S1014 (s1014-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: S1014 (s1014-il) Reynolds number: 500,000 Max Cl/Cd: 42.04 at α=9.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-s1014-il-500000-n5.txt Download as CSV file: xf-s1014-il-500000-n5.csv |
XFOIL Version 6.96
Calculated polar for: S1014
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 -1.1180 0.09134 0.08685 -0.0455 0.8714 0.0177
-19.500 -1.1328 0.08512 0.08047 -0.0488 0.8664 0.0180
-19.000 -1.1549 0.07452 0.06956 -0.0540 0.8579 0.0183
-18.750 -1.1619 0.07006 0.06497 -0.0560 0.8540 0.0187
-18.500 -1.1689 0.06579 0.06055 -0.0577 0.8504 0.0189
-18.250 -1.1716 0.06228 0.05690 -0.0588 0.8469 0.0192
-18.000 -1.1742 0.05890 0.05339 -0.0598 0.8440 0.0196
-17.750 -1.1743 0.05592 0.05028 -0.0605 0.8411 0.0199
-17.500 -1.1739 0.05311 0.04737 -0.0610 0.8382 0.0204
-17.250 -1.1747 0.05031 0.04447 -0.0612 0.8355 0.0208
-17.000 -1.1732 0.04787 0.04194 -0.0612 0.8329 0.0213
-16.750 -1.1702 0.04568 0.03965 -0.0611 0.8306 0.0219
-16.250 -1.1597 0.04191 0.03569 -0.0604 0.8270 0.0229
-16.000 -1.1526 0.04027 0.03396 -0.0600 0.8252 0.0235
-15.750 -1.1442 0.03879 0.03238 -0.0594 0.8235 0.0242
-15.500 -1.1384 0.03715 0.03070 -0.0587 0.8218 0.0251
-15.250 -1.1298 0.03577 0.02926 -0.0580 0.8202 0.0259
-15.000 -1.1207 0.03448 0.02790 -0.0572 0.8186 0.0266
-14.750 -1.1099 0.03335 0.02669 -0.0564 0.8171 0.0276
-14.500 -1.0982 0.03231 0.02556 -0.0556 0.8157 0.0286
-14.250 -1.0880 0.03118 0.02438 -0.0546 0.8144 0.0296
-14.000 -1.0762 0.03019 0.02334 -0.0537 0.8132 0.0306
-13.750 -1.0639 0.02926 0.02234 -0.0528 0.8119 0.0318
-13.500 -1.0501 0.02841 0.02144 -0.0519 0.8109 0.0330
-13.250 -1.0355 0.02762 0.02059 -0.0511 0.8099 0.0341
-13.000 -1.0225 0.02675 0.01971 -0.0501 0.8088 0.0359
-12.750 -1.0077 0.02600 0.01893 -0.0492 0.8077 0.0375
-12.500 -0.9921 0.02531 0.01819 -0.0483 0.8067 0.0390
-12.250 -0.9763 0.02464 0.01747 -0.0474 0.8056 0.0406
-12.000 -0.9613 0.02394 0.01675 -0.0465 0.8046 0.0424
-11.750 -0.9448 0.02332 0.01611 -0.0456 0.8035 0.0443
-11.500 -0.9277 0.02275 0.01549 -0.0447 0.8024 0.0463
-11.250 -0.9111 0.02215 0.01487 -0.0438 0.8012 0.0485
-11.000 -0.8944 0.02158 0.01429 -0.0428 0.8002 0.0509
-10.750 -0.8765 0.02108 0.01375 -0.0419 0.7992 0.0532
-10.500 -0.8583 0.02059 0.01322 -0.0411 0.7984 0.0555
-10.250 -0.8411 0.02006 0.01269 -0.0401 0.7976 0.0586
-10.000 -0.8227 0.01961 0.01221 -0.0392 0.7967 0.0617
-9.750 -0.8038 0.01918 0.01176 -0.0384 0.7959 0.0648
-9.500 -0.7858 0.01871 0.01129 -0.0374 0.7952 0.0683
-9.250 -0.7667 0.01828 0.01087 -0.0366 0.7945 0.0721
-9.000 -0.7473 0.01788 0.01045 -0.0358 0.7938 0.0755
-8.750 -0.7287 0.01744 0.01004 -0.0348 0.7931 0.0804
-8.500 -0.7089 0.01707 0.00967 -0.0340 0.7924 0.0846
-8.250 -0.6898 0.01667 0.00928 -0.0331 0.7917 0.0893
-8.000 -0.6702 0.01630 0.00892 -0.0322 0.7909 0.0946
-7.750 -0.6504 0.01595 0.00858 -0.0314 0.7901 0.1002
-7.500 -0.6312 0.01558 0.00824 -0.0304 0.7894 0.1065
-7.250 -0.6111 0.01526 0.00792 -0.0295 0.7886 0.1129
-7.000 -0.5921 0.01489 0.00760 -0.0285 0.7878 0.1208
-6.750 -0.5721 0.01458 0.00729 -0.0275 0.7870 0.1280
-6.500 -0.5530 0.01423 0.00698 -0.0265 0.7860 0.1370
-6.250 -0.5341 0.01389 0.00669 -0.0253 0.7851 0.1471
-6.000 -0.5149 0.01358 0.00640 -0.0242 0.7844 0.1578
-5.750 -0.4966 0.01324 0.00612 -0.0229 0.7836 0.1708
-5.500 -0.4791 0.01290 0.00584 -0.0215 0.7829 0.1855
-5.250 -0.4623 0.01258 0.00558 -0.0198 0.7822 0.2019
-5.000 -0.4474 0.01228 0.00536 -0.0178 0.7815 0.2214
-4.750 -0.4344 0.01198 0.00517 -0.0154 0.7807 0.2442
-4.500 -0.4195 0.01171 0.00499 -0.0132 0.7800 0.2699
-4.250 -0.4041 0.01138 0.00480 -0.0113 0.7793 0.3022
-4.000 -0.3892 0.01101 0.00460 -0.0092 0.7785 0.3417
-3.750 -0.3740 0.01059 0.00439 -0.0072 0.7776 0.3869
-3.500 -0.3597 0.01011 0.00417 -0.0051 0.7767 0.4406
-3.250 -0.3466 0.00956 0.00392 -0.0027 0.7758 0.5074
-3.000 -0.3333 0.00898 0.00371 -0.0003 0.7748 0.5856
-2.750 -0.3139 0.00883 0.00398 0.0015 0.7740 0.6649
-2.500 -0.2862 0.00897 0.00417 0.0015 0.7731 0.6925
-2.250 -0.2580 0.00906 0.00425 0.0014 0.7721 0.7051
-2.000 -0.2299 0.00912 0.00427 0.0012 0.7712 0.7146
-1.750 -0.2012 0.00923 0.00439 0.0010 0.7704 0.7211
-1.500 -0.1730 0.00929 0.00440 0.0008 0.7694 0.7277
-1.250 -0.1441 0.00940 0.00452 0.0006 0.7684 0.7326
-1.000 -0.1152 0.00954 0.00467 0.0004 0.7675 0.7383
-0.750 -0.0873 0.00966 0.00475 0.0004 0.7665 0.7457
-0.500 -0.0573 0.00995 0.00511 0.0002 0.7654 0.7526
-0.250 -0.0286 0.01012 0.00527 0.0002 0.7642 0.7593
0.000 0.0000 0.01016 0.00527 0.0000 0.7627 0.7627
0.250 0.0286 0.01012 0.00527 -0.0002 0.7593 0.7642
0.500 0.0573 0.00995 0.00511 -0.0002 0.7526 0.7654
0.750 0.0873 0.00966 0.00475 -0.0004 0.7457 0.7665
1.000 0.1152 0.00954 0.00467 -0.0004 0.7383 0.7675
1.250 0.1441 0.00940 0.00452 -0.0006 0.7327 0.7684
1.500 0.1730 0.00929 0.00440 -0.0008 0.7277 0.7694
1.750 0.2011 0.00923 0.00439 -0.0010 0.7212 0.7704
2.000 0.2299 0.00912 0.00427 -0.0012 0.7146 0.7712
2.250 0.2580 0.00906 0.00425 -0.0014 0.7051 0.7721
2.500 0.2862 0.00896 0.00416 -0.0015 0.6922 0.7731
2.750 0.3139 0.00883 0.00398 -0.0015 0.6651 0.7740
3.000 0.3335 0.00897 0.00371 0.0002 0.5865 0.7748
3.250 0.3466 0.00956 0.00392 0.0027 0.5073 0.7758
3.500 0.3602 0.01010 0.00416 0.0050 0.4425 0.7767
3.750 0.3741 0.01059 0.00439 0.0072 0.3874 0.7776
4.000 0.3895 0.01100 0.00460 0.0092 0.3427 0.7785
4.250 0.4040 0.01138 0.00480 0.0113 0.3018 0.7793
4.500 0.4194 0.01171 0.00499 0.0133 0.2696 0.7800
4.750 0.4343 0.01199 0.00517 0.0154 0.2439 0.7807
5.250 0.4624 0.01258 0.00558 0.0198 0.2019 0.7822
5.500 0.4790 0.01291 0.00584 0.0215 0.1849 0.7829
5.750 0.4966 0.01324 0.00612 0.0229 0.1706 0.7836
6.000 0.5149 0.01358 0.00640 0.0242 0.1576 0.7844
6.250 0.5341 0.01389 0.00668 0.0253 0.1469 0.7851
6.500 0.5531 0.01423 0.00698 0.0264 0.1369 0.7860
6.750 0.5722 0.01457 0.00729 0.0275 0.1279 0.7870
7.000 0.5921 0.01489 0.00759 0.0285 0.1203 0.7878
7.250 0.6112 0.01526 0.00792 0.0295 0.1129 0.7886
7.500 0.6314 0.01557 0.00824 0.0304 0.1066 0.7894
7.750 0.6504 0.01595 0.00858 0.0313 0.1000 0.7901
8.000 0.6704 0.01629 0.00892 0.0322 0.0947 0.7909
8.250 0.6900 0.01667 0.00927 0.0331 0.0893 0.7916
8.500 0.7091 0.01706 0.00966 0.0340 0.0846 0.7924
8.750 0.7289 0.01744 0.01004 0.0348 0.0802 0.7931
9.000 0.7477 0.01787 0.01044 0.0357 0.0758 0.7938
9.250 0.7669 0.01828 0.01086 0.0366 0.0722 0.7945
9.500 0.7861 0.01870 0.01129 0.0374 0.0684 0.7952
9.750 0.8040 0.01918 0.01175 0.0384 0.0646 0.7959
10.000 0.8231 0.01959 0.01220 0.0392 0.0618 0.7967
10.250 0.8414 0.02005 0.01268 0.0401 0.0585 0.7976
10.500 0.8587 0.02058 0.01321 0.0410 0.0555 0.7984
10.750 0.8768 0.02107 0.01374 0.0419 0.0533 0.7993
11.000 0.8948 0.02157 0.01427 0.0428 0.0508 0.8002
11.250 0.9116 0.02214 0.01485 0.0437 0.0485 0.8012
11.500 0.9281 0.02274 0.01548 0.0447 0.0462 0.8024
11.750 0.9453 0.02330 0.01609 0.0455 0.0442 0.8035
12.000 0.9617 0.02392 0.01674 0.0464 0.0424 0.8046
12.250 0.9769 0.02462 0.01745 0.0474 0.0406 0.8056
12.500 0.9925 0.02530 0.01818 0.0483 0.0391 0.8067
12.750 1.0083 0.02598 0.01891 0.0491 0.0375 0.8077
13.000 1.0231 0.02673 0.01969 0.0500 0.0359 0.8088
13.250 1.0365 0.02758 0.02056 0.0510 0.0344 0.8099
13.500 1.0503 0.02842 0.02145 0.0519 0.0332 0.8109
13.750 1.0645 0.02924 0.02233 0.0527 0.0320 0.8120
14.000 1.0770 0.03015 0.02330 0.0536 0.0305 0.8132
14.250 1.0887 0.03116 0.02435 0.0545 0.0295 0.8145
14.500 1.0989 0.03227 0.02552 0.0555 0.0285 0.8158
14.750 1.1108 0.03330 0.02664 0.0563 0.0275 0.8172
15.000 1.1215 0.03444 0.02786 0.0571 0.0267 0.8187
15.250 1.1311 0.03570 0.02918 0.0579 0.0256 0.8203
15.500 1.1397 0.03707 0.03060 0.0586 0.0248 0.8219
15.750 1.1457 0.03870 0.03229 0.0593 0.0241 0.8236
16.000 1.1538 0.04020 0.03389 0.0599 0.0236 0.8253
16.250 1.1610 0.04183 0.03561 0.0603 0.0229 0.8270
16.750 1.1716 0.04558 0.03955 0.0610 0.0219 0.8308
17.000 1.1748 0.04775 0.04182 0.0612 0.0214 0.8331
17.250 1.1762 0.05018 0.04434 0.0611 0.0207 0.8357
17.500 1.1761 0.05291 0.04716 0.0609 0.0204 0.8385
17.750 1.1758 0.05578 0.05014 0.0604 0.0199 0.8414
18.000 1.1754 0.05881 0.05329 0.0597 0.0196 0.8442
18.250 1.1734 0.06210 0.05672 0.0588 0.0192 0.8473
18.500 1.1700 0.06570 0.06046 0.0576 0.0189 0.8508
18.750 1.1638 0.06985 0.06476 0.0560 0.0186 0.8545
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