FX S 03-182 AIRFOIL (fxs03182-il) Xfoil prediction polar at RE=100,000 Ncrit=9
| Details | Polar file |
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Airfoil: FX S 03-182 AIRFOIL (fxs03182-il) Reynolds number: 100,000 Max Cl/Cd: 27.45 at α=11° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-fxs03182-il-100000.txt Download as CSV file: xf-fxs03182-il-100000.csv |
XFOIL Version 6.96
Calculated polar for: FX S 03-182 AIRFOIL
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.100 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-13.000 -0.3363 0.13875 0.13430 -0.0569 1.0000 0.0966
-12.750 -0.3709 0.14132 0.13706 -0.0491 1.0000 0.0966
-12.500 -0.4037 0.13678 0.13265 -0.0575 0.9962 0.1010
-12.250 -0.3727 0.13130 0.12714 -0.0581 0.9933 0.1034
-12.000 -0.3504 0.12717 0.12297 -0.0609 0.9887 0.1063
-11.750 -0.2463 0.09446 0.09036 -0.0929 0.9597 0.0574
-11.500 -0.3313 0.07605 0.07181 -0.1040 0.9580 0.0508
-11.250 -0.3451 0.06895 0.06453 -0.1082 0.9554 0.0480
-11.000 -0.3566 0.06366 0.05915 -0.1103 0.9493 0.0470
-10.750 -0.4666 0.07227 0.06747 -0.1050 0.9583 0.0478
-10.500 -0.4720 0.06713 0.06215 -0.1086 0.9522 0.0468
-10.250 -0.4821 0.06301 0.05781 -0.1102 0.9431 0.0456
-10.000 -0.4972 0.05971 0.05427 -0.1098 0.9332 0.0445
-9.750 -0.5060 0.05507 0.04918 -0.1102 0.9263 0.0419
-9.500 -0.5340 0.05282 0.04623 -0.1048 0.9143 0.0389
-9.250 -0.5330 0.05034 0.04340 -0.1028 0.9076 0.0388
-9.000 -0.5266 0.04869 0.04142 -0.1009 0.9008 0.0384
-8.750 -0.5023 0.04514 0.03743 -0.1022 0.8979 0.0383
-8.500 -0.5107 0.04425 0.03635 -0.0970 0.8888 0.0383
-8.250 -0.4831 0.04048 0.03228 -0.0978 0.8860 0.0393
-8.000 -0.4445 0.03776 0.02942 -0.1000 0.8844 0.0419
-7.750 -0.3998 0.03547 0.02693 -0.1024 0.8832 0.0469
-7.500 -0.4249 0.03611 0.02753 -0.0940 0.8738 0.0474
-7.250 -0.3907 0.03431 0.02581 -0.0948 0.8716 0.0568
-7.000 -0.3603 0.03306 0.02447 -0.0958 0.8693 0.0734
-6.750 -0.3970 0.03401 0.02542 -0.0859 0.8601 0.0727
-6.500 -0.3842 0.03340 0.02490 -0.0842 0.8568 0.0837
-6.250 -0.3623 0.03261 0.02413 -0.0838 0.8546 0.0949
-6.000 -0.3932 0.03346 0.02496 -0.0752 0.8489 0.0947
-5.750 -0.3920 0.03337 0.02481 -0.0715 0.8449 0.1021
-5.500 -0.3798 0.03275 0.02429 -0.0700 0.8421 0.1175
-5.250 -0.3655 0.03176 0.02363 -0.0693 0.8401 0.1583
-5.000 -0.3738 0.02922 0.02305 -0.0671 0.8382 0.4242
-4.750 -0.3813 0.03120 0.02550 -0.0600 0.8357 0.5721
-4.500 -0.3764 0.03311 0.02731 -0.0550 0.8331 0.6131
-4.250 -0.3684 0.03473 0.02879 -0.0508 0.8317 0.6373
-4.000 -0.3599 0.03608 0.03002 -0.0470 0.8310 0.6529
-3.750 -0.3517 0.03751 0.03140 -0.0423 0.8297 0.6644
-3.500 -0.3425 0.03889 0.03271 -0.0379 0.8286 0.6795
-3.250 -0.3431 0.04026 0.03406 -0.0323 0.8295 0.6924
-3.000 -0.3444 0.04154 0.03532 -0.0265 0.8310 0.7062
-2.750 -0.3444 0.04281 0.03656 -0.0207 0.8322 0.7233
-2.500 -0.3439 0.04415 0.03786 -0.0148 0.8359 0.7421
-2.250 -0.4321 0.04212 0.03604 -0.0078 0.9312 0.7266
-2.000 -0.4236 0.04401 0.03792 -0.0012 0.9269 0.7457
-1.750 -0.4235 0.04479 0.03867 0.0056 0.9227 0.7649
-1.500 -0.4153 0.04540 0.03920 0.0104 0.9157 0.7856
-1.250 -0.3984 0.04667 0.04038 0.0138 0.9119 0.8019
-1.000 -0.3914 0.04626 0.03988 0.0168 0.9060 0.8103
-0.750 -0.3662 0.04648 0.03996 0.0158 0.9002 0.8162
-0.500 -0.3331 0.04765 0.04098 0.0138 0.8969 0.8205
-0.250 -0.3243 0.04677 0.03999 0.0152 0.8893 0.8248
0.000 -0.2895 0.04739 0.04045 0.0116 0.8847 0.8280
0.250 -0.2627 0.04823 0.04119 0.0103 0.8818 0.8305
0.500 -0.2491 0.04769 0.04057 0.0112 0.8728 0.8330
0.750 -0.2133 0.04879 0.04155 0.0082 0.8689 0.8356
1.000 -0.2005 0.04855 0.04124 0.0087 0.8622 0.8383
1.250 -0.1668 0.04930 0.04189 0.0057 0.8563 0.8409
1.500 -0.1286 0.05081 0.04330 0.0018 0.8532 0.8430
1.750 -0.1203 0.05018 0.04265 0.0036 0.8436 0.8451
2.000 -0.0827 0.05163 0.04404 0.0004 0.8397 0.8473
2.250 -0.0726 0.05134 0.04372 0.0014 0.8305 0.8490
2.500 -0.0339 0.05272 0.04504 -0.0021 0.8257 0.8510
2.750 -0.0213 0.05280 0.04511 -0.0018 0.8171 0.8534
3.000 0.0177 0.05415 0.04641 -0.0055 0.8117 0.8556
3.250 0.0326 0.05450 0.04676 -0.0057 0.8031 0.8574
3.500 0.0666 0.05568 0.04793 -0.0081 0.7975 0.8593
3.750 0.0784 0.05607 0.04833 -0.0075 0.7886 0.8614
4.000 0.1152 0.05743 0.04970 -0.0102 0.7827 0.8641
4.250 0.1268 0.05785 0.05014 -0.0098 0.7728 0.8668
4.500 0.1748 0.05979 0.05208 -0.0142 0.7672 0.8694
5.000 0.2027 0.06068 0.05304 -0.0139 0.7447 0.8740
5.250 0.2539 0.06247 0.05486 -0.0178 0.7380 0.8770
5.500 0.2610 0.06263 0.05508 -0.0167 0.7256 0.8803
5.750 0.3489 0.06004 0.05247 -0.0205 0.6811 0.8840
6.000 0.3691 0.06037 0.05287 -0.0206 0.6680 0.8873
6.250 0.3867 0.06084 0.05340 -0.0203 0.6559 0.8908
6.500 0.4132 0.06119 0.05383 -0.0209 0.6443 0.8946
6.750 0.4700 0.06071 0.05344 -0.0239 0.6375 0.8988
7.000 0.4842 0.06114 0.05396 -0.0233 0.6249 0.9033
7.250 0.4981 0.06184 0.05475 -0.0227 0.6135 0.9088
7.500 0.5479 0.06132 0.05437 -0.0249 0.6089 0.9148
7.750 0.5614 0.06161 0.05477 -0.0238 0.5961 0.9211
8.000 0.5816 0.06191 0.05518 -0.0237 0.5840 0.9280
8.250 0.6340 0.06023 0.05368 -0.0249 0.5798 0.9363
8.500 0.6504 0.06048 0.05407 -0.0245 0.5671 0.9462
8.750 0.6744 0.06037 0.05413 -0.0247 0.5548 0.9592
9.250 0.7805 0.05587 0.05005 -0.0288 0.5380 1.0000
9.500 0.8403 0.05160 0.04598 -0.0302 0.5249 1.0000
9.750 0.8947 0.04774 0.04231 -0.0314 0.5114 1.0000
10.000 0.9387 0.04512 0.03992 -0.0324 0.4972 1.0000
10.250 0.9765 0.04347 0.03845 -0.0334 0.4817 1.0000
10.500 1.0029 0.04302 0.03812 -0.0340 0.4564 1.0000
10.750 1.0489 0.04037 0.03539 -0.0346 0.4133 1.0000
11.000 1.0784 0.03929 0.03379 -0.0339 0.3389 1.0000
11.250 1.0796 0.04139 0.03542 -0.0328 0.2805 1.0000
11.500 1.0774 0.04406 0.03775 -0.0320 0.2342 1.0000
11.750 1.0753 0.04689 0.04028 -0.0313 0.1935 1.0000
12.000 1.0745 0.04970 0.04282 -0.0308 0.1615 1.0000
12.250 1.0753 0.05244 0.04533 -0.0304 0.1353 1.0000
12.500 1.0790 0.05497 0.04775 -0.0300 0.1145 1.0000
12.750 1.0836 0.05742 0.05011 -0.0297 0.0999 1.0000
13.000 1.0896 0.05977 0.05239 -0.0293 0.0887 1.0000
13.250 1.0961 0.06207 0.05463 -0.0290 0.0795 1.0000
13.500 1.1048 0.06420 0.05683 -0.0288 0.0721 1.0000
13.750 1.1143 0.06628 0.05893 -0.0286 0.0657 1.0000
14.000 1.1212 0.06865 0.06130 -0.0287 0.0602 1.0000
14.250 1.1309 0.07078 0.06350 -0.0286 0.0549 1.0000
14.500 1.1378 0.07325 0.06607 -0.0287 0.0501 1.0000
14.750 1.1466 0.07545 0.06821 -0.0286 0.0460 1.0000
15.000 1.1546 0.07798 0.07101 -0.0286 0.0423 1.0000
15.250 1.1610 0.08063 0.07375 -0.0288 0.0388 1.0000
15.500 1.1648 0.08367 0.07684 -0.0289 0.0350 1.0000
15.750 1.1700 0.08677 0.08017 -0.0289 0.0317 1.0000
16.000 1.1734 0.08996 0.08343 -0.0292 0.0291 1.0000
16.250 1.1817 0.09325 0.08684 -0.0287 0.0268 1.0000
16.500 1.1782 0.09765 0.09158 -0.0295 0.0260 1.0000
16.750 1.1722 0.10249 0.09674 -0.0306 0.0253 1.0000
17.000 1.1634 0.10782 0.10236 -0.0321 0.0249 1.0000
17.250 1.1513 0.11374 0.10857 -0.0342 0.0245 1.0000
17.500 1.1368 0.12020 0.11530 -0.0370 0.0244 1.0000
17.750 1.1199 0.12734 0.12271 -0.0405 0.0245 1.0000
18.000 1.1006 0.13527 0.13089 -0.0449 0.0247 1.0000
18.250 1.0792 0.14409 0.13994 -0.0503 0.0250 1.0000
18.500 1.0563 0.15390 0.14991 -0.0567 0.0254 1.0000
18.750 1.0313 0.16510 0.16125 -0.0641 0.0260 1.0000
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