GOE 384 AIRFOIL (goe384-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 384 AIRFOIL (goe384-il) Reynolds number: 1,000,000 Max Cl/Cd: 100.47 at α=4.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe384-il-1000000-n5.txt Download as CSV file: xf-goe384-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: GOE 384 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
------ -------- --------- --------- -------- -------- --------
-16.500 -0.9191 0.03693 0.03308 -0.1238 0.8074 0.0275
-16.250 -0.9253 0.03284 0.02881 -0.1276 0.7972 0.0276
-16.000 -0.9246 0.03034 0.02615 -0.1290 0.7880 0.0278
-15.750 -0.9197 0.02857 0.02424 -0.1291 0.7765 0.0279
-15.500 -0.9122 0.02720 0.02273 -0.1286 0.7635 0.0281
-15.250 -0.9029 0.02610 0.02148 -0.1275 0.7457 0.0282
-15.000 -0.8943 0.02525 0.02045 -0.1259 0.7188 0.0284
-14.500 -0.8630 0.02372 0.01853 -0.1242 0.6634 0.0287
-14.000 -0.8255 0.02234 0.01689 -0.1228 0.6424 0.0290
-13.750 -0.8050 0.02171 0.01615 -0.1222 0.6360 0.0291
-13.250 -0.7633 0.02042 0.01467 -0.1210 0.6261 0.0294
-13.000 -0.7413 0.01981 0.01400 -0.1205 0.6226 0.0297
-12.750 -0.7182 0.01929 0.01342 -0.1201 0.6192 0.0299
-12.500 -0.6943 0.01883 0.01291 -0.1197 0.6161 0.0301
-12.250 -0.6698 0.01841 0.01243 -0.1194 0.6133 0.0303
-11.750 -0.6196 0.01763 0.01154 -0.1188 0.6083 0.0308
-11.500 -0.5940 0.01725 0.01111 -0.1186 0.6069 0.0310
-11.250 -0.5681 0.01688 0.01069 -0.1184 0.6054 0.0313
-11.000 -0.5419 0.01652 0.01028 -0.1182 0.6038 0.0315
-10.750 -0.5156 0.01618 0.00989 -0.1181 0.6018 0.0318
-10.500 -0.4890 0.01587 0.00952 -0.1179 0.5994 0.0321
-10.250 -0.4623 0.01557 0.00917 -0.1178 0.5968 0.0325
-10.000 -0.4355 0.01529 0.00882 -0.1177 0.5942 0.0327
-9.750 -0.4086 0.01502 0.00848 -0.1175 0.5918 0.0329
-9.500 -0.3819 0.01471 0.00811 -0.1174 0.5894 0.0332
-9.250 -0.3549 0.01436 0.00775 -0.1173 0.5880 0.0336
-9.000 -0.3273 0.01408 0.00745 -0.1173 0.5864 0.0339
-8.750 -0.2995 0.01383 0.00719 -0.1173 0.5848 0.0343
-8.500 -0.2715 0.01361 0.00694 -0.1173 0.5832 0.0346
-8.250 -0.2435 0.01339 0.00671 -0.1174 0.5815 0.0350
-8.000 -0.2154 0.01319 0.00647 -0.1174 0.5793 0.0354
-7.750 -0.1873 0.01300 0.00624 -0.1174 0.5770 0.0358
-7.500 -0.1592 0.01281 0.00601 -0.1175 0.5749 0.0362
-7.250 -0.1310 0.01264 0.00580 -0.1175 0.5731 0.0367
-7.000 -0.1029 0.01249 0.00560 -0.1176 0.5710 0.0370
-6.750 -0.0744 0.01228 0.00538 -0.1177 0.5694 0.0375
-6.500 -0.0458 0.01207 0.00518 -0.1178 0.5674 0.0381
-6.250 -0.0171 0.01191 0.00502 -0.1180 0.5652 0.0387
-6.000 0.0117 0.01177 0.00486 -0.1181 0.5629 0.0392
-5.750 0.0404 0.01163 0.00471 -0.1183 0.5609 0.0398
-5.500 0.0692 0.01150 0.00456 -0.1184 0.5589 0.0404
-5.250 0.0978 0.01138 0.00441 -0.1186 0.5568 0.0410
-5.000 0.1265 0.01129 0.00428 -0.1187 0.5544 0.0415
-4.750 0.1550 0.01116 0.00413 -0.1188 0.5521 0.0421
-4.500 0.1840 0.01101 0.00399 -0.1191 0.5500 0.0429
-4.250 0.2130 0.01089 0.00388 -0.1193 0.5473 0.0437
-4.000 0.2421 0.01080 0.00379 -0.1195 0.5445 0.0446
-3.750 0.2709 0.01072 0.00369 -0.1197 0.5414 0.0455
-3.500 0.2996 0.01065 0.00360 -0.1199 0.5381 0.0462
-3.250 0.3282 0.01059 0.00350 -0.1201 0.5347 0.0469
-3.000 0.3572 0.01046 0.00340 -0.1203 0.5310 0.0480
-2.750 0.3859 0.01039 0.00332 -0.1205 0.5256 0.0490
-2.500 0.4142 0.01035 0.00325 -0.1206 0.5194 0.0501
-2.250 0.4429 0.01030 0.00319 -0.1208 0.5138 0.0512
-2.000 0.4711 0.01029 0.00314 -0.1210 0.5048 0.0522
-1.750 0.4987 0.01026 0.00308 -0.1210 0.4939 0.0537
-1.500 0.5253 0.01032 0.00307 -0.1209 0.4778 0.0552
-1.250 0.5511 0.01043 0.00309 -0.1206 0.4600 0.0567
-1.000 0.5769 0.01056 0.00313 -0.1203 0.4452 0.0581
-0.750 0.6027 0.01066 0.00319 -0.1201 0.4340 0.0607
-0.500 0.6294 0.01073 0.00323 -0.1200 0.4260 0.0635
-0.250 0.6555 0.01082 0.00329 -0.1198 0.4187 0.0671
0.000 0.6826 0.01086 0.00334 -0.1198 0.4138 0.0731
0.250 0.7091 0.01091 0.00341 -0.1197 0.4085 0.0830
0.500 0.7350 0.01101 0.00350 -0.1195 0.4030 0.0917
0.750 0.7616 0.01108 0.00357 -0.1194 0.3989 0.0981
1.000 0.7883 0.01113 0.00363 -0.1193 0.3954 0.1041
1.250 0.8146 0.01120 0.00371 -0.1192 0.3919 0.1096
1.500 0.8404 0.01128 0.00380 -0.1190 0.3884 0.1181
1.750 0.8655 0.01136 0.00390 -0.1187 0.3849 0.1314
2.000 0.8907 0.01124 0.00401 -0.1186 0.3821 0.2267
2.250 0.9165 0.01113 0.00413 -0.1185 0.3798 0.3173
2.500 0.9417 0.01102 0.00427 -0.1184 0.3769 0.4149
2.750 0.9662 0.01091 0.00444 -0.1182 0.3739 0.5226
3.000 0.9892 0.01076 0.00464 -0.1177 0.3709 0.6624
3.250 1.0078 0.01054 0.00488 -0.1161 0.3682 0.8270
3.500 1.0245 0.01054 0.00516 -0.1137 0.3654 0.9521
3.750 1.0632 0.01069 0.00531 -0.1163 0.3636 1.0000
4.000 1.0855 0.01086 0.00546 -0.1155 0.3618 1.0000
4.250 1.1080 0.01104 0.00563 -0.1148 0.3596 1.0000
4.500 1.1303 0.01125 0.00583 -0.1142 0.3572 1.0000
4.750 1.1524 0.01150 0.00605 -0.1135 0.3545 1.0000
5.000 1.1739 0.01178 0.00630 -0.1127 0.3517 1.0000
5.250 1.1952 0.01208 0.00658 -0.1120 0.3488 1.0000
5.500 1.2179 0.01234 0.00684 -0.1115 0.3470 1.0000
5.750 1.2411 0.01258 0.00708 -0.1111 0.3456 1.0000
6.000 1.2641 0.01284 0.00735 -0.1108 0.3438 1.0000
6.250 1.2868 0.01312 0.00763 -0.1104 0.3419 1.0000
6.500 1.3087 0.01344 0.00795 -0.1099 0.3398 1.0000
6.750 1.3301 0.01379 0.00829 -0.1093 0.3376 1.0000
7.000 1.3507 0.01418 0.00868 -0.1087 0.3351 1.0000
7.250 1.3702 0.01464 0.00912 -0.1079 0.3324 1.0000
7.500 1.3909 0.01505 0.00953 -0.1074 0.3303 1.0000
7.750 1.4129 0.01540 0.00991 -0.1070 0.3289 1.0000
8.000 1.4340 0.01579 0.01032 -0.1066 0.3273 1.0000
8.250 1.4548 0.01621 0.01075 -0.1061 0.3255 1.0000
8.500 1.4750 0.01666 0.01121 -0.1056 0.3235 1.0000
8.750 1.4941 0.01719 0.01175 -0.1050 0.3215 1.0000
9.000 1.5121 0.01778 0.01234 -0.1042 0.3187 1.0000
9.250 1.5269 0.01855 0.01310 -0.1032 0.3146 1.0000
9.500 1.5470 0.01904 0.01362 -0.1027 0.3114 1.0000
9.750 1.5650 0.01966 0.01424 -0.1021 0.3072 1.0000
10.000 1.5804 0.02044 0.01502 -0.1012 0.3035 1.0000
10.250 1.5942 0.02133 0.01590 -0.1002 0.2996 1.0000
10.500 1.6105 0.02208 0.01668 -0.0995 0.2965 1.0000
10.750 1.6267 0.02284 0.01746 -0.0988 0.2929 1.0000
11.000 1.6411 0.02374 0.01837 -0.0980 0.2894 1.0000
11.250 1.6536 0.02479 0.01943 -0.0970 0.2861 1.0000
11.500 1.6656 0.02590 0.02055 -0.0960 0.2828 1.0000
11.750 1.6804 0.02683 0.02151 -0.0954 0.2794 1.0000
12.000 1.6925 0.02798 0.02268 -0.0945 0.2748 1.0000
12.250 1.7002 0.02948 0.02418 -0.0934 0.2698 1.0000
12.500 1.7106 0.03083 0.02555 -0.0925 0.2653 1.0000
12.750 1.7192 0.03233 0.02706 -0.0916 0.2590 1.0000
13.000 1.7230 0.03426 0.02898 -0.0904 0.2531 1.0000
13.250 1.7316 0.03584 0.03059 -0.0896 0.2477 1.0000
13.500 1.7343 0.03794 0.03269 -0.0884 0.2410 1.0000
13.750 1.7393 0.03989 0.03465 -0.0875 0.2349 1.0000
14.000 1.7404 0.04221 0.03697 -0.0865 0.2275 1.0000
14.250 1.7416 0.04453 0.03930 -0.0855 0.2211 1.0000
14.500 1.7379 0.04733 0.04209 -0.0843 0.2123 1.0000
14.750 1.7343 0.05013 0.04489 -0.0831 0.2025 1.0000
15.000 1.7246 0.05356 0.04829 -0.0817 0.1916 1.0000
15.250 1.7111 0.05740 0.05211 -0.0803 0.1803 1.0000
15.500 1.6980 0.06130 0.05599 -0.0790 0.1701 1.0000
15.750 1.6886 0.06487 0.05955 -0.0780 0.1611 1.0000
16.000 1.6798 0.06847 0.06317 -0.0771 0.1546 1.0000
16.250 1.6714 0.07209 0.06681 -0.0764 0.1484 1.0000
16.500 1.6655 0.07550 0.07025 -0.0758 0.1432 1.0000
16.750 1.6571 0.07924 0.07402 -0.0753 0.1380 1.0000
17.000 1.6482 0.08306 0.07788 -0.0748 0.1331 1.0000
17.250 1.6416 0.08671 0.08156 -0.0746 0.1284 1.0000
17.500 1.6296 0.09106 0.08595 -0.0743 0.1237 1.0000
17.750 1.6221 0.09491 0.08985 -0.0742 0.1198 1.0000
18.000 1.6131 0.09894 0.09391 -0.0742 0.1151 1.0000
18.250 1.6003 0.10354 0.09855 -0.0743 0.1107 1.0000
18.500 1.5893 0.10797 0.10303 -0.0746 0.1057 1.0000
18.750 1.5746 0.11293 0.10801 -0.0750 0.1003 1.0000
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