GOE 15K AIRFOIL (goe15k-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 15K AIRFOIL (goe15k-il) Reynolds number: 1,000,000 Max Cl/Cd: 83.13 at α=1.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe15k-il-1000000-n5.txt Download as CSV file: xf-goe15k-il-1000000-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 = 1.000 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-18.500 -0.6322 0.09604 0.09329 -0.1326 0.9696 0.0086
-18.250 -0.7126 0.07994 0.07696 -0.1408 0.9692 0.0083
-18.000 -0.7733 0.06717 0.06395 -0.1480 0.9687 0.0081
-17.750 -0.8153 0.05691 0.05349 -0.1547 0.9683 0.0079
-17.500 -0.8487 0.04739 0.04374 -0.1622 0.9679 0.0077
-17.250 -0.8829 0.04268 0.03890 -0.1604 0.9626 0.0079
-17.000 -0.8884 0.03904 0.03513 -0.1623 0.9609 0.0079
-16.750 -0.8991 0.03524 0.03119 -0.1637 0.9596 0.0082
-16.500 -0.9001 0.03273 0.02855 -0.1640 0.9586 0.0078
-16.250 -0.8978 0.03065 0.02637 -0.1639 0.9578 0.0082
-16.000 -0.8914 0.02899 0.02464 -0.1637 0.9572 0.0088
-15.750 -0.9119 0.02781 0.02335 -0.1569 0.9503 0.0085
-15.500 -0.9080 0.02642 0.02187 -0.1551 0.9483 0.0087
-15.250 -0.8986 0.02527 0.02063 -0.1539 0.9470 0.0088
-15.000 -0.8867 0.02423 0.01951 -0.1527 0.9459 0.0094
-14.750 -0.8900 0.02368 0.01891 -0.1477 0.9398 0.0097
-14.500 -0.8849 0.02276 0.01790 -0.1449 0.9365 0.0097
-14.250 -0.8749 0.02189 0.01693 -0.1428 0.9345 0.0097
-14.000 -0.8582 0.02120 0.01615 -0.1417 0.9332 0.0100
-13.750 -0.8548 0.02055 0.01544 -0.1379 0.9281 0.0104
-13.500 -0.8430 0.01990 0.01473 -0.1357 0.9245 0.0107
-13.250 -0.8271 0.01913 0.01389 -0.1344 0.9224 0.0114
-13.000 -0.8063 0.01851 0.01320 -0.1339 0.9207 0.0116
-12.750 -0.7832 0.01790 0.01252 -0.1338 0.9193 0.0120
-12.500 -0.7671 0.01739 0.01194 -0.1322 0.9156 0.0124
-12.250 -0.7490 0.01682 0.01130 -0.1310 0.9119 0.0132
-12.000 -0.7253 0.01625 0.01067 -0.1309 0.9093 0.0138
-11.750 -0.6979 0.01570 0.01006 -0.1316 0.9072 0.0145
-11.500 -0.6696 0.01518 0.00949 -0.1326 0.9052 0.0160
-11.250 -0.6496 0.01474 0.00900 -0.1315 0.9012 0.0170
-11.000 -0.6288 0.01435 0.00856 -0.1306 0.8972 0.0184
-10.750 -0.6036 0.01398 0.00813 -0.1307 0.8940 0.0194
-10.500 -0.5762 0.01355 0.00766 -0.1312 0.8913 0.0212
-10.250 -0.5501 0.01319 0.00727 -0.1314 0.8885 0.0236
-10.000 -0.5344 0.01293 0.00700 -0.1293 0.8841 0.0263
-9.750 -0.5123 0.01268 0.00671 -0.1285 0.8805 0.0279
-9.500 -0.4865 0.01243 0.00647 -0.1285 0.8775 0.0317
-9.250 -0.4578 0.01219 0.00621 -0.1292 0.8751 0.0343
-9.000 -0.4369 0.01204 0.00602 -0.1280 0.8720 0.0359
-8.750 -0.4198 0.01189 0.00588 -0.1260 0.8685 0.0381
-8.500 -0.3984 0.01174 0.00571 -0.1249 0.8653 0.0402
-8.250 -0.3740 0.01160 0.00556 -0.1245 0.8627 0.0420
-8.000 -0.3475 0.01147 0.00538 -0.1246 0.8604 0.0433
-7.500 -0.3043 0.01122 0.00505 -0.1224 0.8555 0.0446
-7.250 -0.2857 0.01115 0.00495 -0.1205 0.8526 0.0451
-7.000 -0.2656 0.01098 0.00475 -0.1191 0.8500 0.0468
-6.750 -0.2433 0.01077 0.00451 -0.1182 0.8477 0.0483
-6.500 -0.2188 0.01061 0.00434 -0.1178 0.8458 0.0498
-6.250 -0.1925 0.01049 0.00420 -0.1177 0.8440 0.0513
-6.000 -0.1641 0.01034 0.00403 -0.1182 0.8424 0.0523
-5.750 -0.1473 0.01025 0.00392 -0.1159 0.8405 0.0530
-5.500 -0.1286 0.01014 0.00378 -0.1141 0.8387 0.0534
-5.250 -0.1081 0.01005 0.00368 -0.1126 0.8368 0.0544
-5.000 -0.0862 0.00994 0.00355 -0.1115 0.8350 0.0545
-4.750 -0.0630 0.00984 0.00343 -0.1107 0.8333 0.0554
-4.500 -0.0387 0.00975 0.00332 -0.1102 0.8317 0.0558
-4.250 -0.0132 0.00966 0.00321 -0.1099 0.8303 0.0561
-4.000 0.0137 0.00952 0.00305 -0.1099 0.8290 0.0581
-3.750 0.0422 0.00943 0.00294 -0.1104 0.8277 0.0587
-3.500 0.0712 0.00931 0.00283 -0.1109 0.8262 0.0618
-3.250 0.0889 0.00925 0.00278 -0.1087 0.8247 0.0629
-3.000 0.1091 0.00918 0.00273 -0.1072 0.8233 0.0658
-2.750 0.1303 0.00911 0.00268 -0.1059 0.8219 0.0690
-2.500 0.1526 0.00901 0.00263 -0.1049 0.8204 0.0790
-2.250 0.1761 0.00877 0.00256 -0.1042 0.8191 0.1228
-2.000 0.1996 0.00852 0.00251 -0.1036 0.8176 0.1752
-1.750 0.2242 0.00840 0.00247 -0.1032 0.8161 0.2007
-1.500 0.2501 0.00830 0.00243 -0.1030 0.8138 0.2217
-1.250 0.2799 0.00817 0.00237 -0.1037 0.8116 0.2499
-1.000 0.3027 0.00806 0.00238 -0.1028 0.8096 0.2817
-0.750 0.3146 0.00799 0.00241 -0.0994 0.8066 0.3082
-0.500 0.3336 0.00793 0.00243 -0.0976 0.8045 0.3329
-0.250 0.3529 0.00788 0.00245 -0.0958 0.8021 0.3546
0.000 0.3745 0.00778 0.00245 -0.0946 0.7994 0.3856
0.250 0.4000 0.00768 0.00245 -0.0943 0.7975 0.4171
0.500 0.4297 0.00763 0.00243 -0.0950 0.7947 0.4334
0.750 0.4397 0.00752 0.00251 -0.0911 0.7922 0.4833
1.000 0.4546 0.00733 0.00256 -0.0884 0.7900 0.5552
1.250 0.4399 0.00662 0.00259 -0.0788 0.7861 0.7737
1.750 0.6343 0.00763 0.00407 -0.1111 0.7798 0.9245
2.000 0.6440 0.00795 0.00442 -0.1069 0.7722 0.9373
2.250 0.6568 0.00810 0.00455 -0.1035 0.7662 0.9436
2.500 0.6840 0.00826 0.00472 -0.1036 0.7608 0.9458
2.750 0.6934 0.00854 0.00497 -0.0994 0.7470 0.9515
3.000 0.6994 0.00882 0.00521 -0.0945 0.7269 0.9556
3.250 0.7117 0.00920 0.00548 -0.0912 0.6929 0.9577
3.500 0.6848 0.01020 0.00621 -0.0790 0.6371 0.9656
3.750 0.6859 0.01118 0.00691 -0.0737 0.5773 0.9673
4.000 0.6760 0.01241 0.00777 -0.0663 0.4895 0.9697
4.250 0.6680 0.01366 0.00868 -0.0594 0.4175 0.9740
4.500 0.6784 0.01423 0.00915 -0.0561 0.3941 0.9763
4.750 0.7035 0.01460 0.00945 -0.0562 0.3723 0.9770
5.000 0.7302 0.01507 0.00980 -0.0568 0.3450 0.9783
5.250 0.7521 0.01550 0.01014 -0.0562 0.3196 0.9795
5.500 0.7655 0.01619 0.01065 -0.0539 0.2769 0.9812
5.750 0.7749 0.01702 0.01126 -0.0509 0.2325 0.9836
6.000 0.7872 0.01763 0.01179 -0.0482 0.2116 0.9856
6.250 0.8066 0.01809 0.01213 -0.0473 0.1853 0.9861
6.500 0.8257 0.01853 0.01247 -0.0463 0.1620 0.9866
6.750 0.8428 0.01901 0.01283 -0.0449 0.1384 0.9870
7.000 0.8659 0.01925 0.01308 -0.0445 0.1351 0.9875
7.250 0.8806 0.01992 0.01355 -0.0428 0.1002 0.9882
7.500 0.8996 0.02031 0.01392 -0.0417 0.0917 0.9887
7.750 0.9164 0.02079 0.01432 -0.0403 0.0785 0.9892
8.250 0.9529 0.02159 0.01509 -0.0378 0.0666 0.9902
8.500 0.9719 0.02198 0.01548 -0.0367 0.0640 0.9908
8.750 0.9891 0.02248 0.01595 -0.0355 0.0563 0.9915
9.000 1.0067 0.02290 0.01637 -0.0341 0.0543 0.9919
9.250 1.0232 0.02336 0.01683 -0.0326 0.0506 0.9923
9.500 1.0407 0.02377 0.01727 -0.0313 0.0486 0.9927
9.750 1.0556 0.02438 0.01783 -0.0296 0.0409 0.9933
10.000 1.0717 0.02507 0.01850 -0.0281 0.0357 0.9944
10.250 1.0871 0.02561 0.01902 -0.0266 0.0296 0.9946
10.500 1.1021 0.02619 0.01956 -0.0251 0.0245 0.9947
10.750 1.1181 0.02672 0.02010 -0.0237 0.0224 0.9948
11.000 1.1328 0.02733 0.02071 -0.0222 0.0200 0.9950
11.250 1.1481 0.02790 0.02130 -0.0208 0.0182 0.9951
11.500 1.1625 0.02854 0.02196 -0.0192 0.0169 0.9953
11.750 1.1774 0.02915 0.02260 -0.0178 0.0162 0.9954
12.000 1.1925 0.02975 0.02322 -0.0164 0.0152 0.9956
12.250 1.2063 0.03043 0.02394 -0.0149 0.0145 0.9957
12.500 1.2190 0.03117 0.02468 -0.0132 0.0131 0.9958
12.750 1.2328 0.03186 0.02542 -0.0117 0.0129 0.9959
13.000 1.2469 0.03263 0.02622 -0.0104 0.0118 0.9962
13.250 1.2623 0.03337 0.02700 -0.0094 0.0117 0.9966
13.500 1.2738 0.03424 0.02790 -0.0077 0.0110 0.9967
13.750 1.2844 0.03513 0.02883 -0.0059 0.0103 0.9967
14.000 1.2949 0.03603 0.02978 -0.0042 0.0103 0.9967
14.250 1.3067 0.03685 0.03063 -0.0026 0.0098 0.9968
14.500 1.3165 0.03781 0.03164 -0.0008 0.0094 0.9968
14.750 1.3251 0.03884 0.03274 0.0011 0.0095 0.9967
15.000 1.3326 0.04000 0.03394 0.0031 0.0089 0.9967
15.250 1.3411 0.04107 0.03506 0.0049 0.0087 0.9966
15.500 1.3473 0.04233 0.03638 0.0069 0.0086 0.9965
15.750 1.3566 0.04334 0.03743 0.0084 0.0079 0.9965
16.000 1.3605 0.04481 0.03898 0.0106 0.0079 0.9964
16.250 1.3667 0.04610 0.04034 0.0124 0.0077 0.9963
16.500 1.3745 0.04725 0.04151 0.0139 0.0072 0.9962
16.750 1.3753 0.04904 0.04340 0.0161 0.0073 0.9960
17.000 1.3796 0.05054 0.04492 0.0179 0.0064 0.9959
17.250 1.3842 0.05205 0.04654 0.0195 0.0070 0.9958
17.500 1.3849 0.05397 0.04853 0.0213 0.0069 0.9957
17.750 1.3853 0.05594 0.05055 0.0229 0.0066 0.9956
18.000 1.3874 0.05782 0.05253 0.0243 0.0068 0.9956
18.250 1.3874 0.06001 0.05479 0.0257 0.0063 0.9955
18.500 1.3867 0.06253 0.05741 0.0265 0.0066 0.9957
18.750 1.3907 0.06459 0.05954 0.0269 0.0062 0.9958
19.000 1.3887 0.06714 0.06218 0.0279 0.0062 0.9957
19.250 1.3834 0.07008 0.06523 0.0289 0.0062 0.9957
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