GEMINI (smoothed) (geminism-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: GEMINI (smoothed) (geminism-il) Reynolds number: 1,000,000 Max Cl/Cd: 110.58 at α=6.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-geminism-il-1000000.txt Download as CSV file: xf-geminism-il-1000000.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 = 1.000 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-18.500 -0.8964 0.11279 0.11036 -0.0356 1.0000 0.0122
-18.250 -0.9293 0.10282 0.10024 -0.0409 1.0000 0.0122
-18.000 -0.9582 0.09380 0.09109 -0.0458 1.0000 0.0122
-17.750 -0.9839 0.08559 0.08274 -0.0502 1.0000 0.0122
-17.500 -1.0066 0.07803 0.07506 -0.0543 1.0000 0.0122
-17.250 -1.0261 0.07121 0.06811 -0.0581 1.0000 0.0123
-17.000 -1.0428 0.06500 0.06177 -0.0615 1.0000 0.0123
-16.750 -1.0564 0.05952 0.05615 -0.0644 1.0000 0.0124
-16.500 -1.0666 0.05470 0.05121 -0.0669 1.0000 0.0124
-16.250 -1.0742 0.05042 0.04680 -0.0690 1.0000 0.0125
-16.000 -1.0786 0.04671 0.04299 -0.0707 1.0000 0.0125
-15.750 -1.0805 0.04346 0.03963 -0.0720 1.0000 0.0126
-15.500 -1.0942 0.03915 0.03516 -0.0731 1.0000 0.0128
-15.250 -1.1049 0.03548 0.03135 -0.0736 1.0000 0.0130
-15.000 -1.1091 0.03275 0.02852 -0.0734 1.0000 0.0132
-14.750 -1.1082 0.03069 0.02639 -0.0728 1.0000 0.0134
-14.500 -1.1044 0.02906 0.02469 -0.0719 1.0000 0.0136
-14.250 -1.0987 0.02771 0.02328 -0.0707 1.0000 0.0138
-14.000 -1.0923 0.02654 0.02205 -0.0692 1.0000 0.0141
-13.750 -1.0857 0.02550 0.02095 -0.0674 1.0000 0.0143
-13.500 -1.0793 0.02457 0.01996 -0.0652 1.0000 0.0146
-13.250 -1.0734 0.02377 0.01909 -0.0626 1.0000 0.0149
-13.000 -1.0682 0.02310 0.01836 -0.0595 1.0000 0.0151
-12.750 -1.0652 0.02256 0.01776 -0.0557 1.0000 0.0154
-12.500 -1.0673 0.02216 0.01731 -0.0507 1.0000 0.0156
-12.250 -1.0702 0.02184 0.01694 -0.0454 1.0000 0.0157
-12.000 -1.0498 0.02077 0.01577 -0.0452 0.9986 0.0162
-11.750 -1.0232 0.01960 0.01455 -0.0464 0.9958 0.0169
-11.500 -0.9942 0.01895 0.01389 -0.0474 0.9926 0.0175
-11.250 -0.9644 0.01839 0.01328 -0.0485 0.9891 0.0180
-11.000 -0.9341 0.01783 0.01268 -0.0497 0.9859 0.0187
-10.750 -0.9033 0.01730 0.01210 -0.0509 0.9832 0.0193
-10.500 -0.8706 0.01686 0.01161 -0.0523 0.9812 0.0197
-10.250 -0.8411 0.01575 0.01043 -0.0537 0.9794 0.0208
-10.000 -0.8084 0.01522 0.00989 -0.0553 0.9760 0.0217
-9.750 -0.7744 0.01482 0.00947 -0.0571 0.9716 0.0226
-9.500 -0.7372 0.01439 0.00900 -0.0595 0.9683 0.0236
-9.250 -0.7061 0.01404 0.00860 -0.0605 0.9590 0.0242
-9.000 -0.6763 0.01331 0.00780 -0.0616 0.9496 0.0254
-8.750 -0.6441 0.01280 0.00726 -0.0629 0.9403 0.0266
-8.500 -0.6128 0.01248 0.00689 -0.0640 0.9297 0.0278
-8.250 -0.5860 0.01223 0.00658 -0.0639 0.9164 0.0290
-8.000 -0.5599 0.01203 0.00631 -0.0637 0.9028 0.0298
-7.750 -0.5381 0.01155 0.00575 -0.0627 0.8883 0.0314
-7.500 -0.5144 0.01128 0.00542 -0.0620 0.8746 0.0331
-7.250 -0.4901 0.01108 0.00516 -0.0613 0.8617 0.0347
-7.000 -0.4658 0.01092 0.00491 -0.0607 0.8493 0.0360
-6.750 -0.4428 0.01065 0.00457 -0.0597 0.8373 0.0379
-6.500 -0.4197 0.01039 0.00429 -0.0589 0.8262 0.0407
-6.250 -0.3954 0.01024 0.00408 -0.0582 0.8157 0.0432
-6.000 -0.3716 0.01003 0.00382 -0.0574 0.8050 0.0464
-5.750 -0.3479 0.00981 0.00360 -0.0566 0.7952 0.0513
-5.500 -0.3240 0.00964 0.00338 -0.0558 0.7856 0.0571
-5.250 -0.2998 0.00944 0.00319 -0.0551 0.7762 0.0645
-5.000 -0.2764 0.00921 0.00298 -0.0543 0.7673 0.0783
-4.750 -0.2539 0.00891 0.00276 -0.0533 0.7580 0.1013
-4.500 -0.2331 0.00850 0.00253 -0.0520 0.7494 0.1501
-4.250 -0.2109 0.00821 0.00237 -0.0510 0.7406 0.1917
-4.000 -0.1873 0.00800 0.00224 -0.0502 0.7322 0.2211
-3.750 -0.1636 0.00784 0.00212 -0.0494 0.7235 0.2463
-3.500 -0.1395 0.00766 0.00201 -0.0486 0.7153 0.2736
-3.250 -0.1166 0.00746 0.00190 -0.0477 0.7069 0.3088
-3.000 -0.0933 0.00724 0.00180 -0.0468 0.6989 0.3498
-2.750 -0.0706 0.00705 0.00171 -0.0458 0.6907 0.3909
-2.500 -0.0474 0.00685 0.00164 -0.0449 0.6827 0.4358
-2.250 -0.0251 0.00668 0.00159 -0.0437 0.6746 0.4830
-2.000 -0.0014 0.00654 0.00155 -0.0428 0.6666 0.5203
-1.750 0.0218 0.00645 0.00152 -0.0418 0.6584 0.5540
-1.500 0.0463 0.00636 0.00150 -0.0411 0.6504 0.5823
-1.250 0.0699 0.00632 0.00148 -0.0402 0.6421 0.6094
-0.750 0.1199 0.00627 0.00145 -0.0389 0.6256 0.6449
-0.500 0.1454 0.00624 0.00144 -0.0383 0.6171 0.6610
0.000 0.1954 0.00622 0.00144 -0.0370 0.5996 0.6927
0.500 0.2445 0.00621 0.00146 -0.0356 0.5814 0.7273
0.750 0.2690 0.00620 0.00148 -0.0348 0.5724 0.7460
1.250 0.3177 0.00620 0.00154 -0.0333 0.5532 0.7843
1.500 0.3419 0.00622 0.00158 -0.0324 0.5438 0.8052
1.750 0.3658 0.00622 0.00164 -0.0315 0.5338 0.8319
2.000 0.3907 0.00621 0.00171 -0.0308 0.5242 0.8629
2.250 0.4168 0.00626 0.00178 -0.0304 0.5142 0.8892
2.500 0.4465 0.00631 0.00186 -0.0309 0.5040 0.9075
2.750 0.4785 0.00639 0.00194 -0.0318 0.4943 0.9234
3.250 0.5536 0.00661 0.00213 -0.0365 0.4734 0.9471
3.500 0.5949 0.00675 0.00224 -0.0397 0.4633 0.9544
4.000 0.6784 0.00706 0.00249 -0.0463 0.4427 0.9638
4.250 0.7175 0.00723 0.00263 -0.0489 0.4332 0.9668
4.750 0.7894 0.00762 0.00295 -0.0529 0.4098 0.9736
5.000 0.8227 0.00781 0.00311 -0.0542 0.3987 0.9777
5.250 0.8565 0.00803 0.00328 -0.0558 0.3867 0.9815
5.750 0.9212 0.00846 0.00363 -0.0582 0.3621 0.9911
6.000 0.9539 0.00869 0.00383 -0.0595 0.3504 0.9946
6.250 0.9886 0.00894 0.00402 -0.0614 0.3327 0.9968
6.500 1.0225 0.00925 0.00423 -0.0632 0.3125 0.9988
6.750 1.0533 0.00955 0.00445 -0.0642 0.2922 1.0000
7.000 1.0682 0.00983 0.00465 -0.0619 0.2729 1.0000
7.250 1.0814 0.01020 0.00490 -0.0592 0.2500 1.0000
7.500 1.0931 0.01068 0.00523 -0.0562 0.2208 1.0000
7.750 1.1017 0.01136 0.00568 -0.0528 0.1820 1.0000
8.000 1.1053 0.01231 0.00633 -0.0486 0.1321 1.0000
8.250 1.0938 0.01396 0.00750 -0.0417 0.0525 1.0000
8.500 1.1033 0.01455 0.00803 -0.0385 0.0404 1.0000
8.750 1.1118 0.01500 0.00847 -0.0349 0.0351 1.0000
9.000 1.1230 0.01539 0.00887 -0.0320 0.0323 1.0000
9.250 1.1322 0.01592 0.00940 -0.0288 0.0288 1.0000
9.500 1.1462 0.01632 0.00983 -0.0266 0.0272 1.0000
9.750 1.1587 0.01683 0.01035 -0.0243 0.0252 1.0000
10.000 1.1684 0.01753 0.01107 -0.0216 0.0229 1.0000
10.250 1.1831 0.01803 0.01160 -0.0199 0.0217 1.0000
10.500 1.1961 0.01866 0.01224 -0.0180 0.0202 1.0000
10.750 1.2046 0.01957 0.01318 -0.0156 0.0186 1.0000
11.000 1.2175 0.02029 0.01395 -0.0140 0.0178 1.0000
11.250 1.2301 0.02107 0.01477 -0.0124 0.0169 1.0000
11.500 1.2417 0.02195 0.01567 -0.0108 0.0161 1.0000
11.750 1.2507 0.02305 0.01681 -0.0092 0.0153 1.0000
12.000 1.2551 0.02455 0.01837 -0.0072 0.0145 1.0000
12.250 1.2669 0.02557 0.01944 -0.0061 0.0141 1.0000
12.500 1.2770 0.02678 0.02071 -0.0049 0.0137 1.0000
12.750 1.2856 0.02813 0.02212 -0.0038 0.0132 1.0000
13.000 1.2936 0.02960 0.02363 -0.0028 0.0129 1.0000
13.250 1.3003 0.03122 0.02530 -0.0018 0.0125 1.0000
13.500 1.3046 0.03311 0.02725 -0.0008 0.0122 1.0000
13.750 1.3044 0.03546 0.02967 0.0002 0.0118 1.0000
14.000 1.2984 0.03848 0.03279 0.0011 0.0115 1.0000
14.250 1.2992 0.04093 0.03533 0.0017 0.0114 1.0000
14.750 1.3043 0.04571 0.04027 0.0024 0.0111 1.0000
15.000 1.3052 0.04840 0.04303 0.0025 0.0109 1.0000
15.250 1.3048 0.05126 0.04598 0.0026 0.0107 1.0000
15.500 1.3037 0.05429 0.04909 0.0025 0.0106 1.0000
15.750 1.3026 0.05740 0.05227 0.0023 0.0104 1.0000
16.000 1.3012 0.06061 0.05556 0.0020 0.0103 1.0000
16.250 1.2996 0.06387 0.05889 0.0016 0.0101 1.0000
16.500 1.2974 0.06727 0.06236 0.0012 0.0099 1.0000
16.750 1.2947 0.07079 0.06596 0.0006 0.0098 1.0000
17.000 1.2914 0.07445 0.06969 -0.0001 0.0096 1.0000
17.250 1.2870 0.07826 0.07357 -0.0009 0.0095 1.0000
17.500 1.2813 0.08229 0.07767 -0.0017 0.0094 1.0000
17.750 1.2745 0.08651 0.08197 -0.0027 0.0093 1.0000
18.000 1.2669 0.09088 0.08641 -0.0038 0.0092 1.0000
18.250 1.2583 0.09534 0.09096 -0.0048 0.0090 1.0000
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