GEMINI (smoothed) (geminism-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: GEMINI (smoothed) (geminism-il) Reynolds number: 500,000 Max Cl/Cd: 86.67 at α=6.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-geminism-il-500000-n5.txt Download as CSV file: xf-geminism-il-500000-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 = 0.500 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-18.000 -0.8258 0.11672 0.11362 -0.0351 1.0000 0.0126
-17.750 -0.8584 0.10644 0.10319 -0.0405 1.0000 0.0126
-17.500 -0.8868 0.09729 0.09390 -0.0454 1.0000 0.0126
-17.250 -0.9119 0.08898 0.08545 -0.0498 1.0000 0.0126
-17.000 -0.9346 0.08129 0.07761 -0.0540 1.0000 0.0126
-16.750 -0.9541 0.07430 0.07048 -0.0579 1.0000 0.0126
-16.500 -0.9724 0.06780 0.06385 -0.0614 1.0000 0.0127
-16.250 -0.9884 0.06189 0.05781 -0.0646 1.0000 0.0128
-16.000 -1.0016 0.05664 0.05243 -0.0673 1.0000 0.0129
-15.750 -1.0116 0.05201 0.04769 -0.0696 1.0000 0.0130
-15.500 -1.0187 0.04801 0.04358 -0.0714 1.0000 0.0131
-15.250 -1.0229 0.04454 0.04001 -0.0727 1.0000 0.0133
-15.000 -1.0249 0.04155 0.03692 -0.0736 1.0000 0.0134
-14.750 -1.0252 0.03893 0.03420 -0.0741 1.0000 0.0136
-14.500 -1.0243 0.03660 0.03177 -0.0742 1.0000 0.0138
-14.250 -1.0227 0.03453 0.02960 -0.0738 1.0000 0.0140
-14.000 -1.0203 0.03270 0.02768 -0.0731 1.0000 0.0142
-13.750 -1.0174 0.03107 0.02594 -0.0719 1.0000 0.0145
-13.500 -1.0141 0.02962 0.02440 -0.0704 1.0000 0.0147
-13.250 -1.0105 0.02834 0.02302 -0.0685 1.0000 0.0150
-13.000 -1.0068 0.02721 0.02180 -0.0662 1.0000 0.0153
-12.750 -1.0030 0.02623 0.02072 -0.0636 1.0000 0.0155
-12.500 -1.0000 0.02539 0.01979 -0.0604 1.0000 0.0158
-12.250 -1.0003 0.02463 0.01897 -0.0564 1.0000 0.0160
-12.000 -1.0066 0.02399 0.01828 -0.0509 1.0000 0.0162
-11.750 -0.9864 0.02310 0.01735 -0.0508 0.9969 0.0167
-11.500 -0.9621 0.02234 0.01653 -0.0511 0.9893 0.0172
-11.250 -0.9351 0.02162 0.01575 -0.0519 0.9841 0.0179
-11.000 -0.9058 0.02089 0.01494 -0.0531 0.9810 0.0186
-10.750 -0.8750 0.02017 0.01413 -0.0546 0.9787 0.0193
-10.500 -0.8479 0.01952 0.01339 -0.0552 0.9724 0.0198
-10.250 -0.8182 0.01865 0.01247 -0.0566 0.9680 0.0206
-10.000 -0.7906 0.01805 0.01183 -0.0573 0.9597 0.0214
-9.750 -0.7594 0.01749 0.01122 -0.0586 0.9528 0.0222
-9.500 -0.7269 0.01695 0.01061 -0.0601 0.9454 0.0233
-9.250 -0.6947 0.01645 0.01002 -0.0616 0.9372 0.0242
-9.000 -0.6635 0.01580 0.00931 -0.0629 0.9286 0.0253
-8.750 -0.6367 0.01533 0.00879 -0.0631 0.9165 0.0263
-8.500 -0.6100 0.01494 0.00835 -0.0633 0.9037 0.0275
-8.250 -0.5840 0.01459 0.00791 -0.0631 0.8907 0.0288
-8.000 -0.5587 0.01428 0.00749 -0.0629 0.8776 0.0298
-7.750 -0.5354 0.01387 0.00701 -0.0622 0.8648 0.0312
-7.500 -0.5118 0.01355 0.00663 -0.0615 0.8521 0.0327
-7.250 -0.4881 0.01329 0.00629 -0.0609 0.8403 0.0344
-7.000 -0.4641 0.01305 0.00597 -0.0602 0.8293 0.0361
-6.500 -0.4176 0.01250 0.00532 -0.0586 0.8076 0.0405
-6.250 -0.3936 0.01229 0.00504 -0.0579 0.7977 0.0432
-6.000 -0.3699 0.01207 0.00476 -0.0571 0.7876 0.0466
-5.750 -0.3462 0.01184 0.00451 -0.0564 0.7778 0.0512
-5.500 -0.3222 0.01164 0.00426 -0.0557 0.7685 0.0561
-5.250 -0.2983 0.01143 0.00403 -0.0550 0.7586 0.0630
-5.000 -0.2747 0.01121 0.00380 -0.0542 0.7495 0.0724
-4.750 -0.2512 0.01098 0.00358 -0.0534 0.7403 0.0856
-4.500 -0.2282 0.01070 0.00335 -0.0525 0.7314 0.1061
-4.250 -0.2065 0.01035 0.00313 -0.0515 0.7228 0.1465
-4.000 -0.1838 0.01006 0.00297 -0.0506 0.7142 0.1842
-3.500 -0.1363 0.00968 0.00268 -0.0491 0.6974 0.2356
-3.250 -0.1128 0.00950 0.00255 -0.0483 0.6893 0.2625
-3.000 -0.0895 0.00927 0.00242 -0.0474 0.6808 0.2976
-2.750 -0.0673 0.00903 0.00231 -0.0464 0.6727 0.3415
-2.500 -0.0454 0.00876 0.00221 -0.0452 0.6642 0.3950
-2.250 -0.0238 0.00855 0.00213 -0.0440 0.6562 0.4470
-2.000 -0.0016 0.00836 0.00208 -0.0429 0.6476 0.4942
-1.750 0.0212 0.00824 0.00204 -0.0418 0.6396 0.5305
-1.500 0.0455 0.00818 0.00200 -0.0410 0.6309 0.5526
-1.250 0.0701 0.00814 0.00197 -0.0403 0.6227 0.5714
-1.000 0.0949 0.00811 0.00195 -0.0397 0.6138 0.5880
-0.750 0.1197 0.00809 0.00193 -0.0390 0.6053 0.6058
-0.500 0.1442 0.00807 0.00192 -0.0383 0.5963 0.6233
-0.250 0.1691 0.00806 0.00191 -0.0376 0.5874 0.6401
0.250 0.2184 0.00805 0.00192 -0.0362 0.5694 0.6735
0.500 0.2429 0.00806 0.00194 -0.0355 0.5603 0.6893
0.750 0.2674 0.00806 0.00196 -0.0348 0.5506 0.7067
1.000 0.2912 0.00805 0.00200 -0.0339 0.5417 0.7301
1.250 0.3140 0.00803 0.00205 -0.0327 0.5322 0.7614
1.500 0.3380 0.00801 0.00211 -0.0318 0.5227 0.7913
1.750 0.3629 0.00804 0.00218 -0.0312 0.5138 0.8125
2.000 0.3890 0.00808 0.00224 -0.0308 0.5043 0.8325
2.250 0.4157 0.00813 0.00233 -0.0306 0.4952 0.8525
2.500 0.4437 0.00821 0.00241 -0.0307 0.4857 0.8719
2.750 0.4739 0.00829 0.00251 -0.0312 0.4765 0.8901
3.000 0.5063 0.00841 0.00263 -0.0323 0.4671 0.9065
3.250 0.5422 0.00853 0.00275 -0.0343 0.4573 0.9204
3.500 0.5797 0.00868 0.00289 -0.0366 0.4480 0.9315
3.750 0.6169 0.00885 0.00303 -0.0388 0.4384 0.9411
4.000 0.6551 0.00901 0.00318 -0.0413 0.4291 0.9493
4.250 0.6945 0.00920 0.00335 -0.0441 0.4198 0.9544
4.500 0.7336 0.00938 0.00352 -0.0468 0.4104 0.9588
4.750 0.7682 0.00957 0.00369 -0.0485 0.4019 0.9647
5.000 0.8047 0.00978 0.00390 -0.0506 0.3917 0.9681
5.250 0.8385 0.01002 0.00410 -0.0522 0.3782 0.9725
5.500 0.8705 0.01026 0.00431 -0.0534 0.3647 0.9779
5.750 0.9010 0.01053 0.00453 -0.0543 0.3503 0.9844
6.000 0.9286 0.01082 0.00478 -0.0546 0.3363 0.9937
6.250 0.9606 0.01111 0.00503 -0.0559 0.3222 0.9980
6.500 0.9906 0.01143 0.00530 -0.0568 0.3045 1.0000
6.750 1.0059 0.01174 0.00554 -0.0546 0.2864 1.0000
7.000 1.0213 0.01209 0.00580 -0.0523 0.2685 1.0000
7.250 1.0358 0.01249 0.00611 -0.0500 0.2467 1.0000
7.500 1.0480 0.01303 0.00650 -0.0472 0.2193 1.0000
7.750 1.0576 0.01367 0.00697 -0.0441 0.1872 1.0000
8.000 1.0630 0.01451 0.00757 -0.0403 0.1486 1.0000
8.250 1.0546 0.01579 0.00848 -0.0341 0.0877 1.0000
8.500 1.0478 0.01690 0.00936 -0.0282 0.0488 1.0000
8.750 1.0563 0.01752 0.00997 -0.0250 0.0400 1.0000
9.000 1.0668 0.01812 0.01057 -0.0224 0.0350 1.0000
9.250 1.0793 0.01869 0.01116 -0.0202 0.0318 1.0000
9.500 1.0903 0.01937 0.01185 -0.0179 0.0289 1.0000
9.750 1.1035 0.01999 0.01252 -0.0160 0.0271 1.0000
10.000 1.1157 0.02069 0.01326 -0.0141 0.0253 1.0000
10.250 1.1264 0.02153 0.01412 -0.0122 0.0236 1.0000
10.500 1.1381 0.02236 0.01500 -0.0105 0.0222 1.0000
10.750 1.1499 0.02322 0.01591 -0.0089 0.0208 1.0000
11.000 1.1605 0.02421 0.01693 -0.0074 0.0194 1.0000
11.250 1.1692 0.02538 0.01813 -0.0058 0.0183 1.0000
11.500 1.1799 0.02647 0.01929 -0.0046 0.0174 1.0000
11.750 1.1895 0.02768 0.02057 -0.0033 0.0166 1.0000
12.000 1.1980 0.02903 0.02197 -0.0021 0.0158 1.0000
12.250 1.2052 0.03054 0.02352 -0.0010 0.0152 1.0000
12.500 1.2098 0.03233 0.02536 0.0001 0.0146 1.0000
12.750 1.2165 0.03400 0.02712 0.0010 0.0142 1.0000
13.000 1.2221 0.03583 0.02902 0.0018 0.0137 1.0000
13.250 1.2267 0.03780 0.03108 0.0025 0.0133 1.0000
13.500 1.2306 0.03989 0.03325 0.0031 0.0129 1.0000
13.750 1.2337 0.04212 0.03555 0.0035 0.0126 1.0000
14.000 1.2359 0.04451 0.03802 0.0039 0.0123 1.0000
14.250 1.2367 0.04713 0.04070 0.0041 0.0120 1.0000
14.500 1.2355 0.05005 0.04369 0.0043 0.0117 1.0000
14.750 1.2328 0.05321 0.04693 0.0043 0.0114 1.0000
15.000 1.2332 0.05611 0.04992 0.0041 0.0112 1.0000
15.250 1.2326 0.05920 0.05312 0.0039 0.0110 1.0000
15.500 1.2311 0.06243 0.05645 0.0036 0.0108 1.0000
15.750 1.2292 0.06579 0.05990 0.0031 0.0106 1.0000
16.000 1.2266 0.06930 0.06350 0.0025 0.0104 1.0000
16.250 1.2238 0.07290 0.06718 0.0019 0.0102 1.0000
16.500 1.2206 0.07656 0.07093 0.0012 0.0101 1.0000
16.750 1.2172 0.08031 0.07476 0.0004 0.0099 1.0000
17.000 1.2137 0.08412 0.07866 -0.0005 0.0098 1.0000
17.250 1.2103 0.08797 0.08259 -0.0015 0.0096 1.0000
17.500 1.2065 0.09190 0.08660 -0.0025 0.0095 1.0000
17.750 1.2023 0.09590 0.09068 -0.0036 0.0094 1.0000
18.000 1.1982 0.09995 0.09480 -0.0048 0.0093 1.0000
18.250 1.1940 0.10402 0.09895 -0.0060 0.0092 1.0000
18.500 1.1894 0.10820 0.10321 -0.0074 0.0090 1.0000
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