GOE 15K AIRFOIL (goe15k-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: GOE 15K AIRFOIL (goe15k-il) Reynolds number: 1,000,000 Max Cl/Cd: 92.35 at α=3.75° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-goe15k-il-1000000.txt Download as CSV file: xf-goe15k-il-1000000.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 = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.000 -0.6734 0.11660 0.11428 -0.1032 0.9780 0.0145
-18.750 -0.7207 0.10394 0.10148 -0.1102 0.9776 0.0149
-18.500 -0.7688 0.09198 0.08935 -0.1171 0.9773 0.0146
-18.250 -0.8007 0.08271 0.07995 -0.1231 0.9769 0.0150
-18.000 -0.8529 0.07093 0.06796 -0.1305 0.9765 0.0145
-17.750 -0.8797 0.06254 0.05942 -0.1367 0.9762 0.0148
-17.500 -0.9288 0.05382 0.05051 -0.1387 0.9707 0.0143
-17.250 -0.9395 0.04785 0.04439 -0.1436 0.9693 0.0146
-17.000 -0.9377 0.04398 0.04042 -0.1473 0.9683 0.0148
-16.750 -0.9479 0.03918 0.03543 -0.1506 0.9673 0.0149
-16.500 -0.9458 0.03633 0.03245 -0.1523 0.9666 0.0152
-16.250 -0.9464 0.03357 0.02953 -0.1530 0.9659 0.0151
-16.000 -0.9518 0.03210 0.02798 -0.1498 0.9613 0.0154
-15.750 -0.9419 0.03094 0.02672 -0.1489 0.9589 0.0159
-15.500 -0.9290 0.02978 0.02547 -0.1487 0.9576 0.0161
-15.250 -0.9283 0.02781 0.02338 -0.1473 0.9562 0.0166
-15.000 -0.9214 0.02624 0.02169 -0.1460 0.9553 0.0168
-14.750 -0.9073 0.02512 0.02052 -0.1455 0.9547 0.0173
-14.500 -0.9053 0.02450 0.01986 -0.1415 0.9499 0.0180
-14.250 -0.8964 0.02366 0.01894 -0.1392 0.9469 0.0181
-14.000 -0.8817 0.02277 0.01796 -0.1380 0.9454 0.0186
-13.750 -0.8601 0.02219 0.01730 -0.1378 0.9445 0.0193
-13.500 -0.8409 0.02144 0.01647 -0.1372 0.9437 0.0196
-13.250 -0.8278 0.02028 0.01525 -0.1358 0.9428 0.0207
-13.000 -0.8052 0.01968 0.01460 -0.1357 0.9423 0.0217
-12.750 -0.8095 0.01921 0.01408 -0.1296 0.9351 0.0218
-12.500 -0.7904 0.01860 0.01340 -0.1286 0.9335 0.0224
-12.250 -0.7697 0.01801 0.01273 -0.1278 0.9324 0.0232
-12.000 -0.7483 0.01738 0.01204 -0.1272 0.9314 0.0238
-11.750 -0.7239 0.01687 0.01153 -0.1272 0.9306 0.0254
-11.500 -0.6971 0.01645 0.01107 -0.1276 0.9298 0.0269
-11.250 -0.6896 0.01610 0.01067 -0.1237 0.9244 0.0274
-11.000 -0.6693 0.01565 0.01016 -0.1226 0.9219 0.0285
-10.750 -0.6437 0.01527 0.00979 -0.1227 0.9203 0.0302
-10.500 -0.6135 0.01502 0.00952 -0.1237 0.9191 0.0317
-10.250 -0.5834 0.01463 0.00906 -0.1247 0.9181 0.0328
-10.000 -0.5525 0.01420 0.00864 -0.1260 0.9171 0.0347
-9.750 -0.5175 0.01398 0.00841 -0.1280 0.9162 0.0364
-9.500 -0.5034 0.01392 0.00832 -0.1253 0.9113 0.0375
-9.250 -0.4790 0.01378 0.00814 -0.1249 0.9083 0.0385
-9.000 -0.4523 0.01330 0.00760 -0.1252 0.9062 0.0399
-8.750 -0.4201 0.01295 0.00724 -0.1267 0.9048 0.0413
-8.500 -0.3835 0.01277 0.00706 -0.1291 0.9037 0.0430
-8.250 -0.3458 0.01256 0.00682 -0.1318 0.9025 0.0446
-8.000 -0.3256 0.01243 0.00664 -0.1304 0.8992 0.0454
-7.750 -0.3082 0.01249 0.00667 -0.1283 0.8951 0.0461
-7.500 -0.2867 0.01190 0.00603 -0.1274 0.8923 0.0476
-7.250 -0.2557 0.01156 0.00568 -0.1286 0.8905 0.0495
-7.000 -0.2209 0.01133 0.00544 -0.1306 0.8890 0.0514
-6.750 -0.1842 0.01111 0.00518 -0.1330 0.8876 0.0527
-6.500 -0.1705 0.01104 0.00509 -0.1300 0.8843 0.0537
-6.250 -0.1561 0.01091 0.00493 -0.1273 0.8810 0.0540
-6.000 -0.1328 0.01080 0.00479 -0.1265 0.8787 0.0549
-5.750 -0.1080 0.01043 0.00438 -0.1262 0.8767 0.0569
-5.500 -0.0771 0.01020 0.00414 -0.1273 0.8753 0.0592
-5.250 -0.0430 0.01000 0.00392 -0.1291 0.8739 0.0611
-5.000 -0.0059 0.00981 0.00371 -0.1316 0.8727 0.0626
-4.750 0.0167 0.00973 0.00361 -0.1307 0.8708 0.0636
-4.500 0.0238 0.00971 0.00358 -0.1260 0.8679 0.0646
-4.250 0.0435 0.00960 0.00345 -0.1244 0.8658 0.0663
-4.000 0.0674 0.00945 0.00331 -0.1237 0.8639 0.0700
-3.750 0.0940 0.00931 0.00319 -0.1237 0.8622 0.0744
-3.500 0.1221 0.00912 0.00305 -0.1241 0.8608 0.0886
-3.250 0.1532 0.00866 0.00292 -0.1254 0.8597 0.1699
-3.000 0.1873 0.00837 0.00284 -0.1273 0.8586 0.2305
-2.750 0.2235 0.00816 0.00280 -0.1298 0.8576 0.2787
-2.500 0.2564 0.00801 0.00279 -0.1313 0.8565 0.3188
-2.250 0.2539 0.00801 0.00287 -0.1244 0.8540 0.3392
-2.000 0.2656 0.00796 0.00290 -0.1209 0.8516 0.3663
-1.750 0.2855 0.00786 0.00291 -0.1193 0.8496 0.3970
-1.500 0.3094 0.00773 0.00289 -0.1187 0.8476 0.4314
-1.250 0.3361 0.00755 0.00284 -0.1187 0.8454 0.4760
-1.000 0.3600 0.00721 0.00280 -0.1182 0.8434 0.5710
-0.750 0.3618 0.00667 0.00280 -0.1125 0.8406 0.7334
-0.500 0.4915 0.00700 0.00367 -0.1360 0.8426 0.8910
-0.250 0.5292 0.00718 0.00384 -0.1383 0.8409 0.9006
0.000 0.5283 0.00737 0.00406 -0.1316 0.8376 0.9107
0.250 0.5501 0.00760 0.00429 -0.1301 0.8346 0.9167
0.500 0.5701 0.00785 0.00454 -0.1282 0.8325 0.9273
0.750 0.6136 0.00811 0.00480 -0.1318 0.8310 0.9298
1.000 0.6600 0.00828 0.00493 -0.1360 0.8272 0.9325
1.250 0.6665 0.00846 0.00511 -0.1312 0.8236 0.9400
1.500 0.7050 0.00874 0.00542 -0.1336 0.8214 0.9420
1.750 0.7355 0.00891 0.00558 -0.1340 0.8153 0.9449
2.000 0.7715 0.00898 0.00562 -0.1359 0.8093 0.9473
2.250 0.7766 0.00922 0.00590 -0.1306 0.8040 0.9533
2.500 0.8065 0.00929 0.00596 -0.1311 0.7978 0.9550
2.750 0.8300 0.00937 0.00604 -0.1302 0.7909 0.9573
3.000 0.8329 0.00966 0.00635 -0.1245 0.7837 0.9639
3.250 0.8640 0.00967 0.00636 -0.1254 0.7750 0.9651
3.500 0.8883 0.00973 0.00643 -0.1247 0.7668 0.9668
3.750 0.9115 0.00987 0.00659 -0.1238 0.7572 0.9701
4.000 0.9267 0.01017 0.00687 -0.1210 0.7431 0.9754
4.250 0.9458 0.01031 0.00693 -0.1192 0.7090 0.9781
4.500 0.9404 0.01120 0.00754 -0.1119 0.6485 0.9858
4.750 0.9307 0.01271 0.00857 -0.1044 0.5501 0.9941
5.000 0.9275 0.01357 0.00890 -0.0989 0.4404 0.9980
5.250 0.9331 0.01421 0.00932 -0.0949 0.3955 0.9994
5.500 0.9397 0.01473 0.00971 -0.0910 0.3630 0.9997
5.750 0.9435 0.01538 0.01014 -0.0867 0.3164 1.0000
6.000 0.9433 0.01615 0.01068 -0.0816 0.2656 1.0000
6.250 0.9438 0.01696 0.01124 -0.0767 0.2170 1.0000
6.500 0.9513 0.01753 0.01169 -0.0731 0.1900 1.0000
6.750 0.9592 0.01811 0.01214 -0.0697 0.1646 1.0000
7.000 0.9696 0.01862 0.01254 -0.0668 0.1422 1.0000
7.250 0.9807 0.01912 0.01296 -0.0639 0.1236 1.0000
7.500 0.9916 0.01964 0.01339 -0.0612 0.1056 1.0000
7.750 1.0032 0.02016 0.01382 -0.0585 0.0895 1.0000
8.000 1.0166 0.02061 0.01423 -0.0563 0.0808 1.0000
8.250 1.0292 0.02110 0.01469 -0.0539 0.0724 1.0000
8.500 1.0436 0.02153 0.01511 -0.0518 0.0678 1.0000
8.750 1.0576 0.02199 0.01556 -0.0497 0.0631 1.0000
9.000 1.0712 0.02248 0.01604 -0.0475 0.0587 1.0000
9.250 1.0868 0.02287 0.01645 -0.0457 0.0555 1.0000
9.500 1.1002 0.02340 0.01696 -0.0436 0.0517 1.0000
9.750 1.1146 0.02387 0.01744 -0.0417 0.0478 1.0000
10.000 1.1285 0.02438 0.01792 -0.0397 0.0433 1.0000
10.250 1.1427 0.02489 0.01845 -0.0378 0.0401 1.0000
10.500 1.1557 0.02548 0.01902 -0.0357 0.0364 1.0000
10.750 1.1692 0.02605 0.01960 -0.0338 0.0334 1.0000
11.000 1.1829 0.02662 0.02017 -0.0319 0.0315 1.0000
11.250 1.1947 0.02732 0.02087 -0.0297 0.0287 1.0000
11.500 1.2081 0.02792 0.02150 -0.0279 0.0271 1.0000
11.750 1.2203 0.02861 0.02220 -0.0259 0.0258 1.0000
12.000 1.2309 0.02943 0.02304 -0.0237 0.0243 1.0000
12.250 1.2435 0.03010 0.02375 -0.0218 0.0237 1.0000
12.500 1.2565 0.03075 0.02444 -0.0200 0.0226 1.0000
12.750 1.2675 0.03156 0.02528 -0.0180 0.0217 1.0000
13.000 1.2762 0.03253 0.02627 -0.0157 0.0204 1.0000
13.250 1.2871 0.03335 0.02714 -0.0139 0.0199 1.0000
13.500 1.2965 0.03431 0.02816 -0.0118 0.0196 1.0000
13.750 1.3091 0.03505 0.02894 -0.0102 0.0190 1.0000
14.000 1.3191 0.03599 0.02993 -0.0083 0.0180 1.0000
14.250 1.3275 0.03705 0.03103 -0.0063 0.0177 1.0000
14.500 1.3289 0.03866 0.03269 -0.0035 0.0165 1.0000
14.750 1.3387 0.03966 0.03374 -0.0018 0.0164 1.0000
15.000 1.3496 0.04059 0.03474 -0.0003 0.0161 1.0000
15.250 1.3558 0.04192 0.03613 0.0017 0.0159 1.0000
15.500 1.3680 0.04276 0.03701 0.0029 0.0151 1.0000
15.750 1.3721 0.04431 0.03864 0.0050 0.0151 1.0000
16.000 1.3742 0.04604 0.04045 0.0071 0.0148 1.0000
16.250 1.3853 0.04702 0.04145 0.0082 0.0143 1.0000
16.500 1.3874 0.04881 0.04331 0.0101 0.0141 1.0000
16.750 1.3766 0.05182 0.04642 0.0128 0.0135 1.0000
17.000 1.3787 0.05375 0.04844 0.0144 0.0133 1.0000
17.250 1.3832 0.05548 0.05024 0.0156 0.0133 1.0000
17.500 1.3851 0.05752 0.05238 0.0170 0.0131 1.0000
17.750 1.3900 0.05930 0.05424 0.0180 0.0128 1.0000
18.000 1.3914 0.06146 0.05647 0.0191 0.0127 1.0000
18.250 1.3870 0.06432 0.05944 0.0203 0.0124 1.0000
18.500 1.3963 0.06574 0.06090 0.0208 0.0119 1.0000
18.750 1.3878 0.06919 0.06448 0.0218 0.0122 1.0000
19.000 1.3875 0.07180 0.06715 0.0223 0.0118 1.0000
19.250 1.3733 0.07617 0.07167 0.0229 0.0118 1.0000
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