S1014 (s1014-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: S1014 (s1014-il) Reynolds number: 1,000,000 Max Cl/Cd: 52.62 at α=9° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-s1014-il-1000000-n5.txt Download as CSV file: xf-s1014-il-1000000-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 = 1.000 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -1.2897 0.06555 0.06070 -0.0564 0.8205 0.0129
-19.500 -1.2943 0.06182 0.05686 -0.0577 0.8181 0.0131
-19.250 -1.2968 0.05848 0.05341 -0.0587 0.8157 0.0133
-18.750 -1.2969 0.05273 0.04745 -0.0598 0.8112 0.0136
-18.500 -1.2961 0.05010 0.04473 -0.0601 0.8095 0.0139
-18.250 -1.2949 0.04760 0.04216 -0.0602 0.8077 0.0141
-18.000 -1.2930 0.04529 0.03977 -0.0601 0.8061 0.0145
-17.750 -1.2888 0.04327 0.03768 -0.0599 0.8044 0.0149
-17.500 -1.2835 0.04142 0.03576 -0.0595 0.8027 0.0151
-17.250 -1.2772 0.03973 0.03400 -0.0591 0.8011 0.0156
-17.000 -1.2702 0.03816 0.03235 -0.0585 0.7996 0.0158
-16.750 -1.2621 0.03670 0.03083 -0.0579 0.7981 0.0162
-16.500 -1.2533 0.03536 0.02942 -0.0572 0.7966 0.0166
-16.250 -1.2438 0.03410 0.02809 -0.0565 0.7953 0.0171
-16.000 -1.2353 0.03278 0.02674 -0.0556 0.7944 0.0179
-15.750 -1.2249 0.03163 0.02554 -0.0548 0.7935 0.0183
-15.500 -1.2139 0.03055 0.02442 -0.0539 0.7924 0.0188
-15.250 -1.2020 0.02956 0.02338 -0.0531 0.7914 0.0196
-15.000 -1.1890 0.02867 0.02244 -0.0523 0.7904 0.0201
-14.750 -1.1769 0.02773 0.02145 -0.0513 0.7893 0.0207
-14.500 -1.1644 0.02683 0.02052 -0.0503 0.7883 0.0217
-14.250 -1.1507 0.02602 0.01968 -0.0494 0.7873 0.0226
-14.000 -1.1366 0.02526 0.01888 -0.0484 0.7863 0.0234
-13.750 -1.1219 0.02455 0.01813 -0.0475 0.7853 0.0243
-13.500 -1.1072 0.02383 0.01738 -0.0465 0.7844 0.0254
-13.250 -1.0921 0.02315 0.01668 -0.0456 0.7834 0.0266
-13.000 -1.0766 0.02251 0.01601 -0.0446 0.7825 0.0278
-12.750 -1.0599 0.02194 0.01540 -0.0437 0.7816 0.0288
-12.500 -1.0439 0.02133 0.01477 -0.0427 0.7807 0.0301
-12.250 -1.0275 0.02075 0.01418 -0.0417 0.7797 0.0317
-12.000 -1.0104 0.02022 0.01362 -0.0408 0.7786 0.0333
-11.750 -0.9924 0.01973 0.01310 -0.0400 0.7780 0.0342
-11.500 -0.9754 0.01918 0.01256 -0.0390 0.7774 0.0366
-11.250 -0.9575 0.01869 0.01207 -0.0381 0.7767 0.0383
-11.000 -0.9389 0.01825 0.01160 -0.0372 0.7761 0.0398
-10.750 -0.9205 0.01779 0.01113 -0.0363 0.7755 0.0416
-10.500 -0.9022 0.01733 0.01068 -0.0354 0.7748 0.0438
-10.250 -0.8832 0.01692 0.01027 -0.0345 0.7741 0.0460
-10.000 -0.8641 0.01652 0.00985 -0.0337 0.7734 0.0481
-9.750 -0.8453 0.01609 0.00944 -0.0327 0.7728 0.0510
-9.500 -0.8258 0.01572 0.00907 -0.0319 0.7721 0.0534
-9.250 -0.8060 0.01537 0.00870 -0.0310 0.7714 0.0557
-9.000 -0.7870 0.01497 0.00832 -0.0300 0.7708 0.0595
-8.750 -0.7672 0.01462 0.00798 -0.0291 0.7701 0.0629
-8.500 -0.7471 0.01429 0.00765 -0.0283 0.7695 0.0657
-8.250 -0.7278 0.01393 0.00731 -0.0273 0.7688 0.0702
-8.000 -0.7074 0.01363 0.00701 -0.0264 0.7682 0.0736
-7.750 -0.6877 0.01330 0.00670 -0.0254 0.7676 0.0781
-7.500 -0.6678 0.01298 0.00640 -0.0244 0.7669 0.0829
-7.250 -0.6474 0.01270 0.00612 -0.0235 0.7663 0.0871
-7.000 -0.6280 0.01238 0.00583 -0.0224 0.7657 0.0932
-6.750 -0.6075 0.01213 0.00558 -0.0215 0.7651 0.0977
-6.500 -0.5884 0.01182 0.00531 -0.0203 0.7644 0.1050
-6.250 -0.5683 0.01157 0.00506 -0.0192 0.7635 0.1111
-6.000 -0.5495 0.01130 0.00482 -0.0178 0.7626 0.1188
-5.750 -0.5298 0.01107 0.00461 -0.0166 0.7619 0.1255
-5.500 -0.5119 0.01082 0.00441 -0.0150 0.7615 0.1343
-5.250 -0.4938 0.01062 0.00425 -0.0134 0.7610 0.1434
-5.000 -0.4759 0.01043 0.00410 -0.0117 0.7606 0.1541
-4.750 -0.4555 0.01022 0.00395 -0.0106 0.7601 0.1658
-4.500 -0.4348 0.00998 0.00380 -0.0095 0.7596 0.1823
-4.250 -0.4132 0.00977 0.00365 -0.0085 0.7590 0.1986
-4.000 -0.3918 0.00952 0.00350 -0.0076 0.7585 0.2201
-3.750 -0.3703 0.00927 0.00336 -0.0066 0.7579 0.2434
-3.500 -0.3489 0.00900 0.00321 -0.0057 0.7573 0.2724
-3.250 -0.3276 0.00870 0.00306 -0.0047 0.7566 0.3062
-3.000 -0.3061 0.00839 0.00290 -0.0038 0.7558 0.3427
-2.750 -0.2852 0.00803 0.00273 -0.0027 0.7550 0.3891
-2.500 -0.2648 0.00762 0.00255 -0.0016 0.7544 0.4428
-2.250 -0.2447 0.00717 0.00235 -0.0005 0.7537 0.5056
-2.000 -0.2246 0.00668 0.00214 0.0007 0.7530 0.5739
-1.750 -0.2041 0.00624 0.00205 0.0019 0.7523 0.6535
-1.500 -0.1766 0.00622 0.00214 0.0020 0.7515 0.6902
-1.250 -0.1473 0.00624 0.00217 0.0016 0.7508 0.7017
-1.000 -0.1177 0.00627 0.00220 0.0012 0.7501 0.7098
-0.750 -0.0881 0.00629 0.00221 0.0008 0.7490 0.7155
-0.500 -0.0586 0.00631 0.00222 0.0005 0.7467 0.7214
-0.250 -0.0293 0.00628 0.00218 0.0002 0.7420 0.7274
0.000 0.0000 0.00622 0.00213 0.0000 0.7340 0.7340
0.250 0.0292 0.00628 0.00218 -0.0002 0.7274 0.7420
0.500 0.0586 0.00631 0.00222 -0.0005 0.7214 0.7467
0.750 0.0881 0.00629 0.00221 -0.0008 0.7155 0.7490
1.000 0.1177 0.00627 0.00220 -0.0012 0.7098 0.7501
1.250 0.1473 0.00624 0.00217 -0.0016 0.7017 0.7508
1.500 0.1766 0.00622 0.00214 -0.0020 0.6900 0.7515
1.750 0.2040 0.00624 0.00205 -0.0019 0.6525 0.7523
2.000 0.2247 0.00668 0.00214 -0.0007 0.5746 0.7530
2.250 0.2449 0.00716 0.00235 0.0004 0.5073 0.7537
2.500 0.2651 0.00761 0.00255 0.0016 0.4446 0.7544
2.750 0.2853 0.00803 0.00273 0.0027 0.3895 0.7550
3.000 0.3061 0.00838 0.00290 0.0038 0.3430 0.7558
3.250 0.3275 0.00870 0.00306 0.0047 0.3056 0.7566
3.500 0.3486 0.00901 0.00321 0.0057 0.2713 0.7573
3.750 0.3703 0.00927 0.00336 0.0066 0.2434 0.7579
4.000 0.3917 0.00953 0.00350 0.0076 0.2196 0.7585
4.250 0.4133 0.00976 0.00365 0.0085 0.1991 0.7590
4.500 0.4347 0.00999 0.00380 0.0095 0.1818 0.7596
4.750 0.4555 0.01022 0.00395 0.0106 0.1660 0.7601
5.000 0.4759 0.01043 0.00410 0.0117 0.1542 0.7606
5.250 0.4939 0.01062 0.00425 0.0134 0.1436 0.7610
5.500 0.5121 0.01081 0.00440 0.0150 0.1349 0.7615
5.750 0.5298 0.01107 0.00461 0.0166 0.1254 0.7619
6.000 0.5495 0.01130 0.00482 0.0178 0.1186 0.7626
6.250 0.5684 0.01157 0.00506 0.0191 0.1112 0.7636
6.500 0.5883 0.01182 0.00531 0.0203 0.1047 0.7644
6.750 0.6076 0.01212 0.00557 0.0214 0.0983 0.7651
7.000 0.6282 0.01238 0.00583 0.0224 0.0935 0.7657
7.250 0.6475 0.01270 0.00612 0.0235 0.0873 0.7663
7.500 0.6680 0.01298 0.00639 0.0244 0.0830 0.7669
7.750 0.6879 0.01329 0.00669 0.0254 0.0782 0.7676
8.000 0.7076 0.01362 0.00700 0.0264 0.0738 0.7682
8.250 0.7280 0.01392 0.00731 0.0272 0.0704 0.7688
8.500 0.7474 0.01428 0.00764 0.0282 0.0660 0.7695
8.750 0.7673 0.01462 0.00798 0.0291 0.0628 0.7701
9.000 0.7872 0.01496 0.00832 0.0300 0.0595 0.7708
9.250 0.8061 0.01536 0.00870 0.0310 0.0556 0.7714
9.500 0.8261 0.01572 0.00906 0.0318 0.0534 0.7721
9.750 0.8455 0.01609 0.00944 0.0327 0.0507 0.7728
10.000 0.8642 0.01652 0.00985 0.0336 0.0479 0.7735
10.250 0.8835 0.01691 0.01026 0.0345 0.0459 0.7741
10.500 0.9025 0.01733 0.01068 0.0354 0.0437 0.7748
10.750 0.9208 0.01778 0.01113 0.0363 0.0416 0.7755
11.000 0.9392 0.01824 0.01159 0.0372 0.0397 0.7761
11.250 0.9579 0.01868 0.01206 0.0380 0.0383 0.7767
11.500 0.9758 0.01917 0.01255 0.0389 0.0366 0.7774
11.750 0.9931 0.01970 0.01308 0.0399 0.0346 0.7780
12.000 1.0108 0.02021 0.01361 0.0408 0.0332 0.7786
12.250 1.0279 0.02074 0.01416 0.0417 0.0315 0.7797
12.500 1.0444 0.02131 0.01475 0.0427 0.0302 0.7807
12.750 1.0604 0.02192 0.01538 0.0436 0.0287 0.7816
13.000 1.0772 0.02249 0.01599 0.0445 0.0277 0.7825
13.250 1.0928 0.02312 0.01665 0.0455 0.0267 0.7835
13.500 1.1076 0.02382 0.01737 0.0465 0.0252 0.7844
13.750 1.1224 0.02453 0.01811 0.0474 0.0241 0.7854
14.000 1.1373 0.02523 0.01885 0.0484 0.0233 0.7863
14.250 1.1514 0.02599 0.01965 0.0493 0.0225 0.7873
14.500 1.1651 0.02680 0.02049 0.0502 0.0217 0.7883
14.750 1.1779 0.02768 0.02140 0.0512 0.0209 0.7894
15.000 1.1899 0.02863 0.02239 0.0522 0.0201 0.7904
15.250 1.2028 0.02953 0.02334 0.0530 0.0196 0.7915
15.500 1.2150 0.03050 0.02437 0.0538 0.0190 0.7925
15.750 1.2260 0.03158 0.02549 0.0547 0.0184 0.7935
16.000 1.2364 0.03272 0.02667 0.0555 0.0178 0.7944
16.250 1.2449 0.03404 0.02802 0.0564 0.0171 0.7953
16.500 1.2540 0.03533 0.02938 0.0571 0.0166 0.7967
16.750 1.2630 0.03665 0.03078 0.0578 0.0164 0.7982
17.000 1.2715 0.03806 0.03226 0.0584 0.0160 0.7997
17.250 1.2786 0.03963 0.03390 0.0590 0.0154 0.8012
17.500 1.2850 0.04130 0.03564 0.0594 0.0151 0.8028
17.750 1.2902 0.04317 0.03757 0.0598 0.0148 0.8045
18.000 1.2942 0.04520 0.03967 0.0600 0.0144 0.8062
18.250 1.2965 0.04747 0.04202 0.0601 0.0141 0.8079
18.500 1.2976 0.04998 0.04460 0.0601 0.0138 0.8096
18.750 1.2990 0.05254 0.04726 0.0598 0.0136 0.8114
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