GEMINI (smoothed) (geminism-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: GEMINI (smoothed) (geminism-il) Reynolds number: 500,000 Max Cl/Cd: 92.73 at α=6.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-geminism-il-500000.txt Download as CSV file: xf-geminism-il-500000.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 = 0.500 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-15.750 -0.7035 0.10249 0.09977 -0.0451 1.0000 0.0197
-15.500 -0.7687 0.08536 0.08242 -0.0554 1.0000 0.0193
-15.250 -0.8079 0.07440 0.07125 -0.0625 1.0000 0.0191
-15.000 -0.8377 0.06600 0.06265 -0.0679 1.0000 0.0190
-14.750 -0.8607 0.05935 0.05581 -0.0718 1.0000 0.0191
-14.500 -0.8792 0.05391 0.05017 -0.0746 1.0000 0.0191
-14.250 -0.8939 0.04944 0.04551 -0.0763 1.0000 0.0193
-14.000 -0.9056 0.04574 0.04162 -0.0772 1.0000 0.0194
-13.750 -0.9146 0.04274 0.03845 -0.0772 1.0000 0.0196
-13.500 -0.9215 0.04033 0.03586 -0.0764 1.0000 0.0197
-13.250 -0.9360 0.03703 0.03235 -0.0746 1.0000 0.0200
-13.000 -0.9427 0.03451 0.02969 -0.0724 1.0000 0.0203
-12.750 -0.9428 0.03295 0.02807 -0.0701 1.0000 0.0206
-12.500 -0.9417 0.03179 0.02686 -0.0674 1.0000 0.0209
-12.250 -0.9416 0.03083 0.02585 -0.0641 1.0000 0.0212
-12.000 -0.9441 0.03003 0.02497 -0.0598 1.0000 0.0215
-11.750 -0.9502 0.02935 0.02423 -0.0546 1.0000 0.0218
-11.500 -0.9537 0.02864 0.02344 -0.0498 1.0000 0.0222
-11.250 -0.9568 0.02797 0.02270 -0.0450 1.0000 0.0225
-11.000 -0.9499 0.02712 0.02176 -0.0421 0.9993 0.0230
-10.750 -0.9194 0.02595 0.02042 -0.0439 0.9966 0.0238
-10.500 -0.8894 0.02489 0.01918 -0.0454 0.9933 0.0245
-10.250 -0.8628 0.02309 0.01733 -0.0466 0.9896 0.0257
-10.000 -0.8303 0.02233 0.01655 -0.0484 0.9865 0.0267
-9.750 -0.7989 0.02151 0.01566 -0.0499 0.9828 0.0278
-9.500 -0.7651 0.02067 0.01472 -0.0518 0.9804 0.0289
-9.250 -0.7293 0.02001 0.01394 -0.0539 0.9786 0.0298
-9.000 -0.7036 0.01849 0.01239 -0.0545 0.9729 0.0314
-8.750 -0.6680 0.01784 0.01173 -0.0567 0.9699 0.0330
-8.500 -0.6346 0.01722 0.01107 -0.0583 0.9648 0.0345
-8.250 -0.6012 0.01662 0.01039 -0.0599 0.9588 0.0359
-8.000 -0.5723 0.01567 0.00938 -0.0607 0.9510 0.0376
-7.750 -0.5394 0.01499 0.00869 -0.0622 0.9442 0.0398
-7.500 -0.5101 0.01452 0.00818 -0.0628 0.9344 0.0418
-7.250 -0.4794 0.01410 0.00767 -0.0636 0.9252 0.0437
-7.000 -0.4541 0.01344 0.00694 -0.0634 0.9141 0.0464
-6.750 -0.4305 0.01304 0.00652 -0.0627 0.9013 0.0493
-6.500 -0.4058 0.01273 0.00614 -0.0622 0.8894 0.0522
-6.250 -0.3822 0.01232 0.00565 -0.0614 0.8780 0.0558
-6.000 -0.3580 0.01196 0.00525 -0.0607 0.8670 0.0612
-5.750 -0.3354 0.01164 0.00489 -0.0597 0.8553 0.0679
-5.500 -0.3121 0.01133 0.00455 -0.0589 0.8446 0.0772
-5.250 -0.2899 0.01090 0.00417 -0.0579 0.8345 0.0971
-5.000 -0.2713 0.01032 0.00384 -0.0563 0.8235 0.1514
-4.750 -0.2501 0.00991 0.00362 -0.0551 0.8139 0.2077
-4.500 -0.2273 0.00964 0.00342 -0.0542 0.8044 0.2431
-4.250 -0.2048 0.00937 0.00325 -0.0532 0.7949 0.2765
-4.000 -0.1819 0.00912 0.00307 -0.0523 0.7863 0.3149
-3.750 -0.1604 0.00884 0.00293 -0.0510 0.7769 0.3579
-3.500 -0.1382 0.00860 0.00280 -0.0499 0.7685 0.4040
-3.250 -0.1167 0.00837 0.00271 -0.0487 0.7594 0.4506
-3.000 -0.0945 0.00819 0.00262 -0.0475 0.7511 0.4950
-2.750 -0.0723 0.00805 0.00256 -0.0462 0.7422 0.5330
-2.500 -0.0496 0.00793 0.00252 -0.0451 0.7340 0.5677
-2.250 -0.0267 0.00784 0.00247 -0.0439 0.7254 0.5987
-2.000 -0.0036 0.00778 0.00245 -0.0428 0.7171 0.6278
-1.750 0.0197 0.00771 0.00242 -0.0417 0.7087 0.6526
-1.500 0.0441 0.00767 0.00239 -0.0409 0.7003 0.6715
-1.250 0.0687 0.00765 0.00235 -0.0401 0.6920 0.6891
-1.000 0.0933 0.00761 0.00233 -0.0394 0.6834 0.7058
-0.750 0.1179 0.00760 0.00230 -0.0386 0.6751 0.7235
-0.500 0.1424 0.00756 0.00230 -0.0378 0.6663 0.7417
0.000 0.1918 0.00751 0.00230 -0.0362 0.6488 0.7788
0.250 0.2169 0.00752 0.00231 -0.0355 0.6405 0.7980
0.500 0.2423 0.00750 0.00234 -0.0349 0.6310 0.8173
0.750 0.2681 0.00752 0.00237 -0.0344 0.6222 0.8376
1.000 0.2948 0.00754 0.00241 -0.0340 0.6128 0.8600
1.250 0.3239 0.00757 0.00249 -0.0342 0.6032 0.8848
1.500 0.3534 0.00765 0.00256 -0.0344 0.5938 0.9065
1.750 0.3866 0.00772 0.00263 -0.0355 0.5834 0.9219
2.000 0.4241 0.00783 0.00272 -0.0377 0.5731 0.9337
2.250 0.4631 0.00797 0.00280 -0.0402 0.5625 0.9433
2.500 0.5007 0.00809 0.00290 -0.0424 0.5513 0.9528
2.750 0.5445 0.00825 0.00303 -0.0460 0.5400 0.9568
3.000 0.5824 0.00843 0.00315 -0.0483 0.5292 0.9629
3.250 0.6211 0.00861 0.00330 -0.0508 0.5179 0.9669
3.500 0.6595 0.00879 0.00345 -0.0532 0.5069 0.9705
3.750 0.6942 0.00899 0.00360 -0.0548 0.4966 0.9763
4.000 0.7329 0.00918 0.00376 -0.0574 0.4856 0.9797
4.250 0.7689 0.00936 0.00392 -0.0594 0.4752 0.9849
4.500 0.8059 0.00955 0.00408 -0.0616 0.4652 0.9894
4.750 0.8422 0.00976 0.00426 -0.0637 0.4541 0.9940
5.000 0.8805 0.00991 0.00439 -0.0663 0.4410 0.9973
5.250 0.9184 0.01007 0.00454 -0.0688 0.4283 1.0000
5.500 0.9364 0.01022 0.00465 -0.0671 0.4176 1.0000
5.750 0.9543 0.01037 0.00477 -0.0653 0.4068 1.0000
6.000 0.9730 0.01050 0.00491 -0.0637 0.3970 1.0000
6.250 0.9904 0.01068 0.00507 -0.0618 0.3869 1.0000
6.500 1.0074 0.01088 0.00524 -0.0598 0.3749 1.0000
6.750 1.0254 0.01106 0.00542 -0.0580 0.3624 1.0000
7.000 1.0431 0.01128 0.00562 -0.0561 0.3499 1.0000
7.250 1.0603 0.01154 0.00584 -0.0542 0.3353 1.0000
7.500 1.0768 0.01184 0.00609 -0.0521 0.3183 1.0000
7.750 1.0919 0.01221 0.00638 -0.0499 0.2984 1.0000
8.000 1.1062 0.01263 0.00671 -0.0475 0.2742 1.0000
8.250 1.1171 0.01319 0.00713 -0.0445 0.2441 1.0000
8.500 1.1218 0.01404 0.00771 -0.0405 0.2012 1.0000
8.750 1.1140 0.01525 0.00855 -0.0344 0.1435 1.0000
9.000 1.0921 0.01701 0.00982 -0.0262 0.0687 1.0000
9.250 1.0905 0.01816 0.01085 -0.0217 0.0478 1.0000
9.500 1.0981 0.01900 0.01171 -0.0187 0.0415 1.0000
9.750 1.1057 0.01990 0.01263 -0.0160 0.0376 1.0000
10.000 1.1127 0.02090 0.01367 -0.0134 0.0346 1.0000
10.250 1.1228 0.02179 0.01463 -0.0114 0.0322 1.0000
10.500 1.1289 0.02298 0.01585 -0.0091 0.0300 1.0000
10.750 1.1324 0.02442 0.01735 -0.0068 0.0281 1.0000
11.000 1.1424 0.02551 0.01851 -0.0053 0.0266 1.0000
11.250 1.1499 0.02683 0.01989 -0.0037 0.0252 1.0000
11.500 1.1537 0.02851 0.02161 -0.0021 0.0241 1.0000
11.750 1.1474 0.03108 0.02427 -0.0001 0.0230 1.0000
12.000 1.1549 0.03265 0.02592 0.0009 0.0224 1.0000
12.250 1.1604 0.03445 0.02780 0.0019 0.0217 1.0000
12.500 1.1644 0.03643 0.02986 0.0027 0.0210 1.0000
12.750 1.1676 0.03856 0.03206 0.0035 0.0204 1.0000
13.000 1.1696 0.04085 0.03440 0.0042 0.0198 1.0000
13.250 1.1699 0.04336 0.03697 0.0047 0.0193 1.0000
13.500 1.1662 0.04634 0.04001 0.0053 0.0188 1.0000
13.750 1.1571 0.04988 0.04363 0.0060 0.0184 1.0000
14.000 1.1623 0.05212 0.04596 0.0061 0.0181 1.0000
14.250 1.1660 0.05457 0.04849 0.0062 0.0177 1.0000
14.500 1.1686 0.05715 0.05116 0.0062 0.0172 1.0000
14.750 1.1706 0.05983 0.05391 0.0063 0.0169 1.0000
15.000 1.1724 0.06255 0.05670 0.0062 0.0165 1.0000
15.250 1.1744 0.06528 0.05950 0.0061 0.0162 1.0000
15.500 1.1765 0.06804 0.06231 0.0059 0.0159 1.0000
15.750 1.1784 0.07084 0.06516 0.0057 0.0156 1.0000
16.000 1.1803 0.07359 0.06797 0.0055 0.0153 1.0000
16.250 1.1821 0.07629 0.07071 0.0055 0.0151 1.0000
16.500 1.1849 0.07852 0.07297 0.0062 0.0148 1.0000
16.750 1.1887 0.08073 0.07525 0.0068 0.0145 1.0000
17.000 1.1910 0.08362 0.07825 0.0063 0.0144 1.0000
17.250 1.1925 0.08664 0.08137 0.0058 0.0142 1.0000
17.500 1.1936 0.08974 0.08459 0.0052 0.0140 1.0000
17.750 1.1942 0.09295 0.08791 0.0045 0.0138 1.0000
18.000 1.1940 0.09632 0.09139 0.0037 0.0135 1.0000
18.250 1.1934 0.09978 0.09495 0.0028 0.0133 1.0000
18.500 1.1922 0.10335 0.09864 0.0017 0.0131 1.0000
18.750 1.1905 0.10704 0.10243 0.0005 0.0129 1.0000
19.000 1.1887 0.11078 0.10627 -0.0008 0.0128 1.0000
19.250 1.1859 0.11475 0.11034 -0.0022 0.0126 1.0000
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