847 0.08275 0.07759 0.0216 0.0088 1.0000
19.000 1.2778 0.08660 0.08157 0.0213 0.0088 1.0000
19.250 1.2661 0.09125 0.08634 0.0207 0.0087 1.0000
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