GEMINI (smoothed) (geminism-il) Xfoil prediction polar at RE=200,000 Ncrit=5
| Details | Polar file |
|---|---|
|
Airfoil: GEMINI (smoothed) (geminism-il) Reynolds number: 200,000 Max Cl/Cd: 65.44 at α=6.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-geminism-il-200000-n5.txt Download as CSV file: xf-geminism-il-200000-n5.csv |
XFOIL Version 6.96
Calculated polar for: GEMINI (smoothed)
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.200 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-14.000 -0.7581 0.06691 0.06233 -0.0680 1.0000 0.0218
-13.750 -0.7831 0.06012 0.05532 -0.0720 1.0000 0.0218
-13.500 -0.8018 0.05493 0.04993 -0.0744 1.0000 0.0220
-13.250 -0.8168 0.05071 0.04551 -0.0756 1.0000 0.0222
-13.000 -0.8295 0.04719 0.04178 -0.0758 1.0000 0.0224
-12.750 -0.8402 0.04421 0.03860 -0.0750 1.0000 0.0227
-12.500 -0.8493 0.04166 0.03586 -0.0734 1.0000 0.0230
-12.250 -0.8569 0.03948 0.03347 -0.0711 1.0000 0.0233
-12.000 -0.8636 0.03761 0.03140 -0.0680 1.0000 0.0237
-11.750 -0.8695 0.03604 0.02962 -0.0644 1.0000 0.0241
-11.500 -0.8755 0.03476 0.02816 -0.0600 1.0000 0.0244
-11.250 -0.8789 0.03364 0.02701 -0.0558 1.0000 0.0248
-11.000 -0.8786 0.03277 0.02611 -0.0521 1.0000 0.0252
-10.750 -0.8779 0.03203 0.02535 -0.0482 1.0000 0.0257
-10.250 -0.8451 0.02998 0.02308 -0.0467 0.9941 0.0274
-10.000 -0.8186 0.02863 0.02153 -0.0477 0.9880 0.0286
-9.750 -0.7910 0.02732 0.01999 -0.0487 0.9828 0.0296
-9.500 -0.7617 0.02599 0.01859 -0.0502 0.9791 0.0307
-9.250 -0.7341 0.02510 0.01766 -0.0511 0.9728 0.0320
-9.000 -0.7029 0.02419 0.01666 -0.0526 0.9684 0.0336
-8.750 -0.6762 0.02329 0.01564 -0.0531 0.9603 0.0351
-8.500 -0.6450 0.02240 0.01460 -0.0543 0.9548 0.0365
-8.250 -0.6189 0.02141 0.01362 -0.0548 0.9468 0.0382
-8.000 -0.5884 0.02068 0.01285 -0.0560 0.9404 0.0403
-7.750 -0.5592 0.01997 0.01205 -0.0568 0.9327 0.0425
-7.500 -0.5292 0.01930 0.01126 -0.0576 0.9253 0.0443
-7.250 -0.5027 0.01850 0.01046 -0.0579 0.9162 0.0470
-7.000 -0.4761 0.01796 0.00987 -0.0581 0.9064 0.0501
-6.500 -0.4230 0.01682 0.00861 -0.0582 0.8870 0.0572
-6.250 -0.3968 0.01637 0.00808 -0.0581 0.8771 0.0624
-6.000 -0.3707 0.01586 0.00753 -0.0579 0.8677 0.0687
-5.750 -0.3466 0.01547 0.00708 -0.0573 0.8570 0.0765
-5.500 -0.3221 0.01500 0.00660 -0.0569 0.8474 0.0887
-5.250 -0.2992 0.01450 0.00617 -0.0561 0.8372 0.1099
-5.000 -0.2780 0.01396 0.00582 -0.0551 0.8271 0.1521
-4.750 -0.2546 0.01353 0.00550 -0.0544 0.8180 0.1980
-4.500 -0.2327 0.01319 0.00525 -0.0534 0.8077 0.2344
-4.250 -0.2097 0.01287 0.00501 -0.0525 0.7986 0.2704
-4.000 -0.1876 0.01254 0.00478 -0.0515 0.7891 0.3083
-3.750 -0.1661 0.01223 0.00459 -0.0503 0.7797 0.3514
-3.500 -0.1442 0.01194 0.00442 -0.0492 0.7710 0.3994
-3.250 -0.1239 0.01167 0.00432 -0.0476 0.7615 0.4510
-3.000 -0.1027 0.01144 0.00423 -0.0462 0.7532 0.5049
-2.750 -0.0814 0.01127 0.00419 -0.0448 0.7439 0.5494
-2.500 -0.0580 0.01116 0.00411 -0.0437 0.7356 0.5822
-2.250 -0.0339 0.01109 0.00403 -0.0428 0.7267 0.6047
-2.000 -0.0090 0.01103 0.00396 -0.0421 0.7183 0.6250
-1.750 0.0157 0.01098 0.00389 -0.0413 0.7095 0.6449
-1.500 0.0406 0.01093 0.00384 -0.0406 0.7009 0.6639
-1.250 0.0658 0.01089 0.00378 -0.0399 0.6922 0.6827
-1.000 0.0910 0.01086 0.00376 -0.0392 0.6835 0.7013
-0.750 0.1167 0.01084 0.00371 -0.0386 0.6750 0.7196
-0.500 0.1421 0.01082 0.00371 -0.0380 0.6659 0.7382
-0.250 0.1683 0.01082 0.00369 -0.0375 0.6576 0.7582
0.000 0.1948 0.01080 0.00373 -0.0371 0.6480 0.7806
0.250 0.2220 0.01082 0.00377 -0.0367 0.6394 0.8074
0.500 0.2518 0.01086 0.00384 -0.0369 0.6299 0.8313
0.750 0.2821 0.01091 0.00389 -0.0373 0.6207 0.8500
1.000 0.3137 0.01099 0.00393 -0.0380 0.6114 0.8663
1.250 0.3466 0.01107 0.00401 -0.0391 0.6014 0.8815
1.500 0.3805 0.01118 0.00407 -0.0404 0.5920 0.8954
1.750 0.4142 0.01129 0.00415 -0.0416 0.5817 0.9085
2.000 0.4491 0.01141 0.00425 -0.0432 0.5715 0.9202
2.250 0.4859 0.01155 0.00433 -0.0452 0.5616 0.9295
2.500 0.5200 0.01168 0.00444 -0.0466 0.5510 0.9398
2.750 0.5567 0.01183 0.00456 -0.0486 0.5406 0.9478
3.000 0.5932 0.01199 0.00466 -0.0506 0.5305 0.9549
3.250 0.6294 0.01215 0.00481 -0.0526 0.5195 0.9617
3.500 0.6653 0.01232 0.00496 -0.0545 0.5093 0.9678
3.750 0.7003 0.01251 0.00511 -0.0562 0.4992 0.9743
4.000 0.7357 0.01269 0.00529 -0.0581 0.4885 0.9808
4.250 0.7694 0.01289 0.00548 -0.0596 0.4786 0.9884
4.500 0.8036 0.01311 0.00567 -0.0613 0.4687 0.9953
4.750 0.8397 0.01330 0.00588 -0.0634 0.4583 1.0000
5.000 0.8581 0.01347 0.00604 -0.0618 0.4501 1.0000
5.250 0.8768 0.01364 0.00622 -0.0602 0.4413 1.0000
5.500 0.8954 0.01384 0.00642 -0.0585 0.4332 1.0000
5.750 0.9141 0.01404 0.00663 -0.0569 0.4248 1.0000
6.000 0.9325 0.01426 0.00685 -0.0553 0.4155 1.0000
6.250 0.9496 0.01451 0.00707 -0.0533 0.4043 1.0000
6.500 0.9664 0.01477 0.00732 -0.0514 0.3909 1.0000
6.750 0.9832 0.01503 0.00758 -0.0494 0.3772 1.0000
7.000 1.0003 0.01531 0.00787 -0.0475 0.3650 1.0000
7.250 1.0164 0.01562 0.00817 -0.0454 0.3517 1.0000
7.500 1.0316 0.01595 0.00849 -0.0432 0.3368 1.0000
7.750 1.0465 0.01631 0.00884 -0.0409 0.3226 1.0000
8.000 1.0602 0.01670 0.00921 -0.0385 0.3062 1.0000
8.250 1.0722 0.01715 0.00961 -0.0358 0.2875 1.0000
8.500 1.0809 0.01771 0.01009 -0.0326 0.2649 1.0000
8.750 1.0866 0.01831 0.01061 -0.0288 0.2409 1.0000
9.000 1.0889 0.01905 0.01122 -0.0247 0.2135 1.0000
9.250 1.0872 0.02011 0.01207 -0.0202 0.1783 1.0000
9.500 1.0793 0.02166 0.01330 -0.0154 0.1276 1.0000
10.000 1.0603 0.02564 0.01673 -0.0070 0.0501 1.0000
10.250 1.0636 0.02710 0.01820 -0.0047 0.0438 1.0000
10.500 1.0705 0.02839 0.01958 -0.0029 0.0399 1.0000
10.750 1.0750 0.02992 0.02117 -0.0011 0.0370 1.0000
11.000 1.0786 0.03161 0.02293 0.0005 0.0348 1.0000
11.250 1.0845 0.03319 0.02463 0.0018 0.0328 1.0000
11.500 1.0885 0.03500 0.02653 0.0030 0.0310 1.0000
11.750 1.0894 0.03715 0.02874 0.0041 0.0295 1.0000
12.000 1.0888 0.03953 0.03121 0.0051 0.0282 1.0000
12.250 1.0916 0.04168 0.03350 0.0059 0.0271 1.0000
12.500 1.0924 0.04410 0.03601 0.0065 0.0261 1.0000
12.750 1.0922 0.04668 0.03869 0.0070 0.0252 1.0000
13.000 1.0911 0.04944 0.04154 0.0073 0.0244 1.0000
13.250 1.0889 0.05240 0.04457 0.0076 0.0238 1.0000
13.500 1.0846 0.05567 0.04790 0.0077 0.0232 1.0000
13.750 1.0832 0.05869 0.05100 0.0077 0.0226 1.0000
14.000 1.0840 0.06151 0.05394 0.0077 0.0220 1.0000
14.250 1.0848 0.06440 0.05692 0.0075 0.0213 1.0000
14.500 1.0856 0.06732 0.05992 0.0073 0.0206 1.0000
14.750 1.0865 0.07027 0.06296 0.0070 0.0199 1.0000
15.000 1.0873 0.07327 0.06601 0.0067 0.0194 1.0000
15.250 1.0878 0.07630 0.06909 0.0063 0.0189 1.0000
15.500 1.0882 0.07930 0.07212 0.0060 0.0185 1.0000
15.750 1.0905 0.08204 0.07492 0.0059 0.0182 1.0000
16.000 1.0936 0.08473 0.07773 0.0057 0.0178 1.0000
16.250 1.0969 0.08740 0.08050 0.0055 0.0174 1.0000
16.500 1.1003 0.09008 0.08327 0.0053 0.0170 1.0000
16.750 1.1034 0.09282 0.08611 0.0049 0.0166 1.0000
17.000 1.1063 0.09563 0.08902 0.0045 0.0163 1.0000
17.250 1.1086 0.09859 0.09208 0.0039 0.0160 1.0000
17.500 1.1102 0.10167 0.09524 0.0032 0.0157 1.0000
17.750 1.1114 0.10487 0.09852 0.0023 0.0154 1.0000
18.000 1.1126 0.10808 0.10180 0.0013 0.0151 1.0000
18.250 1.1139 0.11127 0.10504 0.0003 0.0148 1.0000
18.500 1.1156 0.11429 0.10810 -0.0006 0.0146 1.0000
18.750 1.1123 0.11851 0.11251 -0.0022 0.0143 1.0000
19.000 1.1083 0.12289 0.11707 -0.0040 0.0141 1.0000
19.250 1.1034 0.12749 0.12185 -0.0060 0.0139 1.0000
|
Polar data table (+)
Polar graphs
<< Back to GEMINI (smoothed) (geminism-il)