FX 83-W-227 (fx83w227-il) Xfoil prediction polar at RE=100,000 Ncrit=5
| Details | Polar file |
|---|---|
|
Airfoil: FX 83-W-227 (fx83w227-il) Reynolds number: 100,000 Max Cl/Cd: 31.29 at α=6.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx83w227-il-100000-n5.txt Download as CSV file: xf-fx83w227-il-100000-n5.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 = 0.100 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-16.000 -0.6944 0.08376 0.07737 -0.0911 1.0000 0.0808
-15.750 -0.7565 0.07518 0.06851 -0.0930 1.0000 0.0810
-15.500 -0.7775 0.07011 0.06326 -0.0952 0.9980 0.0818
-15.250 -0.7569 0.06822 0.06139 -0.0978 0.9942 0.0831
-15.000 -0.7517 0.06485 0.05790 -0.1008 0.9896 0.0844
-14.750 -0.7509 0.06118 0.05406 -0.1039 0.9847 0.0858
-14.500 -0.7518 0.05751 0.05016 -0.1067 0.9797 0.0872
-14.250 -0.7545 0.05405 0.04642 -0.1087 0.9731 0.0888
-14.000 -0.7556 0.05081 0.04285 -0.1105 0.9670 0.0904
-13.750 -0.7353 0.04948 0.04157 -0.1116 0.9610 0.0919
-13.500 -0.7146 0.04792 0.03997 -0.1136 0.9568 0.0937
-13.250 -0.7047 0.04627 0.03822 -0.1139 0.9488 0.0954
-13.000 -0.6903 0.04439 0.03615 -0.1153 0.9435 0.0978
-12.750 -0.6818 0.04266 0.03418 -0.1153 0.9358 0.0998
-12.500 -0.6609 0.04135 0.03285 -0.1162 0.9301 0.1019
-12.250 -0.6352 0.04011 0.03160 -0.1180 0.9265 0.1043
-12.000 -0.6239 0.03904 0.03044 -0.1172 0.9176 0.1066
-11.750 -0.6033 0.03771 0.02894 -0.1181 0.9126 0.1097
-11.500 -0.5748 0.03642 0.02754 -0.1201 0.9094 0.1127
-11.250 -0.5631 0.03566 0.02679 -0.1187 0.8998 0.1150
-11.000 -0.5376 0.03461 0.02567 -0.1199 0.8951 0.1185
-10.750 -0.5109 0.03351 0.02439 -0.1213 0.8912 0.1227
-10.500 -0.4989 0.03283 0.02373 -0.1196 0.8817 0.1255
-10.250 -0.4729 0.03191 0.02278 -0.1206 0.8769 0.1295
-10.000 -0.4516 0.03111 0.02188 -0.1206 0.8709 0.1340
-9.750 -0.4360 0.03045 0.02117 -0.1194 0.8629 0.1380
-9.500 -0.4100 0.02961 0.02032 -0.1202 0.8582 0.1428
-9.250 -0.3938 0.02902 0.01965 -0.1191 0.8509 0.1479
-9.000 -0.3773 0.02841 0.01903 -0.1179 0.8436 0.1530
-8.750 -0.3520 0.02765 0.01824 -0.1184 0.8389 0.1592
-8.500 -0.3416 0.02729 0.01778 -0.1159 0.8307 0.1650
-8.250 -0.3267 0.02672 0.01726 -0.1144 0.8238 0.1709
-8.000 -0.3011 0.02605 0.01652 -0.1146 0.8193 0.1797
-7.750 -0.2996 0.02583 0.01631 -0.1104 0.8104 0.1851
-7.500 -0.2851 0.02536 0.01584 -0.1086 0.8041 0.1933
-7.250 -0.2618 0.02474 0.01520 -0.1083 0.7997 0.2036
-7.000 -0.2674 0.02472 0.01520 -0.1025 0.7904 0.2101
-6.750 -0.2534 0.02432 0.01479 -0.1004 0.7845 0.2208
-6.500 -0.2298 0.02378 0.01424 -0.1000 0.7805 0.2353
-6.250 -0.2360 0.02378 0.01429 -0.0941 0.7714 0.2445
-6.000 -0.2220 0.02340 0.01395 -0.0918 0.7657 0.2596
-5.750 -0.1994 0.02289 0.01347 -0.0912 0.7617 0.2796
-5.500 -0.2032 0.02289 0.01353 -0.0856 0.7535 0.2938
-5.250 -0.1920 0.02260 0.01330 -0.0827 0.7475 0.3144
-5.000 -0.1700 0.02215 0.01291 -0.0818 0.7434 0.3417
-4.750 -0.1667 0.02207 0.01290 -0.0774 0.7365 0.3632
-4.500 -0.1599 0.02193 0.01285 -0.0737 0.7299 0.3871
-4.250 -0.1384 0.02159 0.01260 -0.0725 0.7256 0.4174
-4.000 -0.1110 0.02126 0.01234 -0.0724 0.7223 0.4497
-3.750 -0.1203 0.02149 0.01268 -0.0655 0.7134 0.4685
-3.500 -0.1009 0.02137 0.01262 -0.0638 0.7086 0.4968
-3.250 -0.0709 0.02117 0.01242 -0.0640 0.7051 0.5251
-3.000 -0.0660 0.02133 0.01263 -0.0597 0.6984 0.5449
-2.750 -0.0553 0.02143 0.01275 -0.0564 0.6921 0.5648
-2.500 -0.0279 0.02136 0.01265 -0.0561 0.6881 0.5859
-2.250 0.0077 0.02123 0.01247 -0.0573 0.6850 0.6061
-2.000 -0.0032 0.02158 0.01285 -0.0502 0.6766 0.6202
-1.750 0.0174 0.02165 0.01291 -0.0486 0.6716 0.6362
-1.500 0.0508 0.02159 0.01281 -0.0493 0.6681 0.6531
-1.250 0.0741 0.02165 0.01283 -0.0483 0.6637 0.6683
-1.000 0.0623 0.02194 0.01314 -0.0410 0.6556 0.6815
-0.750 0.0916 0.02197 0.01317 -0.0410 0.6514 0.6950
-0.500 0.1300 0.02189 0.01301 -0.0426 0.6483 0.7085
-0.250 0.1240 0.02217 0.01330 -0.0365 0.6414 0.7207
0.000 0.1372 0.02236 0.01352 -0.0337 0.6353 0.7312
0.250 0.1657 0.02224 0.01331 -0.0337 0.6315 0.7438
0.500 0.2113 0.02213 0.01314 -0.0367 0.6287 0.7530
0.750 0.1888 0.02268 0.01375 -0.0279 0.6201 0.7648
1.000 0.2139 0.02277 0.01384 -0.0273 0.6152 0.7739
1.250 0.2465 0.02256 0.01354 -0.0281 0.6118 0.7850
1.500 0.2806 0.02257 0.01353 -0.0291 0.6080 0.7933
1.750 0.2639 0.02323 0.01427 -0.0217 0.5995 0.8059
2.000 0.2974 0.02322 0.01424 -0.0227 0.5954 0.8147
2.500 0.3416 0.02356 0.01456 -0.0210 0.5855 0.8356
2.750 0.3544 0.02390 0.01492 -0.0188 0.5794 0.8474
3.000 0.3960 0.02381 0.01479 -0.0213 0.5758 0.8557
3.250 0.4390 0.02354 0.01444 -0.0239 0.5729 0.8654
3.500 0.4394 0.02457 0.01561 -0.0203 0.5645 0.8769
3.750 0.4696 0.02476 0.01579 -0.0211 0.5596 0.8872
4.000 0.5184 0.02463 0.01561 -0.0249 0.5562 0.8937
4.250 0.5504 0.02482 0.01578 -0.0261 0.5517 0.9041
4.500 0.5651 0.02582 0.01688 -0.0254 0.5440 0.9152
4.750 0.6054 0.02587 0.01690 -0.0280 0.5398 0.9239
5.000 0.6569 0.02569 0.01665 -0.0323 0.5367 0.9296
5.250 0.6710 0.02673 0.01778 -0.0317 0.5294 0.9425
5.500 0.6997 0.02719 0.01826 -0.0329 0.5237 0.9540
5.750 0.7473 0.02711 0.01813 -0.0367 0.5200 0.9595
6.000 0.7915 0.02702 0.01798 -0.0399 0.5166 0.9679
6.250 0.7987 0.02854 0.01965 -0.0391 0.5084 0.9833
6.500 0.8394 0.02868 0.01977 -0.0422 0.5038 0.9917
6.750 0.8904 0.02846 0.01949 -0.0465 0.5004 0.9980
7.000 0.8571 0.02969 0.02075 -0.0382 0.4940 1.0000
7.250 0.8413 0.03067 0.02172 -0.0324 0.4879 1.0000
7.500 0.8628 0.03059 0.02158 -0.0315 0.4842 1.0000
7.750 0.8978 0.03016 0.02107 -0.0323 0.4814 1.0000
8.000 0.8415 0.03323 0.02425 -0.0224 0.4718 1.0000
8.250 0.8587 0.03352 0.02451 -0.0211 0.4677 1.0000
8.500 0.8907 0.03315 0.02409 -0.0215 0.4649 1.0000
8.750 0.8564 0.03607 0.02709 -0.0152 0.4564 1.0000
9.000 0.8600 0.03719 0.02822 -0.0129 0.4508 1.0000
9.250 0.8901 0.03686 0.02786 -0.0129 0.4480 1.0000
9.500 0.9278 0.03617 0.02714 -0.0138 0.4459 1.0000
10.000 0.8887 0.04148 0.03257 -0.0058 0.4307 1.0000
10.250 0.9257 0.04066 0.03172 -0.0064 0.4288 1.0000
10.750 0.8845 0.04716 0.03836 0.0001 0.4128 1.0000
11.000 0.9226 0.04603 0.03721 -0.0004 0.4111 1.0000
11.250 0.9623 0.04492 0.03610 -0.0010 0.4097 1.0000
11.750 0.8244 0.06139 0.05281 0.0075 0.3796 1.0000
12.000 0.8513 0.06093 0.05237 0.0078 0.3777 1.0000
12.250 0.8812 0.06020 0.05165 0.0080 0.3763 1.0000
12.500 0.9154 0.05909 0.05055 0.0081 0.3752 1.0000
15.000 0.8688 0.09000 0.08201 0.0135 0.3045 1.0000
|
Polar data table (+)
Polar graphs
<< Back to FX 83-W-227 (fx83w227-il)