FX 84-W-150 (fx84w150-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: FX 84-W-150 (fx84w150-il) Reynolds number: 1,000,000 Max Cl/Cd: 133.33 at α=6° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx84w150-il-1000000-n5.txt Download as CSV file: xf-fx84w150-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: FX 84-W-150
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
------ -------- --------- --------- -------- -------- --------
-17.000 -0.6128 0.11515 0.11305 -0.0541 0.9923 0.0106
-16.750 -0.6710 0.09881 0.09654 -0.0649 0.9743 0.0105
-16.500 -0.8476 0.06292 0.06016 -0.0906 0.9606 0.0100
-16.250 -0.9180 0.04377 0.04048 -0.1080 0.9266 0.0098
-16.000 -0.9403 0.03810 0.03456 -0.1115 0.9037 0.0099
-15.750 -0.9563 0.03420 0.03046 -0.1128 0.8881 0.0099
-15.500 -0.9647 0.03149 0.02759 -0.1129 0.8761 0.0100
-15.000 -0.9711 0.02765 0.02348 -0.1112 0.8566 0.0101
-14.750 -0.9695 0.02630 0.02201 -0.1098 0.8481 0.0103
-14.500 -0.9672 0.02507 0.02068 -0.1080 0.8403 0.0104
-14.250 -0.9632 0.02407 0.01957 -0.1060 0.8331 0.0106
-14.000 -0.9588 0.02316 0.01857 -0.1035 0.8269 0.0106
-13.750 -0.9496 0.02242 0.01772 -0.1015 0.8208 0.0108
-13.500 -0.9360 0.02166 0.01686 -0.1001 0.8153 0.0110
-13.250 -0.9198 0.02096 0.01607 -0.0991 0.8100 0.0112
-13.000 -0.9024 0.02029 0.01530 -0.0981 0.8046 0.0114
-12.500 -0.8643 0.01904 0.01387 -0.0965 0.7954 0.0117
-12.250 -0.8436 0.01848 0.01321 -0.0958 0.7905 0.0118
-12.000 -0.8235 0.01783 0.01248 -0.0951 0.7855 0.0121
-11.750 -0.8022 0.01723 0.01181 -0.0945 0.7811 0.0124
-11.500 -0.7796 0.01671 0.01124 -0.0940 0.7765 0.0128
-11.250 -0.7565 0.01624 0.01070 -0.0936 0.7715 0.0131
-10.750 -0.7085 0.01540 0.00972 -0.0929 0.7628 0.0139
-10.500 -0.6838 0.01501 0.00927 -0.0927 0.7581 0.0143
-10.250 -0.6589 0.01464 0.00883 -0.0924 0.7536 0.0146
-10.000 -0.6343 0.01421 0.00834 -0.0921 0.7494 0.0151
-9.750 -0.6090 0.01381 0.00791 -0.0920 0.7451 0.0157
-9.500 -0.5833 0.01347 0.00752 -0.0918 0.7407 0.0162
-9.250 -0.5574 0.01316 0.00715 -0.0917 0.7364 0.0168
-9.000 -0.5312 0.01286 0.00680 -0.0916 0.7323 0.0174
-8.750 -0.5046 0.01258 0.00646 -0.0915 0.7280 0.0179
-8.500 -0.4784 0.01225 0.00611 -0.0914 0.7237 0.0188
-8.250 -0.4518 0.01199 0.00581 -0.0913 0.7197 0.0197
-8.000 -0.4248 0.01174 0.00553 -0.0913 0.7161 0.0206
-7.750 -0.3976 0.01151 0.00526 -0.0913 0.7118 0.0214
-7.500 -0.3706 0.01125 0.00496 -0.0913 0.7073 0.0224
-7.250 -0.3435 0.01102 0.00471 -0.0913 0.7031 0.0236
-7.000 -0.3159 0.01081 0.00448 -0.0914 0.6995 0.0247
-6.750 -0.2882 0.01063 0.00426 -0.0914 0.6954 0.0258
-6.500 -0.2608 0.01041 0.00402 -0.0915 0.6909 0.0274
-6.000 -0.2052 0.01007 0.00363 -0.0916 0.6825 0.0303
-5.750 -0.1774 0.00989 0.00343 -0.0917 0.6777 0.0319
-5.500 -0.1497 0.00973 0.00325 -0.0918 0.6728 0.0339
-5.250 -0.1216 0.00960 0.00309 -0.0919 0.6686 0.0359
-5.000 -0.0935 0.00943 0.00292 -0.0921 0.6642 0.0385
-4.750 -0.0654 0.00929 0.00277 -0.0922 0.6596 0.0413
-4.500 -0.0374 0.00918 0.00263 -0.0923 0.6551 0.0444
-4.250 -0.0091 0.00904 0.00250 -0.0925 0.6512 0.0481
-4.000 0.0192 0.00891 0.00238 -0.0926 0.6470 0.0523
-3.750 0.0474 0.00880 0.00227 -0.0928 0.6425 0.0574
-3.500 0.0756 0.00870 0.00216 -0.0929 0.6382 0.0631
-3.250 0.1041 0.00859 0.00207 -0.0931 0.6340 0.0698
-3.000 0.1324 0.00848 0.00198 -0.0933 0.6296 0.0783
-2.750 0.1607 0.00839 0.00190 -0.0935 0.6254 0.0880
-2.500 0.1890 0.00829 0.00183 -0.0937 0.6213 0.0995
-2.250 0.2175 0.00820 0.00177 -0.0939 0.6170 0.1116
-2.000 0.2458 0.00810 0.00171 -0.0941 0.6123 0.1279
-1.750 0.2739 0.00801 0.00166 -0.0943 0.6080 0.1477
-1.500 0.3023 0.00790 0.00162 -0.0945 0.6040 0.1720
-1.250 0.3306 0.00778 0.00158 -0.0948 0.5992 0.2022
-1.000 0.3586 0.00767 0.00155 -0.0949 0.5939 0.2376
-0.750 0.3865 0.00752 0.00153 -0.0952 0.5890 0.2855
-0.500 0.4144 0.00732 0.00150 -0.0954 0.5839 0.3450
-0.250 0.4420 0.00712 0.00149 -0.0956 0.5790 0.4192
0.000 0.4695 0.00691 0.00150 -0.0958 0.5747 0.4990
0.250 0.4974 0.00673 0.00152 -0.0960 0.5701 0.5700
0.500 0.5253 0.00664 0.00155 -0.0962 0.5649 0.6222
0.750 0.5531 0.00662 0.00160 -0.0963 0.5601 0.6595
1.000 0.5814 0.00658 0.00165 -0.0964 0.5561 0.6928
1.250 0.6095 0.00658 0.00171 -0.0966 0.5515 0.7183
1.500 0.6373 0.00661 0.00177 -0.0966 0.5465 0.7397
1.750 0.6652 0.00665 0.00184 -0.0967 0.5418 0.7611
2.000 0.6927 0.00666 0.00193 -0.0967 0.5368 0.7872
2.250 0.7200 0.00671 0.00201 -0.0966 0.5315 0.8066
2.500 0.7476 0.00679 0.00208 -0.0967 0.5262 0.8172
2.750 0.7753 0.00685 0.00216 -0.0967 0.5200 0.8267
3.000 0.8023 0.00695 0.00225 -0.0967 0.5140 0.8347
3.250 0.8299 0.00702 0.00233 -0.0967 0.5087 0.8424
3.500 0.8573 0.00710 0.00242 -0.0968 0.5028 0.8495
3.750 0.8837 0.00721 0.00253 -0.0966 0.4973 0.8572
4.250 0.9372 0.00739 0.00274 -0.0964 0.4845 0.8719
4.500 0.9634 0.00752 0.00285 -0.0963 0.4762 0.8796
4.750 0.9885 0.00765 0.00298 -0.0959 0.4676 0.8871
5.000 1.0141 0.00777 0.00311 -0.0956 0.4597 0.8954
5.250 1.0385 0.00791 0.00326 -0.0951 0.4522 0.9036
5.750 1.0865 0.00818 0.00355 -0.0939 0.4375 0.9231
6.000 1.1093 0.00832 0.00371 -0.0930 0.4298 0.9349
6.250 1.1297 0.00852 0.00390 -0.0917 0.4173 0.9509
6.500 1.1517 0.00889 0.00417 -0.0911 0.3901 0.9751
6.750 1.1727 0.00942 0.00453 -0.0904 0.3580 1.0000
7.000 1.1891 0.00990 0.00489 -0.0887 0.3319 1.0000
7.250 1.2004 0.01043 0.00528 -0.0861 0.3054 1.0000
7.500 1.2097 0.01101 0.00573 -0.0831 0.2818 1.0000
7.750 1.2196 0.01161 0.00623 -0.0804 0.2594 1.0000
8.000 1.2291 0.01228 0.00680 -0.0778 0.2377 1.0000
8.250 1.2367 0.01307 0.00747 -0.0750 0.2135 1.0000
8.500 1.2436 0.01394 0.00822 -0.0723 0.1913 1.0000
8.750 1.2514 0.01483 0.00901 -0.0698 0.1697 1.0000
9.000 1.2563 0.01591 0.00997 -0.0671 0.1459 1.0000
9.250 1.2621 0.01701 0.01096 -0.0646 0.1247 1.0000
9.500 1.2686 0.01813 0.01199 -0.0624 0.1072 1.0000
9.750 1.2764 0.01922 0.01302 -0.0604 0.0926 1.0000
10.000 1.2844 0.02035 0.01409 -0.0586 0.0802 1.0000
10.250 1.2930 0.02147 0.01519 -0.0569 0.0703 1.0000
10.500 1.3016 0.02264 0.01632 -0.0553 0.0617 1.0000
10.750 1.3111 0.02379 0.01745 -0.0538 0.0545 1.0000
11.000 1.3206 0.02496 0.01861 -0.0525 0.0487 1.0000
11.250 1.3293 0.02623 0.01987 -0.0511 0.0431 1.0000
11.500 1.3381 0.02752 0.02115 -0.0499 0.0384 1.0000
11.750 1.3484 0.02873 0.02239 -0.0488 0.0358 1.0000
12.000 1.3574 0.03009 0.02375 -0.0477 0.0325 1.0000
12.250 1.3668 0.03145 0.02513 -0.0467 0.0300 1.0000
12.500 1.3764 0.03283 0.02654 -0.0458 0.0281 1.0000
12.750 1.3846 0.03436 0.02808 -0.0449 0.0260 1.0000
13.000 1.3941 0.03582 0.02958 -0.0441 0.0245 1.0000
13.250 1.4027 0.03739 0.03118 -0.0434 0.0231 1.0000
13.500 1.4106 0.03907 0.03288 -0.0427 0.0219 1.0000
13.750 1.4189 0.04074 0.03459 -0.0420 0.0211 1.0000
14.000 1.4275 0.04240 0.03630 -0.0415 0.0200 1.0000
14.250 1.4350 0.04422 0.03817 -0.0410 0.0193 1.0000
14.500 1.4419 0.04613 0.04011 -0.0405 0.0185 1.0000
14.750 1.4476 0.04822 0.04224 -0.0401 0.0176 1.0000
15.000 1.4553 0.05012 0.04419 -0.0397 0.0171 1.0000
15.250 1.4622 0.05213 0.04626 -0.0395 0.0165 1.0000
15.500 1.4681 0.05431 0.04849 -0.0393 0.0159 1.0000
15.750 1.4737 0.05654 0.05076 -0.0391 0.0153 1.0000
16.000 1.4778 0.05899 0.05326 -0.0390 0.0147 1.0000
16.250 1.4820 0.06146 0.05578 -0.0390 0.0143 1.0000
16.500 1.4876 0.06381 0.05820 -0.0391 0.0139 1.0000
16.750 1.4919 0.06637 0.06082 -0.0392 0.0135 1.0000
17.000 1.4964 0.06892 0.06344 -0.0394 0.0131 1.0000
17.250 1.4994 0.07172 0.06630 -0.0397 0.0126 1.0000
17.500 1.5022 0.07457 0.06920 -0.0401 0.0122 1.0000
17.750 1.5040 0.07759 0.07228 -0.0405 0.0119 1.0000
18.000 1.5044 0.08086 0.07561 -0.0411 0.0115 1.0000
18.250 1.5074 0.08379 0.07861 -0.0417 0.0113 1.0000
18.500 1.5091 0.08697 0.08187 -0.0424 0.0110 1.0000
18.750 1.5106 0.09018 0.08516 -0.0432 0.0108 1.0000
19.000 1.5115 0.09352 0.08858 -0.0440 0.0105 1.0000
19.250 1.5112 0.09708 0.09221 -0.0450 0.0102 1.0000
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