Marsden (marsden-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: Marsden (marsden-il) Reynolds number: 1,000,000 Max Cl/Cd: 97.96 at α=5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-marsden-il-1000000-n5.txt Download as CSV file: xf-marsden-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: Marsden
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
------ -------- --------- --------- -------- -------- --------
-18.250 -0.1865 0.08708 0.08118 -0.1550 0.4301 0.0352
-18.000 -0.2289 0.07774 0.07168 -0.1612 0.4301 0.0353
-17.750 -0.2499 0.07163 0.06547 -0.1653 0.4300 0.0355
-17.500 -0.2621 0.06681 0.06057 -0.1686 0.4299 0.0356
-17.250 -0.2697 0.06263 0.05632 -0.1714 0.4297 0.0357
-17.000 -0.2747 0.05885 0.05248 -0.1740 0.4295 0.0359
-16.750 -0.2770 0.05542 0.04899 -0.1764 0.4293 0.0360
-16.500 -0.2774 0.05229 0.04580 -0.1785 0.4291 0.0360
-16.250 -0.2760 0.04944 0.04290 -0.1803 0.4288 0.0361
-16.000 -0.2729 0.04683 0.04024 -0.1820 0.4285 0.0362
-15.750 -0.2686 0.04444 0.03779 -0.1835 0.4281 0.0363
-15.500 -0.2630 0.04225 0.03555 -0.1847 0.4277 0.0363
-15.250 -0.2565 0.04023 0.03349 -0.1858 0.4274 0.0364
-15.000 -0.2491 0.03839 0.03160 -0.1867 0.4270 0.0365
-14.750 -0.2400 0.03678 0.02995 -0.1873 0.4267 0.0366
-14.500 -0.2308 0.03525 0.02838 -0.1878 0.4264 0.0366
-14.250 -0.2208 0.03385 0.02695 -0.1882 0.4260 0.0367
-14.000 -0.2096 0.03262 0.02568 -0.1883 0.4257 0.0368
-13.750 -0.1988 0.03143 0.02446 -0.1884 0.4254 0.0369
-13.500 -0.1867 0.03039 0.02339 -0.1883 0.4250 0.0370
-13.250 -0.1749 0.02938 0.02235 -0.1881 0.4247 0.0370
-13.000 -0.1622 0.02850 0.02145 -0.1878 0.4243 0.0371
-12.750 -0.1498 0.02766 0.02058 -0.1873 0.4240 0.0372
-12.500 -0.1373 0.02688 0.01978 -0.1867 0.4236 0.0373
-12.250 -0.1240 0.02620 0.01907 -0.1860 0.4233 0.0374
-12.000 -0.1121 0.02547 0.01833 -0.1851 0.4232 0.0375
-11.750 -0.0994 0.02484 0.01768 -0.1841 0.4231 0.0376
-11.500 -0.0869 0.02424 0.01707 -0.1830 0.4230 0.0377
-11.250 -0.0755 0.02363 0.01645 -0.1816 0.4230 0.0378
-11.000 -0.0637 0.02310 0.01590 -0.1802 0.4229 0.0379
-10.750 -0.0526 0.02259 0.01538 -0.1785 0.4228 0.0380
-10.500 -0.0430 0.02209 0.01488 -0.1766 0.4227 0.0381
-10.250 -0.0348 0.02163 0.01441 -0.1743 0.4226 0.0382
-10.000 -0.0284 0.02120 0.01398 -0.1716 0.4225 0.0383
-9.750 -0.0275 0.02079 0.01356 -0.1679 0.4224 0.0384
-9.500 -0.0393 0.02040 0.01318 -0.1619 0.4223 0.0385
-9.250 -0.0351 0.01995 0.01273 -0.1587 0.4222 0.0386
-9.000 -0.0242 0.01951 0.01228 -0.1567 0.4221 0.0387
-8.750 -0.0087 0.01910 0.01186 -0.1554 0.4220 0.0388
-8.500 0.0100 0.01869 0.01145 -0.1547 0.4218 0.0389
-8.250 0.0315 0.01831 0.01105 -0.1543 0.4217 0.0391
-8.000 0.0554 0.01796 0.01069 -0.1544 0.4215 0.0392
-7.750 0.0811 0.01762 0.01034 -0.1547 0.4213 0.0393
-7.500 0.1085 0.01731 0.01002 -0.1553 0.4211 0.0395
-7.250 0.1373 0.01703 0.00973 -0.1560 0.4209 0.0396
-7.000 0.1673 0.01676 0.00945 -0.1570 0.4207 0.0397
-6.750 0.1986 0.01646 0.00914 -0.1582 0.4205 0.0400
-6.500 0.2313 0.01615 0.00883 -0.1597 0.4203 0.0403
-6.250 0.2645 0.01591 0.00858 -0.1613 0.4201 0.0407
-6.000 0.2976 0.01571 0.00839 -0.1626 0.4199 0.0411
-5.750 0.3307 0.01556 0.00824 -0.1640 0.4196 0.0415
-5.500 0.3637 0.01542 0.00811 -0.1652 0.4194 0.0419
-5.250 0.3969 0.01531 0.00799 -0.1665 0.4192 0.0423
-5.000 0.4302 0.01520 0.00788 -0.1678 0.4189 0.0426
-4.750 0.4635 0.01509 0.00778 -0.1690 0.4186 0.0429
-4.500 0.4969 0.01500 0.00769 -0.1703 0.4183 0.0433
-4.250 0.5304 0.01493 0.00761 -0.1716 0.4179 0.0437
-4.000 0.5642 0.01487 0.00756 -0.1730 0.4177 0.0441
-3.750 0.5981 0.01483 0.00752 -0.1743 0.4174 0.0444
-3.500 0.6322 0.01480 0.00749 -0.1757 0.4172 0.0448
-3.250 0.6671 0.01475 0.00746 -0.1773 0.4169 0.0456
-3.000 0.7016 0.01473 0.00745 -0.1788 0.4166 0.0465
-2.750 0.7358 0.01473 0.00746 -0.1803 0.4164 0.0474
-2.500 0.7697 0.01474 0.00748 -0.1816 0.4161 0.0484
-2.250 0.8033 0.01475 0.00750 -0.1830 0.4158 0.0494
-2.000 0.8372 0.01475 0.00751 -0.1844 0.4154 0.0507
-1.750 0.8712 0.01475 0.00753 -0.1858 0.4151 0.0526
-1.500 0.9044 0.01475 0.00755 -0.1871 0.4146 0.0548
-1.250 0.9381 0.01476 0.00758 -0.1884 0.4142 0.0578
-1.000 0.9714 0.01478 0.00762 -0.1897 0.4139 0.0617
-0.750 1.0057 0.01481 0.00768 -0.1913 0.4136 0.0680
-0.500 1.0414 0.01483 0.00775 -0.1932 0.4133 0.0798
-0.250 1.0796 0.01482 0.00784 -0.1956 0.4130 0.1056
0.000 1.1196 0.01481 0.00794 -0.1985 0.4128 0.1423
0.250 1.1619 0.01478 0.00805 -0.2019 0.4125 0.1906
0.500 1.2037 0.01477 0.00818 -0.2052 0.4122 0.2417
0.750 1.2461 0.01477 0.00832 -0.2086 0.4120 0.2946
1.000 1.3013 0.01467 0.00847 -0.2148 0.4116 0.3994
1.250 1.3631 0.01459 0.00876 -0.2223 0.4113 0.5552
1.500 1.3938 0.01474 0.00898 -0.2231 0.4109 0.5897
1.750 1.4212 0.01491 0.00917 -0.2233 0.4105 0.6039
2.000 1.4481 0.01509 0.00934 -0.2234 0.4101 0.6105
2.250 1.4747 0.01529 0.00955 -0.2235 0.4098 0.6157
2.500 1.5008 0.01551 0.00978 -0.2235 0.4094 0.6208
2.750 1.5269 0.01575 0.01002 -0.2235 0.4090 0.6254
3.000 1.5531 0.01603 0.01029 -0.2235 0.4085 0.6302
3.250 1.5794 0.01634 0.01060 -0.2237 0.4079 0.6339
3.500 1.6053 0.01662 0.01090 -0.2238 0.4076 0.6374
3.750 1.6302 0.01680 0.01111 -0.2236 0.4074 0.6390
4.000 1.6548 0.01700 0.01133 -0.2235 0.4073 0.6405
4.250 1.6791 0.01720 0.01154 -0.2233 0.4071 0.6421
4.500 1.7031 0.01741 0.01178 -0.2230 0.4070 0.6438
4.750 1.7265 0.01763 0.01202 -0.2227 0.4068 0.6455
5.000 1.7495 0.01786 0.01228 -0.2223 0.4065 0.6471
5.250 1.7722 0.01810 0.01255 -0.2219 0.4063 0.6485
5.500 1.7947 0.01835 0.01282 -0.2216 0.4061 0.6499
5.750 1.8171 0.01861 0.01310 -0.2212 0.4058 0.6512
6.000 1.8391 0.01888 0.01340 -0.2207 0.4055 0.6525
6.250 1.8602 0.01917 0.01372 -0.2202 0.4051 0.6537
6.500 1.8810 0.01947 0.01405 -0.2196 0.4048 0.6549
6.750 1.9017 0.01979 0.01439 -0.2191 0.4044 0.6560
7.000 1.9219 0.02012 0.01475 -0.2184 0.4040 0.6569
7.250 1.9417 0.02046 0.01513 -0.2178 0.4036 0.6583
7.500 1.9612 0.02082 0.01552 -0.2172 0.4032 0.6599
7.750 1.9804 0.02119 0.01593 -0.2165 0.4027 0.6614
8.000 1.9988 0.02158 0.01636 -0.2158 0.4022 0.6629
8.250 2.0172 0.02197 0.01679 -0.2150 0.4017 0.6642
8.500 2.0350 0.02239 0.01725 -0.2143 0.4012 0.6655
8.750 2.0524 0.02281 0.01771 -0.2135 0.4006 0.6668
9.000 2.0698 0.02327 0.01820 -0.2128 0.4001 0.6681
9.250 2.0861 0.02378 0.01875 -0.2120 0.3996 0.6694
9.500 2.1027 0.02430 0.01930 -0.2112 0.3991 0.6709
9.750 2.1183 0.02487 0.01991 -0.2104 0.3986 0.6725
10.000 2.1336 0.02547 0.02055 -0.2096 0.3981 0.6740
10.250 2.1482 0.02611 0.02123 -0.2088 0.3976 0.6752
10.500 2.1621 0.02682 0.02198 -0.2080 0.3971 0.6764
10.750 2.1755 0.02760 0.02279 -0.2073 0.3965 0.6775
11.000 2.1886 0.02842 0.02365 -0.2065 0.3960 0.6785
11.250 2.2011 0.02932 0.02458 -0.2058 0.3953 0.6794
11.500 2.2128 0.03029 0.02557 -0.2051 0.3944 0.6802
11.750 2.2221 0.03147 0.02678 -0.2042 0.3934 0.6809
12.000 2.2225 0.03335 0.02877 -0.2029 0.3927 0.6820
12.250 2.2183 0.03574 0.03128 -0.2015 0.3915 0.6835
12.500 2.2086 0.03877 0.03443 -0.2001 0.3897 0.6848
12.750 2.1930 0.04252 0.03830 -0.1988 0.3876 0.6860
13.000 2.1553 0.04864 0.04457 -0.1971 0.3845 0.6868
13.250 2.0967 0.05705 0.05307 -0.1949 0.3798 0.6873
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