S1046 17% (Danny Howell) (s1046-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: S1046 17% (Danny Howell) (s1046-il) Reynolds number: 1,000,000 Max Cl/Cd: 80.94 at α=8° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-s1046-il-1000000-n5.txt Download as CSV file: xf-s1046-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: S1046 17% (Danny Howell)
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
------ -------- --------- --------- -------- -------- --------
-19.500 -1.1560 0.10361 0.09956 -0.0115 1.0000 0.0070
-19.250 -1.1650 0.09858 0.09445 -0.0138 1.0000 0.0071
-19.000 -1.1744 0.09360 0.08938 -0.0161 1.0000 0.0072
-18.500 -1.1937 0.08381 0.07941 -0.0203 1.0000 0.0075
-18.250 -1.2028 0.07912 0.07464 -0.0222 1.0000 0.0076
-18.000 -1.2123 0.07449 0.06993 -0.0241 1.0000 0.0080
-17.750 -1.2200 0.07016 0.06553 -0.0257 1.0000 0.0081
-17.500 -1.2269 0.06604 0.06132 -0.0272 1.0000 0.0083
-17.250 -1.2333 0.06209 0.05729 -0.0286 1.0000 0.0086
-17.000 -1.2383 0.05836 0.05348 -0.0298 1.0000 0.0089
-16.750 -1.2421 0.05485 0.04990 -0.0308 1.0000 0.0092
-16.500 -1.2444 0.05163 0.04660 -0.0317 1.0000 0.0094
-16.250 -1.2460 0.04855 0.04345 -0.0325 1.0000 0.0096
-16.000 -1.2497 0.04534 0.04017 -0.0332 1.0000 0.0101
-15.750 -1.2513 0.04248 0.03724 -0.0336 1.0000 0.0105
-15.500 -1.2514 0.03985 0.03455 -0.0339 1.0000 0.0110
-15.250 -1.2501 0.03744 0.03207 -0.0341 1.0000 0.0113
-15.000 -1.2473 0.03522 0.02979 -0.0341 1.0000 0.0118
-14.750 -1.2429 0.03323 0.02774 -0.0341 1.0000 0.0121
-14.500 -1.2404 0.03113 0.02559 -0.0338 1.0000 0.0129
-14.250 -1.2359 0.02927 0.02368 -0.0335 1.0000 0.0135
-14.000 -1.2301 0.02759 0.02196 -0.0330 1.0000 0.0142
-13.750 -1.2229 0.02609 0.02041 -0.0324 1.0000 0.0149
-13.500 -1.2159 0.02464 0.01891 -0.0316 1.0000 0.0157
-13.250 -1.2090 0.02327 0.01751 -0.0307 1.0000 0.0168
-13.000 -1.2006 0.02209 0.01629 -0.0296 1.0000 0.0179
-12.750 -1.1924 0.02097 0.01515 -0.0283 1.0000 0.0193
-12.500 -1.1843 0.01994 0.01409 -0.0268 1.0000 0.0212
-12.250 -1.1768 0.01897 0.01311 -0.0250 1.0000 0.0239
-12.000 -1.1682 0.01814 0.01227 -0.0231 1.0000 0.0270
-11.750 -1.1608 0.01734 0.01148 -0.0207 1.0000 0.0310
-11.500 -1.1511 0.01672 0.01085 -0.0184 1.0000 0.0342
-11.250 -1.1430 0.01611 0.01026 -0.0156 1.0000 0.0392
-11.000 -1.1353 0.01558 0.00974 -0.0125 1.0000 0.0437
-10.750 -1.1223 0.01513 0.00930 -0.0102 1.0000 0.0478
-10.500 -1.1030 0.01458 0.00878 -0.0093 0.9920 0.0539
-10.250 -1.0617 0.01389 0.00812 -0.0130 0.9521 0.0639
-10.000 -1.0360 0.01339 0.00757 -0.0131 0.9001 0.0744
-9.750 -1.0198 0.01304 0.00715 -0.0112 0.8643 0.0832
-9.500 -1.0022 0.01266 0.00674 -0.0096 0.8387 0.0942
-9.250 -0.9819 0.01234 0.00638 -0.0084 0.8186 0.1032
-9.000 -0.9609 0.01202 0.00604 -0.0074 0.8005 0.1131
-8.750 -0.9394 0.01168 0.00570 -0.0064 0.7854 0.1238
-8.500 -0.9175 0.01134 0.00538 -0.0055 0.7716 0.1363
-8.000 -0.8710 0.01075 0.00480 -0.0041 0.7470 0.1597
-7.750 -0.8467 0.01051 0.00456 -0.0036 0.7364 0.1708
-7.250 -0.7967 0.01006 0.00410 -0.0027 0.7160 0.1895
-7.000 -0.7709 0.00989 0.00391 -0.0024 0.7065 0.1985
-6.750 -0.7454 0.00967 0.00371 -0.0020 0.6969 0.2096
-6.500 -0.7195 0.00948 0.00353 -0.0017 0.6884 0.2198
-6.250 -0.6929 0.00934 0.00337 -0.0015 0.6790 0.2283
-6.000 -0.6665 0.00917 0.00320 -0.0012 0.6709 0.2375
-5.750 -0.6394 0.00906 0.00307 -0.0011 0.6618 0.2444
-5.500 -0.6126 0.00891 0.00292 -0.0009 0.6534 0.2533
-5.250 -0.5853 0.00881 0.00279 -0.0008 0.6442 0.2600
-5.000 -0.5582 0.00867 0.00266 -0.0006 0.6359 0.2685
-4.750 -0.5307 0.00859 0.00255 -0.0005 0.6261 0.2760
-4.500 -0.5034 0.00847 0.00243 -0.0004 0.6166 0.2848
-4.250 -0.4757 0.00839 0.00233 -0.0004 0.6071 0.2920
-4.000 -0.4482 0.00829 0.00223 -0.0003 0.5968 0.3006
-3.750 -0.4204 0.00822 0.00214 -0.0002 0.5863 0.3078
-3.500 -0.3928 0.00814 0.00205 -0.0001 0.5759 0.3160
-3.250 -0.3649 0.00808 0.00197 -0.0001 0.5649 0.3239
-3.000 -0.3371 0.00802 0.00190 -0.0001 0.5546 0.3320
-2.750 -0.3092 0.00797 0.00183 0.0000 0.5439 0.3398
-2.500 -0.2812 0.00792 0.00177 0.0000 0.5335 0.3487
-2.250 -0.2532 0.00787 0.00172 0.0000 0.5234 0.3565
-1.750 -0.1971 0.00779 0.00162 0.0000 0.5037 0.3744
-1.500 -0.1690 0.00777 0.00159 0.0000 0.4938 0.3834
-1.250 -0.1410 0.00774 0.00156 0.0001 0.4836 0.3923
-0.500 -0.0564 0.00769 0.00150 0.0000 0.4554 0.4188
-0.250 -0.0282 0.00769 0.00149 0.0000 0.4466 0.4280
0.000 0.0000 0.00768 0.00149 0.0000 0.4374 0.4374
0.250 0.0282 0.00769 0.00149 0.0000 0.4282 0.4466
0.500 0.0564 0.00769 0.00150 0.0000 0.4188 0.4554
1.250 0.1410 0.00774 0.00156 -0.0001 0.3923 0.4837
1.500 0.1690 0.00777 0.00159 0.0000 0.3834 0.4939
1.750 0.1971 0.00779 0.00162 0.0000 0.3742 0.5036
2.250 0.2532 0.00787 0.00172 0.0000 0.3565 0.5237
2.500 0.2812 0.00791 0.00177 0.0000 0.3489 0.5336
2.750 0.3092 0.00797 0.00183 0.0000 0.3400 0.5439
3.000 0.3371 0.00802 0.00190 0.0001 0.3320 0.5545
3.250 0.3649 0.00808 0.00197 0.0001 0.3239 0.5650
3.500 0.3928 0.00815 0.00205 0.0001 0.3159 0.5758
3.750 0.4204 0.00822 0.00214 0.0002 0.3078 0.5864
4.000 0.4483 0.00829 0.00223 0.0003 0.3006 0.5966
4.250 0.4757 0.00839 0.00233 0.0004 0.2918 0.6071
4.500 0.5034 0.00846 0.00243 0.0004 0.2848 0.6168
4.750 0.5307 0.00859 0.00255 0.0005 0.2759 0.6261
5.000 0.5582 0.00868 0.00266 0.0006 0.2684 0.6356
5.250 0.5852 0.00881 0.00279 0.0008 0.2599 0.6444
5.500 0.6126 0.00891 0.00292 0.0009 0.2533 0.6535
5.750 0.6394 0.00906 0.00307 0.0011 0.2445 0.6617
6.000 0.6665 0.00917 0.00320 0.0012 0.2375 0.6706
6.250 0.6929 0.00934 0.00337 0.0015 0.2284 0.6790
6.500 0.7196 0.00948 0.00352 0.0017 0.2201 0.6882
6.750 0.7455 0.00967 0.00371 0.0020 0.2098 0.6967
7.000 0.7709 0.00989 0.00391 0.0024 0.1982 0.7064
7.250 0.7966 0.01007 0.00411 0.0027 0.1892 0.7160
7.750 0.8467 0.01051 0.00456 0.0036 0.1707 0.7363
8.000 0.8709 0.01076 0.00481 0.0041 0.1592 0.7470
8.500 0.9175 0.01134 0.00538 0.0055 0.1363 0.7715
8.750 0.9394 0.01168 0.00570 0.0064 0.1238 0.7858
9.000 0.9609 0.01202 0.00604 0.0074 0.1129 0.8008
9.250 0.9822 0.01232 0.00637 0.0084 0.1039 0.8186
9.500 1.0019 0.01268 0.00675 0.0096 0.0933 0.8390
9.750 1.0203 0.01302 0.00714 0.0111 0.0843 0.8645
10.000 1.0358 0.01340 0.00758 0.0131 0.0737 0.9002
10.250 1.0618 0.01391 0.00814 0.0129 0.0629 0.9527
10.500 1.1032 0.01458 0.00878 0.0093 0.0537 0.9922
10.750 1.1225 0.01513 0.00930 0.0102 0.0477 1.0000
11.000 1.1353 0.01559 0.00974 0.0125 0.0434 1.0000
11.250 1.1430 0.01613 0.01027 0.0156 0.0388 1.0000
11.500 1.1523 0.01668 0.01082 0.0182 0.0348 1.0000
11.750 1.1612 0.01734 0.01147 0.0207 0.0310 1.0000
12.000 1.1684 0.01815 0.01228 0.0230 0.0267 1.0000
12.250 1.1773 0.01896 0.01310 0.0249 0.0239 1.0000
12.500 1.1848 0.01994 0.01409 0.0267 0.0211 1.0000
12.750 1.1936 0.02093 0.01511 0.0282 0.0195 1.0000
13.000 1.2012 0.02208 0.01628 0.0295 0.0178 1.0000
13.250 1.2097 0.02326 0.01750 0.0306 0.0167 1.0000
13.500 1.2172 0.02459 0.01886 0.0315 0.0158 1.0000
13.750 1.2239 0.02606 0.02038 0.0322 0.0148 1.0000
14.000 1.2311 0.02756 0.02193 0.0328 0.0141 1.0000
14.250 1.2368 0.02925 0.02366 0.0333 0.0133 1.0000
14.500 1.2414 0.03112 0.02558 0.0337 0.0127 1.0000
14.750 1.2447 0.03315 0.02766 0.0339 0.0122 1.0000
15.000 1.2489 0.03517 0.02974 0.0340 0.0117 1.0000
15.250 1.2520 0.03736 0.03199 0.0339 0.0113 1.0000
15.500 1.2523 0.03987 0.03456 0.0337 0.0106 1.0000
15.750 1.2526 0.04247 0.03722 0.0334 0.0103 1.0000
16.000 1.2514 0.04530 0.04012 0.0329 0.0100 1.0000
16.250 1.2484 0.04844 0.04333 0.0323 0.0095 1.0000
16.500 1.2469 0.05152 0.04649 0.0315 0.0094 1.0000
16.750 1.2445 0.05475 0.04979 0.0306 0.0090 1.0000
17.000 1.2407 0.05826 0.05338 0.0295 0.0090 1.0000
17.250 1.2358 0.06197 0.05717 0.0283 0.0086 1.0000
17.500 1.2292 0.06596 0.06124 0.0270 0.0082 1.0000
17.750 1.2226 0.07005 0.06541 0.0255 0.0082 1.0000
18.000 1.2136 0.07455 0.06998 0.0238 0.0078 1.0000
18.250 1.2051 0.07904 0.07455 0.0220 0.0076 1.0000
18.500 1.1970 0.08357 0.07917 0.0201 0.0076 1.0000
18.750 1.1872 0.08846 0.08414 0.0181 0.0074 1.0000
19.000 1.1765 0.09354 0.08931 0.0158 0.0073 1.0000
19.250 1.1681 0.09837 0.09423 0.0136 0.0072 1.0000
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