GOE 288 AIRFOIL (goe288-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 288 AIRFOIL (goe288-il) Reynolds number: 1,000,000 Max Cl/Cd: 113.86 at α=8° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe288-il-1000000-n5.txt Download as CSV file: xf-goe288-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: GOE 288 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
------ -------- --------- --------- -------- -------- --------
-18.750 -0.6944 0.13306 0.13061 -0.0403 1.0000 0.0232
-18.500 -0.7142 0.12533 0.12279 -0.0448 1.0000 0.0234
-18.250 -0.7289 0.11870 0.11609 -0.0486 1.0000 0.0235
-18.000 -0.7399 0.11290 0.11023 -0.0520 1.0000 0.0237
-17.750 -0.7533 0.10674 0.10400 -0.0556 1.0000 0.0238
-17.500 -0.7668 0.10071 0.09789 -0.0591 1.0000 0.0239
-17.250 -0.7780 0.09514 0.09225 -0.0624 1.0000 0.0240
-17.000 -0.7886 0.08977 0.08682 -0.0656 1.0000 0.0241
-16.750 -0.7995 0.08441 0.08138 -0.0688 1.0000 0.0241
-16.500 -0.8102 0.07919 0.07609 -0.0720 1.0000 0.0242
-16.250 -0.8202 0.07416 0.07099 -0.0751 1.0000 0.0243
-16.000 -0.8291 0.06940 0.06616 -0.0780 1.0000 0.0244
-15.750 -0.8384 0.06470 0.06140 -0.0809 1.0000 0.0244
-15.500 -0.8490 0.06002 0.05665 -0.0839 1.0000 0.0245
-15.250 -0.8618 0.05538 0.05193 -0.0868 1.0000 0.0245
-15.000 -0.8756 0.05080 0.04728 -0.0896 1.0000 0.0246
-14.750 -0.8825 0.04597 0.04237 -0.0942 0.9919 0.0247
-14.500 -0.8864 0.04104 0.03733 -0.0997 0.9764 0.0247
-14.250 -0.8928 0.03611 0.03228 -0.1048 0.9540 0.0248
-14.000 -0.8952 0.03076 0.02675 -0.1118 0.9306 0.0249
-13.750 -0.8790 0.02622 0.02199 -0.1194 0.9124 0.0250
-13.500 -0.8601 0.02437 0.01997 -0.1216 0.8962 0.0251
-13.250 -0.8399 0.02308 0.01855 -0.1227 0.8805 0.0252
-13.000 -0.8183 0.02204 0.01737 -0.1233 0.8650 0.0254
-12.750 -0.7956 0.02114 0.01635 -0.1238 0.8497 0.0255
-12.500 -0.7720 0.02036 0.01545 -0.1242 0.8337 0.0257
-12.250 -0.7477 0.01971 0.01467 -0.1245 0.8166 0.0258
-12.000 -0.7229 0.01912 0.01396 -0.1247 0.7979 0.0260
-11.750 -0.6978 0.01858 0.01329 -0.1248 0.7772 0.0261
-11.500 -0.6725 0.01808 0.01264 -0.1249 0.7553 0.0262
-11.250 -0.6467 0.01762 0.01204 -0.1250 0.7337 0.0263
-11.000 -0.6215 0.01696 0.01125 -0.1253 0.7141 0.0265
-10.750 -0.5955 0.01640 0.01058 -0.1255 0.6968 0.0268
-10.500 -0.5688 0.01591 0.00999 -0.1257 0.6813 0.0270
-10.250 -0.5416 0.01548 0.00948 -0.1259 0.6680 0.0272
-10.000 -0.5141 0.01511 0.00901 -0.1261 0.6556 0.0275
-9.750 -0.4862 0.01474 0.00858 -0.1263 0.6449 0.0277
-9.500 -0.4582 0.01442 0.00818 -0.1265 0.6353 0.0279
-9.250 -0.4298 0.01411 0.00780 -0.1268 0.6260 0.0282
-9.000 -0.4014 0.01383 0.00744 -0.1270 0.6174 0.0285
-8.750 -0.3727 0.01354 0.00709 -0.1272 0.6100 0.0287
-8.500 -0.3440 0.01328 0.00677 -0.1274 0.6029 0.0290
-8.250 -0.3151 0.01303 0.00646 -0.1277 0.5972 0.0293
-8.000 -0.2859 0.01278 0.00616 -0.1279 0.5919 0.0296
-7.750 -0.2568 0.01256 0.00589 -0.1282 0.5862 0.0299
-7.250 -0.1982 0.01212 0.00535 -0.1287 0.5767 0.0304
-7.000 -0.1689 0.01186 0.00506 -0.1290 0.5711 0.0310
-6.750 -0.1396 0.01167 0.00482 -0.1292 0.5646 0.0317
-6.500 -0.1102 0.01150 0.00461 -0.1295 0.5586 0.0323
-6.250 -0.0806 0.01133 0.00441 -0.1297 0.5527 0.0329
-6.000 -0.0511 0.01118 0.00422 -0.1300 0.5472 0.0335
-5.500 0.0083 0.01091 0.00387 -0.1305 0.5392 0.0349
-5.250 0.0381 0.01074 0.00369 -0.1308 0.5349 0.0361
-5.000 0.0678 0.01062 0.00354 -0.1311 0.5299 0.0375
-4.750 0.0974 0.01053 0.00341 -0.1313 0.5248 0.0391
-4.500 0.1272 0.01038 0.00326 -0.1316 0.5207 0.0422
-4.250 0.1570 0.01024 0.00312 -0.1319 0.5164 0.0471
-4.000 0.1868 0.01007 0.00298 -0.1322 0.5117 0.0572
-3.750 0.2163 0.00988 0.00284 -0.1326 0.5066 0.0771
-3.500 0.2461 0.00973 0.00275 -0.1329 0.5026 0.0935
-3.250 0.2760 0.00964 0.00268 -0.1332 0.4986 0.1032
-3.000 0.3058 0.00958 0.00262 -0.1335 0.4944 0.1102
-2.750 0.3355 0.00952 0.00257 -0.1337 0.4905 0.1179
-2.500 0.3651 0.00949 0.00252 -0.1340 0.4865 0.1252
-2.250 0.3950 0.00941 0.00248 -0.1343 0.4835 0.1361
-1.750 0.4545 0.00926 0.00239 -0.1349 0.4747 0.1650
-1.500 0.4838 0.00919 0.00236 -0.1351 0.4692 0.1876
-1.250 0.5135 0.00907 0.00234 -0.1355 0.4646 0.2188
-1.000 0.5431 0.00901 0.00234 -0.1358 0.4592 0.2443
-0.750 0.5724 0.00901 0.00236 -0.1360 0.4533 0.2645
-0.500 0.6018 0.00901 0.00238 -0.1362 0.4481 0.2806
-0.250 0.6312 0.00904 0.00241 -0.1364 0.4413 0.2921
0.000 0.6601 0.00911 0.00246 -0.1365 0.4336 0.3018
0.250 0.6893 0.00916 0.00250 -0.1367 0.4248 0.3103
0.500 0.7179 0.00927 0.00256 -0.1368 0.4135 0.3174
0.750 0.7460 0.00942 0.00263 -0.1368 0.3985 0.3226
1.000 0.7738 0.00959 0.00273 -0.1368 0.3815 0.3289
1.250 0.8014 0.00978 0.00285 -0.1367 0.3662 0.3353
1.500 0.8291 0.00996 0.00297 -0.1367 0.3533 0.3417
1.750 0.8569 0.01011 0.00309 -0.1367 0.3435 0.3503
2.000 0.8845 0.01029 0.00323 -0.1366 0.3344 0.3585
2.250 0.9125 0.01041 0.00335 -0.1366 0.3282 0.3671
2.500 0.9403 0.01055 0.00347 -0.1366 0.3221 0.3724
2.750 0.9677 0.01073 0.00361 -0.1365 0.3159 0.3761
3.000 0.9958 0.01084 0.00372 -0.1365 0.3119 0.3800
3.250 1.0235 0.01097 0.00384 -0.1365 0.3076 0.3845
3.500 1.0508 0.01112 0.00399 -0.1364 0.3034 0.3896
3.750 1.0780 0.01129 0.00414 -0.1363 0.2994 0.3944
4.000 1.1056 0.01141 0.00427 -0.1363 0.2970 0.3989
4.250 1.1332 0.01151 0.00440 -0.1363 0.2947 0.4041
4.500 1.1605 0.01164 0.00454 -0.1362 0.2922 0.4095
4.750 1.1875 0.01179 0.00469 -0.1361 0.2896 0.4149
5.000 1.2141 0.01194 0.00487 -0.1359 0.2869 0.4222
5.250 1.2404 0.01212 0.00505 -0.1357 0.2839 0.4295
5.750 1.2932 0.01241 0.00540 -0.1353 0.2794 0.4457
6.000 1.3197 0.01254 0.00558 -0.1351 0.2776 0.4567
6.250 1.3458 0.01268 0.00576 -0.1349 0.2757 0.4720
6.500 1.3715 0.01283 0.00597 -0.1346 0.2737 0.4913
6.750 1.3969 0.01298 0.00619 -0.1343 0.2716 0.5167
7.000 1.4218 0.01314 0.00643 -0.1339 0.2695 0.5539
7.250 1.4462 0.01328 0.00672 -0.1335 0.2669 0.6189
7.500 1.4644 0.01289 0.00703 -0.1317 0.2643 1.0000
7.750 1.4892 0.01308 0.00724 -0.1312 0.2630 1.0000
8.000 1.5132 0.01329 0.00747 -0.1307 0.2614 1.0000
8.250 1.5366 0.01351 0.00770 -0.1300 0.2595 1.0000
8.500 1.5590 0.01376 0.00796 -0.1291 0.2571 1.0000
8.750 1.5791 0.01404 0.00825 -0.1279 0.2546 1.0000
9.000 1.5983 0.01437 0.00857 -0.1265 0.2520 1.0000
9.250 1.6171 0.01473 0.00894 -0.1251 0.2496 1.0000
9.500 1.6367 0.01507 0.00930 -0.1239 0.2480 1.0000
9.750 1.6575 0.01537 0.00963 -0.1229 0.2468 1.0000
10.000 1.6777 0.01570 0.00999 -0.1218 0.2443 1.0000
10.250 1.6969 0.01608 0.01039 -0.1207 0.2413 1.0000
10.500 1.7150 0.01653 0.01086 -0.1194 0.2385 1.0000
10.750 1.7317 0.01707 0.01139 -0.1180 0.2353 1.0000
11.000 1.7485 0.01762 0.01196 -0.1166 0.2325 1.0000
11.250 1.7672 0.01808 0.01246 -0.1156 0.2307 1.0000
11.500 1.7850 0.01860 0.01302 -0.1145 0.2278 1.0000
11.750 1.8001 0.01929 0.01372 -0.1131 0.2232 1.0000
12.000 1.8125 0.02017 0.01459 -0.1115 0.2182 1.0000
12.250 1.8287 0.02085 0.01530 -0.1104 0.2149 1.0000
12.500 1.8430 0.02167 0.01615 -0.1091 0.2108 1.0000
12.750 1.8537 0.02275 0.01723 -0.1076 0.2057 1.0000
13.000 1.8651 0.02382 0.01832 -0.1062 0.2002 1.0000
13.250 1.8721 0.02526 0.01975 -0.1046 0.1920 1.0000
13.500 1.8777 0.02686 0.02134 -0.1029 0.1832 1.0000
13.750 1.8742 0.02926 0.02369 -0.1008 0.1692 1.0000
14.000 1.8557 0.03308 0.02740 -0.0981 0.1471 1.0000
14.250 1.8208 0.03870 0.03288 -0.0950 0.1186 1.0000
14.500 1.7930 0.04404 0.03816 -0.0930 0.0993 1.0000
14.750 1.7731 0.04883 0.04294 -0.0917 0.0874 1.0000
15.000 1.7634 0.05265 0.04678 -0.0909 0.0811 1.0000
15.250 1.7541 0.05648 0.05065 -0.0902 0.0765 1.0000
15.500 1.7501 0.05982 0.05405 -0.0897 0.0735 1.0000
15.750 1.7450 0.06333 0.05762 -0.0893 0.0707 1.0000
16.000 1.7375 0.06712 0.06147 -0.0890 0.0681 1.0000
16.250 1.7336 0.07054 0.06495 -0.0887 0.0659 1.0000
16.500 1.7270 0.07437 0.06884 -0.0886 0.0632 1.0000
16.750 1.7175 0.07860 0.07313 -0.0885 0.0605 1.0000
17.000 1.7096 0.08264 0.07722 -0.0885 0.0578 1.0000
17.250 1.7002 0.08695 0.08159 -0.0886 0.0545 1.0000
17.500 1.6876 0.09175 0.08646 -0.0889 0.0516 1.0000
17.750 1.6748 0.09665 0.09141 -0.0894 0.0478 1.0000
18.000 1.6597 0.10190 0.09672 -0.0900 0.0442 1.0000
18.250 1.6442 0.10730 0.10217 -0.0908 0.0406 1.0000
18.500 1.6287 0.11281 0.10775 -0.0917 0.0369 1.0000
18.750 1.6126 0.11845 0.11344 -0.0929 0.0335 1.0000
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