FX 83-W-227 (fx83w227-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
|---|---|
|
Airfoil: FX 83-W-227 (fx83w227-il) Reynolds number: 1,000,000 Max Cl/Cd: 84.36 at α=8.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-fx83w227-il-1000000.txt Download as CSV file: xf-fx83w227-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: FX 83-W-227
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 1.000 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -1.0615 0.06696 0.06297 -0.0963 1.0000 0.0409
-19.500 -1.0684 0.06390 0.05984 -0.0966 1.0000 0.0413
-19.250 -1.0724 0.06128 0.05714 -0.0966 1.0000 0.0417
-19.000 -1.0808 0.05768 0.05347 -0.0977 0.9998 0.0423
-18.750 -1.0779 0.05406 0.04981 -0.1006 0.9990 0.0432
-18.500 -1.0697 0.05109 0.04679 -0.1033 0.9980 0.0439
-18.250 -1.0586 0.04849 0.04413 -0.1058 0.9968 0.0446
-18.000 -1.0444 0.04624 0.04183 -0.1082 0.9955 0.0454
-17.750 -1.0301 0.04400 0.03951 -0.1106 0.9943 0.0460
-17.500 -1.0108 0.04227 0.03772 -0.1129 0.9933 0.0467
-17.250 -0.9991 0.04000 0.03539 -0.1149 0.9918 0.0474
-17.000 -0.9899 0.03767 0.03304 -0.1165 0.9895 0.0485
-16.750 -0.9745 0.03579 0.03112 -0.1183 0.9874 0.0495
-16.500 -0.9553 0.03418 0.02947 -0.1204 0.9857 0.0503
-16.250 -0.9338 0.03274 0.02800 -0.1224 0.9842 0.0513
-16.000 -0.9113 0.03139 0.02658 -0.1246 0.9830 0.0520
-15.750 -0.8871 0.03013 0.02528 -0.1268 0.9820 0.0529
-15.500 -0.8784 0.02840 0.02353 -0.1270 0.9774 0.0542
-15.250 -0.8605 0.02700 0.02211 -0.1283 0.9742 0.0553
-15.000 -0.8361 0.02594 0.02103 -0.1300 0.9720 0.0566
-14.750 -0.8109 0.02489 0.01994 -0.1318 0.9701 0.0576
-14.500 -0.7923 0.02411 0.01912 -0.1319 0.9639 0.0586
-14.250 -0.7730 0.02281 0.01778 -0.1332 0.9589 0.0601
-14.000 -0.7463 0.02172 0.01668 -0.1354 0.9546 0.0616
-13.750 -0.7213 0.02083 0.01577 -0.1369 0.9460 0.0630
-13.500 -0.6823 0.02004 0.01493 -0.1409 0.9415 0.0644
-13.250 -0.6466 0.01939 0.01422 -0.1441 0.9327 0.0655
-13.000 -0.6113 0.01832 0.01310 -0.1481 0.9231 0.0679
-12.750 -0.5762 0.01761 0.01233 -0.1513 0.9095 0.0696
-12.500 -0.5485 0.01706 0.01169 -0.1528 0.8924 0.0714
-12.250 -0.5262 0.01667 0.01118 -0.1529 0.8753 0.0728
-12.000 -0.5133 0.01611 0.01053 -0.1515 0.8589 0.0743
-11.750 -0.5018 0.01560 0.00996 -0.1497 0.8449 0.0764
-11.500 -0.4890 0.01520 0.00949 -0.1480 0.8328 0.0781
-11.250 -0.4751 0.01486 0.00908 -0.1462 0.8219 0.0799
-11.000 -0.4599 0.01456 0.00871 -0.1446 0.8129 0.0813
-10.750 -0.4497 0.01412 0.00823 -0.1423 0.8036 0.0839
-10.500 -0.4375 0.01376 0.00784 -0.1402 0.7953 0.0862
-10.250 -0.4236 0.01347 0.00751 -0.1382 0.7871 0.0883
-10.000 -0.4081 0.01326 0.00722 -0.1364 0.7795 0.0903
-9.750 -0.3959 0.01290 0.00686 -0.1341 0.7727 0.0933
-9.500 -0.3829 0.01262 0.00656 -0.1319 0.7652 0.0963
-9.250 -0.3677 0.01241 0.00631 -0.1299 0.7585 0.0994
-9.000 -0.3530 0.01216 0.00604 -0.1278 0.7518 0.1027
-8.750 -0.3400 0.01193 0.00579 -0.1254 0.7450 0.1064
-8.500 -0.3244 0.01174 0.00558 -0.1233 0.7389 0.1099
-8.250 -0.3090 0.01154 0.00535 -0.1212 0.7326 0.1136
-8.000 -0.2958 0.01133 0.00514 -0.1187 0.7261 0.1187
-7.750 -0.2798 0.01118 0.00496 -0.1166 0.7203 0.1227
-7.500 -0.2653 0.01097 0.00477 -0.1142 0.7146 0.1279
-7.250 -0.2515 0.01081 0.00459 -0.1117 0.7086 0.1331
-7.000 -0.2365 0.01071 0.00445 -0.1093 0.7026 0.1375
-6.750 -0.2238 0.01052 0.00430 -0.1064 0.6976 0.1446
-6.500 -0.2099 0.01044 0.00420 -0.1037 0.6919 0.1499
-6.250 -0.1982 0.01034 0.00409 -0.1006 0.6860 0.1575
-6.000 -0.1808 0.01021 0.00398 -0.0987 0.6812 0.1647
-5.750 -0.1645 0.01005 0.00385 -0.0965 0.6759 0.1747
-5.500 -0.1473 0.00994 0.00374 -0.0945 0.6706 0.1842
-5.250 -0.1310 0.00982 0.00363 -0.0923 0.6651 0.1963
-5.000 -0.1132 0.00964 0.00351 -0.0904 0.6606 0.2102
-4.750 -0.0958 0.00948 0.00340 -0.0884 0.6556 0.2255
-4.500 -0.0794 0.00934 0.00329 -0.0862 0.6504 0.2431
-4.250 -0.0622 0.00919 0.00320 -0.0842 0.6456 0.2624
-4.000 -0.0441 0.00901 0.00310 -0.0823 0.6412 0.2842
-3.750 -0.0267 0.00885 0.00300 -0.0803 0.6361 0.3071
-3.500 -0.0103 0.00870 0.00291 -0.0781 0.6312 0.3307
-3.250 0.0068 0.00855 0.00283 -0.0760 0.6267 0.3567
-3.000 0.0254 0.00838 0.00275 -0.0742 0.6225 0.3814
-2.500 0.0567 0.00811 0.00261 -0.0694 0.6126 0.4300
-2.250 0.0727 0.00799 0.00255 -0.0670 0.6082 0.4562
-2.000 0.0909 0.00786 0.00250 -0.0650 0.6043 0.4825
-1.750 0.1085 0.00776 0.00247 -0.0630 0.5995 0.5059
-1.500 0.1256 0.00770 0.00245 -0.0608 0.5945 0.5276
-1.250 0.1448 0.00769 0.00245 -0.0591 0.5897 0.5453
-1.000 0.1664 0.00765 0.00246 -0.0578 0.5859 0.5623
-0.750 0.1870 0.00764 0.00248 -0.0564 0.5812 0.5770
-0.500 0.2065 0.00766 0.00251 -0.0547 0.5761 0.5897
0.000 0.2493 0.00771 0.00258 -0.0522 0.5672 0.6125
0.250 0.2713 0.00775 0.00262 -0.0511 0.5624 0.6225
0.500 0.2910 0.00780 0.00267 -0.0495 0.5574 0.6326
0.750 0.3123 0.00788 0.00273 -0.0482 0.5523 0.6418
1.000 0.3343 0.00789 0.00278 -0.0471 0.5480 0.6517
1.250 0.3555 0.00796 0.00284 -0.0458 0.5429 0.6619
1.500 0.3740 0.00803 0.00292 -0.0441 0.5377 0.6717
1.750 0.3961 0.00811 0.00299 -0.0430 0.5330 0.6800
2.000 0.4177 0.00814 0.00306 -0.0419 0.5279 0.6883
2.250 0.4376 0.00823 0.00314 -0.0404 0.5228 0.6963
2.500 0.4558 0.00838 0.00324 -0.0386 0.5172 0.7036
2.750 0.4784 0.00841 0.00332 -0.0377 0.5131 0.7111
3.000 0.4997 0.00849 0.00341 -0.0365 0.5079 0.7183
3.250 0.5181 0.00863 0.00352 -0.0349 0.5023 0.7250
3.500 0.5371 0.00873 0.00365 -0.0333 0.4975 0.7328
3.750 0.5588 0.00882 0.00375 -0.0322 0.4929 0.7402
4.000 0.5785 0.00894 0.00387 -0.0309 0.4878 0.7473
4.250 0.5951 0.00910 0.00403 -0.0289 0.4824 0.7556
4.500 0.6157 0.00923 0.00417 -0.0277 0.4780 0.7637
4.750 0.6349 0.00932 0.00431 -0.0262 0.4729 0.7730
5.000 0.6526 0.00949 0.00448 -0.0245 0.4677 0.7821
5.250 0.6685 0.00969 0.00468 -0.0225 0.4626 0.7915
5.500 0.6891 0.00979 0.00483 -0.0214 0.4588 0.8015
5.750 0.7074 0.00993 0.00501 -0.0198 0.4540 0.8122
6.000 0.7235 0.01014 0.00523 -0.0179 0.4489 0.8242
6.250 0.7390 0.01033 0.00547 -0.0159 0.4440 0.8391
6.500 0.7589 0.01044 0.00567 -0.0147 0.4402 0.8576
6.750 0.7808 0.01058 0.00592 -0.0140 0.4355 0.8845
7.000 0.8267 0.01087 0.00631 -0.0186 0.4298 0.9186
7.250 0.8897 0.01118 0.00665 -0.0268 0.4244 0.9388
7.500 0.9490 0.01148 0.00698 -0.0342 0.4191 0.9517
7.750 0.9950 0.01190 0.00737 -0.0389 0.4133 0.9645
8.000 1.0297 0.01231 0.00778 -0.0412 0.4082 0.9779
8.250 1.0646 0.01262 0.00811 -0.0433 0.4040 0.9863
8.500 1.0957 0.01308 0.00856 -0.0449 0.3992 0.9944
9.000 1.1632 0.01399 0.00945 -0.0493 0.3893 1.0000
9.250 1.1756 0.01430 0.00978 -0.0470 0.3852 1.0000
9.500 1.1854 0.01474 0.01020 -0.0444 0.3805 1.0000
9.750 1.1924 0.01533 0.01076 -0.0415 0.3750 1.0000
10.000 1.2078 0.01568 0.01113 -0.0400 0.3716 1.0000
10.250 1.2223 0.01609 0.01156 -0.0383 0.3672 1.0000
10.500 1.2335 0.01665 0.01212 -0.0363 0.3625 1.0000
10.750 1.2419 0.01738 0.01282 -0.0339 0.3571 1.0000
11.000 1.2587 0.01780 0.01327 -0.0328 0.3525 1.0000
11.250 1.2699 0.01849 0.01395 -0.0310 0.3458 1.0000
11.500 1.2782 0.01936 0.01479 -0.0289 0.3391 1.0000
11.750 1.2930 0.01996 0.01541 -0.0277 0.3329 1.0000
12.000 1.3031 0.02081 0.01625 -0.0260 0.3268 1.0000
12.250 1.3134 0.02169 0.01714 -0.0244 0.3221 1.0000
12.500 1.3291 0.02231 0.01778 -0.0235 0.3176 1.0000
12.750 1.3405 0.02318 0.01866 -0.0221 0.3126 1.0000
13.000 1.3472 0.02435 0.01981 -0.0204 0.3064 1.0000
13.250 1.3619 0.02509 0.02059 -0.0195 0.3021 1.0000
13.500 1.3727 0.02608 0.02159 -0.0183 0.2964 1.0000
13.750 1.3772 0.02748 0.02297 -0.0166 0.2896 1.0000
14.000 1.3909 0.02834 0.02386 -0.0157 0.2852 1.0000
14.250 1.4003 0.02947 0.02501 -0.0146 0.2791 1.0000
14.500 1.4042 0.03103 0.02655 -0.0130 0.2723 1.0000
14.750 1.4152 0.03213 0.02768 -0.0121 0.2660 1.0000
15.000 1.4167 0.03391 0.02944 -0.0106 0.2582 1.0000
15.250 1.4250 0.03524 0.03079 -0.0096 0.2514 1.0000
15.500 1.4254 0.03718 0.03271 -0.0082 0.2429 1.0000
15.750 1.4275 0.03905 0.03457 -0.0069 0.2330 1.0000
16.000 1.4267 0.04116 0.03667 -0.0056 0.2243 1.0000
16.250 1.4264 0.04330 0.03880 -0.0044 0.2147 1.0000
16.500 1.4246 0.04559 0.04107 -0.0032 0.2057 1.0000
16.750 1.4178 0.04833 0.04377 -0.0019 0.1944 1.0000
17.000 1.4118 0.05111 0.04654 -0.0008 0.1834 1.0000
17.250 1.4084 0.05370 0.04912 0.0002 0.1747 1.0000
17.500 1.4000 0.05677 0.05216 0.0012 0.1640 1.0000
17.750 1.3908 0.06000 0.05537 0.0021 0.1544 1.0000
18.000 1.3861 0.06290 0.05828 0.0027 0.1464 1.0000
18.250 1.3759 0.06634 0.06169 0.0034 0.1361 1.0000
18.500 1.3703 0.06942 0.06478 0.0038 0.1299 1.0000
18.750 1.3630 0.07273 0.06809 0.0042 0.1223 1.0000
19.000 1.3529 0.07637 0.07171 0.0045 0.1136 1.0000
19.250 1.3459 0.07977 0.07512 0.0046 0.1074 1.0000
|
Polar data table (+)
Polar graphs
<< Back to FX 83-W-227 (fx83w227-il)