SIKORSKY DBLN-526 AIRFOIL (dbln526-il) Xfoil prediction polar at RE=200,000 Ncrit=9
| Details | Polar file |
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Airfoil: SIKORSKY DBLN-526 AIRFOIL (dbln526-il) Reynolds number: 200,000 Max Cl/Cd: 34.96 at α=8.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-dbln526-il-200000.txt Download as CSV file: xf-dbln526-il-200000.csv |
XFOIL Version 6.96
Calculated polar for: SIKORSKY DBLN-526 AIRFOIL
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.200 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-15.750 -0.7451 0.12805 0.12382 -0.0883 0.9930 0.0617
-15.500 -0.8256 0.11553 0.11109 -0.0881 0.9905 0.0617
-15.250 -0.8324 0.11080 0.10631 -0.0892 0.9893 0.0612
-15.000 -0.8721 0.10369 0.09898 -0.0897 0.9883 0.0608
-14.750 -0.9153 0.09845 0.09359 -0.0848 0.9851 0.0607
-14.500 -0.9693 0.09196 0.08675 -0.0805 0.9831 0.0608
-14.250 -0.9904 0.08879 0.08347 -0.0762 0.9816 0.0602
-14.000 -1.0390 0.08381 0.07814 -0.0683 0.9772 0.0604
-13.750 -1.0647 0.08079 0.07484 -0.0627 0.9756 0.0603
-13.500 -1.0936 0.07779 0.07163 -0.0548 0.9695 0.0603
-13.250 -1.1180 0.07511 0.06869 -0.0474 0.9626 0.0603
-13.000 -1.1310 0.07102 0.06418 -0.0421 0.9536 0.0604
-12.750 -1.1460 0.06838 0.06107 -0.0357 0.9468 0.0613
-12.500 -1.1468 0.06621 0.05855 -0.0316 0.9428 0.0616
-12.250 -1.1289 0.06306 0.05517 -0.0316 0.9411 0.0626
-12.000 -1.1191 0.06149 0.05360 -0.0292 0.9342 0.0635
-11.750 -1.0958 0.06013 0.05217 -0.0295 0.9317 0.0644
-11.500 -1.0713 0.05871 0.05058 -0.0300 0.9301 0.0653
-11.250 -1.0693 0.05739 0.04911 -0.0257 0.9235 0.0661
-11.000 -1.0501 0.05590 0.04738 -0.0248 0.9207 0.0667
-10.750 -1.0302 0.05481 0.04595 -0.0239 0.9188 0.0688
-10.500 -1.0016 0.05361 0.04449 -0.0249 0.9177 0.0692
-10.250 -1.0016 0.05261 0.04333 -0.0198 0.9102 0.0695
-10.000 -0.9689 0.05118 0.04198 -0.0220 0.9083 0.0715
-9.750 -0.9360 0.05029 0.04105 -0.0239 0.9066 0.0729
-9.500 -0.9019 0.04950 0.04016 -0.0259 0.9054 0.0742
-9.250 -0.8980 0.04903 0.03962 -0.0217 0.8988 0.0756
-9.000 -0.8760 0.04848 0.03892 -0.0212 0.8961 0.0770
-8.750 -0.8470 0.04777 0.03810 -0.0220 0.8943 0.0789
-8.500 -0.8142 0.04707 0.03750 -0.0241 0.8930 0.0815
-8.250 -0.7806 0.04652 0.03693 -0.0259 0.8921 0.0827
-8.000 -0.7780 0.04641 0.03679 -0.0215 0.8866 0.0844
-7.750 -0.7620 0.04619 0.03652 -0.0197 0.8833 0.0857
-7.500 -0.7376 0.04575 0.03603 -0.0197 0.8813 0.0885
-7.250 -0.7113 0.04524 0.03561 -0.0202 0.8798 0.0914
-7.000 -0.6837 0.04494 0.03530 -0.0209 0.8786 0.0941
-6.750 -0.6533 0.04463 0.03494 -0.0220 0.8777 0.0968
-6.500 -0.6615 0.04476 0.03505 -0.0153 0.8710 0.0988
-6.250 -0.6475 0.04455 0.03491 -0.0133 0.8684 0.1023
-6.000 -0.6268 0.04434 0.03471 -0.0125 0.8665 0.1077
-5.750 -0.6024 0.04414 0.03451 -0.0125 0.8650 0.1118
-5.500 -0.5734 0.04384 0.03427 -0.0133 0.8637 0.1207
-5.250 -0.5377 0.04320 0.03372 -0.0155 0.8625 0.1352
-5.000 -0.5516 0.04379 0.03436 -0.0079 0.8561 0.1413
-4.750 -0.5344 0.04342 0.03415 -0.0065 0.8526 0.1646
-4.500 -0.5059 0.04298 0.03401 -0.0072 0.8502 0.2168
-4.250 -0.4750 0.04272 0.03378 -0.0085 0.8487 0.2506
-4.000 -0.4417 0.04191 0.03312 -0.0103 0.8474 0.2819
-3.750 -0.4165 0.04055 0.03266 -0.0106 0.8465 0.4423
-3.500 -0.4360 0.04143 0.03383 -0.0020 0.8389 0.4903
-3.250 -0.4208 0.04052 0.03398 0.0005 0.8358 0.6552
-3.000 -0.3858 0.04028 0.03377 -0.0012 0.8333 0.7513
-2.750 -0.3567 0.04034 0.03407 -0.0014 0.8319 0.7873
-2.500 -0.2952 0.04148 0.03544 -0.0084 0.8309 0.8356
-2.250 -0.2271 0.04265 0.03661 -0.0173 0.8301 0.8602
-2.000 -0.2152 0.04481 0.03879 -0.0151 0.8230 0.8744
-1.750 -0.1881 0.04587 0.03982 -0.0155 0.8191 0.8871
-1.500 -0.1546 0.04666 0.04054 -0.0167 0.8167 0.9020
-1.250 -0.1211 0.04713 0.04095 -0.0181 0.8149 0.9149
-1.000 -0.0649 0.04794 0.04167 -0.0245 0.8137 0.9202
-0.750 -0.0269 0.04811 0.04177 -0.0271 0.8126 0.9290
-0.500 -0.0171 0.05003 0.04369 -0.0249 0.8043 0.9333
-0.250 0.0069 0.05051 0.04412 -0.0250 0.8000 0.9409
0.000 0.0524 0.05081 0.04437 -0.0295 0.7979 0.9432
0.250 0.0935 0.05106 0.04456 -0.0328 0.7963 0.9510
0.500 0.1472 0.05129 0.04475 -0.0391 0.7951 0.9529
0.750 0.1946 0.05105 0.04446 -0.0440 0.7940 0.9548
1.000 0.2401 0.05098 0.04434 -0.0483 0.7932 0.9612
1.250 0.2930 0.05066 0.04399 -0.0543 0.7926 0.9626
1.500 0.2831 0.05285 0.04622 -0.0484 0.7780 0.9701
1.750 0.3297 0.05243 0.04578 -0.0531 0.7766 0.9714
2.000 0.3773 0.05201 0.04534 -0.0581 0.7756 0.9736
2.250 0.4193 0.05156 0.04486 -0.0618 0.7748 0.9783
2.500 0.4698 0.05110 0.04440 -0.0674 0.7740 0.9800
2.750 0.4657 0.05307 0.04641 -0.0627 0.7593 0.9858
3.000 0.5182 0.05264 0.04598 -0.0688 0.7581 0.9878
3.250 0.5654 0.05206 0.04540 -0.0737 0.7571 0.9910
3.500 0.6160 0.05144 0.04479 -0.0792 0.7562 0.9931
3.750 0.6545 0.05116 0.04454 -0.0825 0.7516 0.9952
4.000 0.7081 0.05041 0.04380 -0.0888 0.7529 0.9973
4.250 0.7660 0.04847 0.04187 -0.0953 0.7537 0.9979
4.500 0.8221 0.04668 0.04009 -0.1016 0.7542 0.9986
4.750 0.8230 0.04833 0.04181 -0.0978 0.7381 0.9999
5.000 0.8585 0.04676 0.04025 -0.0998 0.7374 1.0000
5.250 0.8933 0.04523 0.03872 -0.1015 0.7367 1.0000
5.500 0.9321 0.04355 0.03703 -0.1040 0.7362 1.0000
5.750 0.9709 0.04217 0.03566 -0.1067 0.7355 1.0000
6.000 1.0149 0.04052 0.03402 -0.1104 0.7349 1.0000
6.250 0.9882 0.04210 0.03561 -0.0999 0.7186 1.0000
6.500 1.0290 0.04074 0.03427 -0.1029 0.7176 1.0000
6.750 1.0773 0.03902 0.03257 -0.1074 0.7167 1.0000
7.000 1.1222 0.03755 0.03110 -0.1112 0.7141 1.0000
7.250 1.0987 0.03927 0.03286 -0.1014 0.6996 1.0000
7.500 1.1548 0.03715 0.03073 -0.1073 0.6975 1.0000
7.750 1.2130 0.03527 0.02886 -0.1139 0.6951 1.0000
8.000 1.1789 0.03739 0.03101 -0.1019 0.6792 1.0000
8.250 1.2371 0.03539 0.02899 -0.1083 0.6752 1.0000
8.500 1.2056 0.03753 0.03119 -0.0968 0.6596 1.0000
8.750 1.2528 0.03617 0.02982 -0.1012 0.6553 1.0000
9.000 1.2275 0.03811 0.03180 -0.0912 0.6397 1.0000
9.250 1.2586 0.03751 0.03122 -0.0924 0.6334 1.0000
9.500 1.2493 0.03889 0.03264 -0.0858 0.6204 1.0000
9.750 1.2663 0.03896 0.03272 -0.0843 0.6103 1.0000
10.000 1.2851 0.03888 0.03262 -0.0829 0.5981 1.0000
10.250 1.2915 0.03953 0.03328 -0.0794 0.5847 1.0000
10.500 1.3148 0.03930 0.03299 -0.0790 0.5725 1.0000
10.750 1.3378 0.03907 0.03263 -0.0785 0.5560 1.0000
11.000 1.3396 0.04007 0.03363 -0.0743 0.5412 1.0000
11.250 1.3485 0.04071 0.03424 -0.0715 0.5269 1.0000
11.500 1.3507 0.04169 0.03514 -0.0674 0.5071 1.0000
11.750 1.3536 0.04269 0.03609 -0.0636 0.4902 1.0000
12.000 1.3476 0.04423 0.03761 -0.0584 0.4712 1.0000
12.250 1.3375 0.04613 0.03953 -0.0526 0.4503 1.0000
12.500 1.3297 0.04799 0.04142 -0.0475 0.4277 1.0000
12.750 1.3112 0.05058 0.04386 -0.0408 0.3874 1.0000
13.000 1.2907 0.05344 0.04644 -0.0342 0.3529 1.0000
13.500 1.2699 0.05812 0.05082 -0.0249 0.3077 1.0000
13.750 1.2653 0.06014 0.05274 -0.0213 0.2913 1.0000
14.000 1.2634 0.06204 0.05463 -0.0181 0.2749 1.0000
14.250 1.2623 0.06391 0.05647 -0.0153 0.2603 1.0000
14.500 1.2609 0.06585 0.05836 -0.0125 0.2477 1.0000
14.750 1.2583 0.06792 0.06039 -0.0096 0.2355 1.0000
15.000 1.2572 0.06987 0.06234 -0.0071 0.2234 1.0000
15.250 1.2537 0.07209 0.06451 -0.0044 0.2121 1.0000
15.500 1.2507 0.07431 0.06672 -0.0019 0.1991 1.0000
15.750 1.2488 0.07653 0.06898 0.0003 0.1856 1.0000
16.000 1.2462 0.07881 0.07125 0.0025 0.1728 1.0000
16.250 1.2397 0.08158 0.07399 0.0049 0.1564 1.0000
16.500 1.2348 0.08419 0.07655 0.0070 0.1428 1.0000
16.750 1.2286 0.08695 0.07925 0.0090 0.1308 1.0000
17.000 1.2252 0.08944 0.08169 0.0107 0.1212 1.0000
17.250 1.2228 0.09187 0.08411 0.0123 0.1138 1.0000
17.500 1.2173 0.09461 0.08679 0.0139 0.1073 1.0000
17.750 1.2179 0.09674 0.08896 0.0152 0.1027 1.0000
18.000 1.2176 0.09898 0.09120 0.0163 0.0980 1.0000
18.250 1.2172 0.10107 0.09322 0.0175 0.0942 1.0000
18.500 1.2216 0.10284 0.09506 0.0182 0.0910 1.0000
18.750 1.2238 0.10481 0.09703 0.0190 0.0871 1.0000
19.000 1.2321 0.10574 0.09785 0.0199 0.0842 1.0000
19.250 1.2370 0.10753 0.09975 0.0204 0.0813 1.0000
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