S1016 (s1016-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: S1016 (s1016-il) Reynolds number: 500,000 Max Cl/Cd: 41.77 at α=10.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-s1016-il-500000-n5.txt Download as CSV file: xf-s1016-il-500000-n5.csv |
XFOIL Version 6.96
Calculated polar for: S1016
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
------ -------- --------- --------- -------- -------- --------
-19.750 -1.1231 0.08385 0.07886 -0.0565 0.8716 0.0235
-19.500 -1.1331 0.07882 0.07372 -0.0590 0.8699 0.0239
-19.250 -1.1412 0.07420 0.06897 -0.0611 0.8681 0.0244
-19.000 -1.1462 0.07017 0.06481 -0.0628 0.8664 0.0249
-18.750 -1.1512 0.06625 0.06077 -0.0644 0.8647 0.0253
-18.500 -1.1541 0.06273 0.05713 -0.0656 0.8630 0.0259
-18.250 -1.1585 0.05917 0.05347 -0.0666 0.8614 0.0265
-17.750 -1.1607 0.05315 0.04727 -0.0680 0.8586 0.0279
-17.500 -1.1589 0.05060 0.04464 -0.0683 0.8573 0.0286
-17.250 -1.1551 0.04834 0.04228 -0.0685 0.8560 0.0295
-17.000 -1.1505 0.04623 0.04009 -0.0686 0.8547 0.0304
-16.750 -1.1477 0.04402 0.03782 -0.0684 0.8534 0.0312
-16.500 -1.1430 0.04208 0.03581 -0.0682 0.8521 0.0321
-16.250 -1.1367 0.04035 0.03401 -0.0678 0.8508 0.0332
-16.000 -1.1290 0.03880 0.03238 -0.0673 0.8496 0.0343
-15.750 -1.1199 0.03740 0.03090 -0.0668 0.8484 0.0353
-15.500 -1.1132 0.03586 0.02931 -0.0661 0.8471 0.0367
-15.250 -1.1044 0.03455 0.02795 -0.0653 0.8458 0.0381
-15.000 -1.0942 0.03337 0.02670 -0.0645 0.8445 0.0394
-14.750 -1.0830 0.03230 0.02555 -0.0638 0.8434 0.0407
-14.500 -1.0728 0.03117 0.02438 -0.0629 0.8424 0.0421
-14.250 -1.0615 0.03013 0.02331 -0.0620 0.8416 0.0437
-14.000 -1.0489 0.02920 0.02233 -0.0611 0.8408 0.0455
-13.750 -1.0349 0.02837 0.02145 -0.0603 0.8400 0.0470
-13.500 -1.0230 0.02744 0.02051 -0.0593 0.8391 0.0491
-13.250 -1.0093 0.02663 0.01967 -0.0584 0.8382 0.0511
-13.000 -0.9945 0.02591 0.01891 -0.0575 0.8373 0.0532
-12.750 -0.9796 0.02521 0.01816 -0.0566 0.8364 0.0550
-12.500 -0.9655 0.02446 0.01742 -0.0555 0.8355 0.0575
-12.250 -0.9497 0.02383 0.01676 -0.0546 0.8347 0.0600
-12.000 -0.9330 0.02326 0.01615 -0.0537 0.8338 0.0625
-11.750 -0.9182 0.02259 0.01548 -0.0526 0.8330 0.0655
-11.500 -0.9015 0.02203 0.01490 -0.0517 0.8322 0.0687
-11.250 -0.8836 0.02154 0.01438 -0.0509 0.8314 0.0717
-11.000 -0.8675 0.02096 0.01381 -0.0498 0.8306 0.0754
-10.750 -0.8501 0.02046 0.01330 -0.0489 0.8299 0.0792
-10.500 -0.8318 0.02002 0.01283 -0.0480 0.8292 0.0826
-10.250 -0.8145 0.01952 0.01234 -0.0470 0.8284 0.0867
-10.000 -0.7960 0.01910 0.01190 -0.0461 0.8276 0.0909
-9.750 -0.7775 0.01869 0.01148 -0.0451 0.8266 0.0950
-9.500 -0.7594 0.01826 0.01106 -0.0441 0.8258 0.1001
-9.250 -0.7396 0.01790 0.01069 -0.0434 0.8253 0.1048
-9.000 -0.7208 0.01749 0.01031 -0.0425 0.8247 0.1099
-8.750 -0.7013 0.01712 0.00995 -0.0416 0.8240 0.1158
-8.500 -0.6815 0.01677 0.00961 -0.0408 0.8234 0.1209
-8.250 -0.6623 0.01640 0.00927 -0.0398 0.8227 0.1275
-7.750 -0.6225 0.01573 0.00865 -0.0381 0.8212 0.1410
-7.250 -0.5826 0.01510 0.00808 -0.0363 0.8196 0.1563
-7.000 -0.5622 0.01481 0.00781 -0.0354 0.8187 0.1649
-6.750 -0.5428 0.01448 0.00753 -0.0344 0.8176 0.1754
-6.500 -0.5233 0.01417 0.00727 -0.0334 0.8167 0.1863
-6.250 -0.5032 0.01390 0.00703 -0.0324 0.8159 0.1971
-6.000 -0.4837 0.01360 0.00678 -0.0313 0.8151 0.2101
-5.750 -0.4650 0.01328 0.00654 -0.0301 0.8143 0.2248
-5.500 -0.4462 0.01298 0.00630 -0.0289 0.8135 0.2393
-5.250 -0.4281 0.01267 0.00605 -0.0275 0.8124 0.2562
-5.000 -0.4104 0.01235 0.00581 -0.0260 0.8114 0.2745
-4.750 -0.3936 0.01204 0.00558 -0.0244 0.8106 0.2948
-4.500 -0.3787 0.01174 0.00537 -0.0223 0.8096 0.3176
-4.250 -0.3655 0.01148 0.00521 -0.0199 0.8085 0.3406
-4.000 -0.3539 0.01125 0.00510 -0.0171 0.8072 0.3660
-3.750 -0.3422 0.01101 0.00499 -0.0143 0.8057 0.3940
-3.500 -0.3285 0.01072 0.00486 -0.0119 0.8039 0.4265
-3.250 -0.3137 0.01044 0.00473 -0.0097 0.8022 0.4606
-3.000 -0.2994 0.01010 0.00457 -0.0074 0.8003 0.5013
-2.750 -0.2837 0.00976 0.00442 -0.0052 0.7986 0.5444
-2.500 -0.2674 0.00940 0.00428 -0.0032 0.7970 0.5921
-2.250 -0.2486 0.00910 0.00422 -0.0014 0.7955 0.6421
-2.000 -0.2246 0.00904 0.00438 -0.0005 0.7941 0.6847
-1.750 -0.1967 0.00913 0.00453 -0.0002 0.7926 0.7119
-1.500 -0.1692 0.00920 0.00461 -0.0001 0.7903 0.7278
-1.250 -0.1421 0.00926 0.00469 0.0000 0.7867 0.7382
-1.000 -0.1142 0.00925 0.00467 0.0001 0.7829 0.7459
-0.750 -0.0855 0.00921 0.00460 0.0001 0.7794 0.7523
-0.500 -0.0573 0.00910 0.00442 0.0001 0.7764 0.7587
-0.250 -0.0279 0.00915 0.00449 -0.0001 0.7728 0.7625
0.000 0.0000 0.00920 0.00457 0.0000 0.7672 0.7672
0.250 0.0279 0.00914 0.00449 0.0001 0.7624 0.7728
0.500 0.0573 0.00910 0.00442 -0.0001 0.7587 0.7764
0.750 0.0855 0.00921 0.00460 -0.0001 0.7524 0.7794
1.000 0.1142 0.00925 0.00467 -0.0001 0.7458 0.7829
1.250 0.1421 0.00926 0.00469 0.0000 0.7382 0.7867
1.500 0.1692 0.00920 0.00461 0.0001 0.7279 0.7903
1.750 0.1967 0.00913 0.00453 0.0002 0.7120 0.7926
2.000 0.2246 0.00904 0.00437 0.0005 0.6843 0.7941
2.250 0.2484 0.00911 0.00422 0.0015 0.6411 0.7955
2.500 0.2673 0.00941 0.00428 0.0032 0.5913 0.7970
2.750 0.2838 0.00976 0.00442 0.0052 0.5446 0.7986
3.000 0.2997 0.01009 0.00457 0.0073 0.5026 0.8003
3.250 0.3142 0.01043 0.00473 0.0096 0.4620 0.8022
3.500 0.3285 0.01072 0.00486 0.0119 0.4266 0.8039
3.750 0.3424 0.01100 0.00499 0.0143 0.3944 0.8057
4.000 0.3542 0.01125 0.00510 0.0171 0.3667 0.8072
4.250 0.3658 0.01148 0.00521 0.0198 0.3410 0.8085
4.500 0.3791 0.01173 0.00537 0.0223 0.3182 0.8097
4.750 0.3938 0.01204 0.00558 0.0243 0.2950 0.8106
5.000 0.4106 0.01235 0.00581 0.0260 0.2747 0.8114
5.250 0.4280 0.01267 0.00605 0.0275 0.2554 0.8124
5.500 0.4463 0.01298 0.00630 0.0289 0.2394 0.8135
5.750 0.4650 0.01329 0.00654 0.0301 0.2241 0.8143
6.000 0.4839 0.01359 0.00678 0.0313 0.2100 0.8151
6.250 0.5033 0.01390 0.00703 0.0324 0.1969 0.8159
6.500 0.5233 0.01418 0.00727 0.0334 0.1854 0.8167
6.750 0.5430 0.01448 0.00753 0.0344 0.1754 0.8176
7.000 0.5623 0.01481 0.00781 0.0354 0.1646 0.8187
7.250 0.5829 0.01509 0.00807 0.0363 0.1565 0.8197
7.750 0.6228 0.01573 0.00865 0.0381 0.1408 0.8212
8.000 0.6420 0.01609 0.00896 0.0390 0.1334 0.8220
8.250 0.6626 0.01639 0.00927 0.0398 0.1273 0.8227
8.500 0.6819 0.01676 0.00960 0.0407 0.1210 0.8234
8.750 0.7017 0.01711 0.00994 0.0415 0.1155 0.8240
9.000 0.7211 0.01748 0.01030 0.0424 0.1098 0.8247
9.250 0.7400 0.01789 0.01069 0.0433 0.1047 0.8253
9.500 0.7598 0.01825 0.01105 0.0441 0.1000 0.8259
9.750 0.7777 0.01869 0.01147 0.0451 0.0947 0.8266
10.000 0.7964 0.01909 0.01189 0.0460 0.0907 0.8275
10.250 0.8149 0.01951 0.01233 0.0469 0.0865 0.8284
10.500 0.8322 0.02001 0.01282 0.0479 0.0823 0.8292
10.750 0.8507 0.02045 0.01328 0.0488 0.0790 0.8299
11.000 0.8680 0.02095 0.01380 0.0498 0.0753 0.8306
11.250 0.8842 0.02153 0.01436 0.0508 0.0716 0.8314
11.500 0.9021 0.02202 0.01489 0.0516 0.0686 0.8322
11.750 0.9187 0.02259 0.01547 0.0526 0.0653 0.8330
12.000 0.9336 0.02325 0.01613 0.0537 0.0624 0.8339
12.250 0.9504 0.02382 0.01674 0.0545 0.0601 0.8347
12.500 0.9662 0.02445 0.01740 0.0554 0.0575 0.8355
12.750 0.9805 0.02519 0.01814 0.0565 0.0550 0.8364
13.000 0.9953 0.02588 0.01888 0.0574 0.0531 0.8373
13.250 1.0101 0.02660 0.01965 0.0583 0.0511 0.8382
13.500 1.0238 0.02741 0.02048 0.0592 0.0491 0.8391
13.750 1.0357 0.02835 0.02143 0.0602 0.0472 0.8400
14.000 1.0498 0.02917 0.02230 0.0610 0.0454 0.8408
14.250 1.0625 0.03009 0.02327 0.0619 0.0439 0.8417
14.500 1.0737 0.03114 0.02435 0.0628 0.0421 0.8425
14.750 1.0838 0.03228 0.02552 0.0637 0.0407 0.8435
15.000 1.0953 0.03332 0.02665 0.0644 0.0393 0.8446
15.250 1.1056 0.03449 0.02788 0.0652 0.0380 0.8459
15.500 1.1144 0.03580 0.02925 0.0659 0.0366 0.8471
15.750 1.1216 0.03731 0.03081 0.0667 0.0355 0.8484
16.000 1.1305 0.03871 0.03229 0.0672 0.0342 0.8497
16.250 1.1381 0.04027 0.03393 0.0677 0.0332 0.8509
16.500 1.1443 0.04200 0.03573 0.0681 0.0321 0.8522
16.750 1.1494 0.04391 0.03769 0.0683 0.0311 0.8535
17.000 1.1521 0.04611 0.03995 0.0685 0.0303 0.8548
17.250 1.1568 0.04821 0.04215 0.0684 0.0295 0.8561
17.500 1.1605 0.05048 0.04451 0.0683 0.0285 0.8574
17.750 1.1626 0.05299 0.04711 0.0679 0.0280 0.8587
18.000 1.1626 0.05583 0.05003 0.0674 0.0270 0.8601
18.250 1.1604 0.05900 0.05330 0.0666 0.0264 0.8616
18.500 1.1568 0.06248 0.05688 0.0655 0.0260 0.8632
18.750 1.1536 0.06601 0.06053 0.0643 0.0254 0.8649
19.000 1.1495 0.06981 0.06446 0.0628 0.0249 0.8667
19.250 1.1434 0.07400 0.06876 0.0611 0.0244 0.8684
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