FX 84-W-175 (fx84w175-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: FX 84-W-175 (fx84w175-il) Reynolds number: 1,000,000 Max Cl/Cd: 123.97 at α=6° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx84w175-il-1000000-n5.txt Download as CSV file: xf-fx84w175-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: FX 84-W-175
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
------ -------- --------- --------- -------- -------- --------
-18.500 -0.7410 0.08784 0.08486 -0.0949 0.9353 0.0160
-18.250 -0.7943 0.07571 0.07249 -0.1028 0.9223 0.0159
-18.000 -0.8467 0.06449 0.06101 -0.1096 0.9091 0.0159
-17.750 -0.8860 0.05553 0.05183 -0.1151 0.8968 0.0158
-17.500 -0.9083 0.04935 0.04546 -0.1187 0.8867 0.0159
-17.250 -0.9246 0.04443 0.04036 -0.1213 0.8768 0.0159
-17.000 -0.9345 0.04057 0.03637 -0.1232 0.8681 0.0160
-16.500 -0.9453 0.03467 0.03021 -0.1250 0.8528 0.0163
-16.250 -0.9472 0.03237 0.02779 -0.1252 0.8451 0.0164
-16.000 -0.9458 0.03048 0.02579 -0.1251 0.8388 0.0165
-15.750 -0.9434 0.02876 0.02397 -0.1248 0.8322 0.0167
-15.500 -0.9386 0.02735 0.02245 -0.1242 0.8261 0.0168
-15.250 -0.9330 0.02604 0.02105 -0.1234 0.8208 0.0169
-15.000 -0.9274 0.02479 0.01972 -0.1225 0.8148 0.0171
-14.750 -0.9225 0.02360 0.01844 -0.1212 0.8088 0.0174
-14.500 -0.9152 0.02258 0.01735 -0.1199 0.8039 0.0176
-14.250 -0.9057 0.02171 0.01643 -0.1187 0.7990 0.0180
-14.000 -0.8954 0.02095 0.01560 -0.1173 0.7937 0.0182
-13.500 -0.8727 0.01961 0.01413 -0.1142 0.7842 0.0188
-13.250 -0.8611 0.01900 0.01346 -0.1125 0.7794 0.0190
-13.000 -0.8491 0.01849 0.01288 -0.1106 0.7745 0.0193
-12.750 -0.8365 0.01806 0.01238 -0.1086 0.7700 0.0195
-12.500 -0.8196 0.01762 0.01188 -0.1073 0.7660 0.0198
-12.250 -0.8005 0.01720 0.01140 -0.1063 0.7616 0.0201
-12.000 -0.7819 0.01673 0.01086 -0.1053 0.7573 0.0204
-11.750 -0.7622 0.01628 0.01037 -0.1044 0.7531 0.0209
-11.500 -0.7408 0.01588 0.00993 -0.1037 0.7494 0.0213
-11.250 -0.7188 0.01550 0.00952 -0.1031 0.7455 0.0218
-11.000 -0.6961 0.01515 0.00912 -0.1026 0.7415 0.0223
-10.750 -0.6729 0.01484 0.00875 -0.1021 0.7375 0.0229
-10.500 -0.6490 0.01452 0.00839 -0.1017 0.7339 0.0234
-10.250 -0.6251 0.01419 0.00802 -0.1013 0.7300 0.0239
-10.000 -0.6011 0.01384 0.00764 -0.1009 0.7260 0.0245
-9.750 -0.5766 0.01354 0.00731 -0.1006 0.7222 0.0253
-9.500 -0.5518 0.01327 0.00700 -0.1003 0.7185 0.0260
-9.250 -0.5262 0.01300 0.00669 -0.1001 0.7149 0.0267
-9.000 -0.5004 0.01275 0.00641 -0.0999 0.7109 0.0273
-8.750 -0.4748 0.01248 0.00611 -0.0997 0.7070 0.0283
-8.500 -0.4491 0.01223 0.00584 -0.0996 0.7031 0.0293
-8.250 -0.4228 0.01200 0.00558 -0.0995 0.6996 0.0304
-8.000 -0.3961 0.01179 0.00534 -0.0994 0.6958 0.0314
-7.750 -0.3696 0.01157 0.00510 -0.0993 0.6918 0.0324
-7.500 -0.3432 0.01135 0.00486 -0.0992 0.6878 0.0338
-7.250 -0.3164 0.01116 0.00465 -0.0992 0.6840 0.0352
-7.000 -0.2890 0.01099 0.00445 -0.0993 0.6805 0.0366
-6.750 -0.2620 0.01077 0.00424 -0.0993 0.6768 0.0386
-6.500 -0.2348 0.01060 0.00405 -0.0993 0.6726 0.0405
-6.250 -0.2075 0.01046 0.00388 -0.0993 0.6687 0.0423
-6.000 -0.1800 0.01028 0.00370 -0.0993 0.6653 0.0448
-5.750 -0.1522 0.01013 0.00355 -0.0995 0.6617 0.0475
-5.500 -0.1247 0.00997 0.00339 -0.0995 0.6577 0.0507
-5.250 -0.0970 0.00985 0.00325 -0.0996 0.6535 0.0538
-5.000 -0.0694 0.00971 0.00311 -0.0997 0.6498 0.0574
-4.750 -0.0412 0.00958 0.00299 -0.0999 0.6464 0.0616
-4.500 -0.0133 0.00944 0.00287 -0.1000 0.6424 0.0666
-4.250 0.0146 0.00934 0.00275 -0.1001 0.6382 0.0712
-3.750 0.0706 0.00911 0.00255 -0.1004 0.6308 0.0841
-3.500 0.0989 0.00901 0.00246 -0.1006 0.6268 0.0909
-3.250 0.1268 0.00890 0.00238 -0.1007 0.6226 0.1002
-3.000 0.1546 0.00881 0.00230 -0.1008 0.6183 0.1097
-2.750 0.1829 0.00871 0.00223 -0.1010 0.6148 0.1205
-2.500 0.2111 0.00860 0.00217 -0.1013 0.6108 0.1342
-2.250 0.2391 0.00850 0.00211 -0.1014 0.6065 0.1502
-2.000 0.2669 0.00841 0.00206 -0.1016 0.6022 0.1681
-1.750 0.2949 0.00831 0.00201 -0.1017 0.5986 0.1897
-1.500 0.3231 0.00820 0.00197 -0.1020 0.5947 0.2143
-1.250 0.3509 0.00807 0.00194 -0.1022 0.5901 0.2452
-1.000 0.3785 0.00796 0.00191 -0.1023 0.5860 0.2792
-0.750 0.4062 0.00782 0.00189 -0.1025 0.5823 0.3217
-0.500 0.4340 0.00765 0.00187 -0.1027 0.5783 0.3708
-0.250 0.4615 0.00748 0.00186 -0.1029 0.5737 0.4297
0.000 0.4888 0.00733 0.00186 -0.1030 0.5695 0.4880
0.250 0.5163 0.00722 0.00189 -0.1032 0.5656 0.5394
0.500 0.5445 0.00714 0.00192 -0.1034 0.5615 0.5801
0.750 0.5723 0.00711 0.00196 -0.1035 0.5568 0.6112
1.000 0.5998 0.00712 0.00201 -0.1035 0.5523 0.6398
1.250 0.6277 0.00713 0.00207 -0.1037 0.5483 0.6622
1.500 0.6558 0.00714 0.00213 -0.1038 0.5438 0.6805
1.750 0.6833 0.00719 0.00220 -0.1039 0.5389 0.6975
2.000 0.7102 0.00726 0.00228 -0.1038 0.5342 0.7140
2.250 0.7380 0.00729 0.00235 -0.1039 0.5301 0.7328
2.500 0.7654 0.00735 0.00244 -0.1039 0.5252 0.7491
2.750 0.7919 0.00742 0.00253 -0.1038 0.5201 0.7599
3.250 0.8460 0.00758 0.00270 -0.1037 0.5109 0.7751
3.500 0.8725 0.00768 0.00280 -0.1036 0.5056 0.7826
3.750 0.8980 0.00780 0.00291 -0.1033 0.5007 0.7891
4.000 0.9247 0.00787 0.00301 -0.1032 0.4963 0.7958
4.250 0.9507 0.00798 0.00312 -0.1030 0.4909 0.8025
4.500 0.9750 0.00812 0.00325 -0.1025 0.4852 0.8085
4.750 1.0003 0.00822 0.00337 -0.1022 0.4797 0.8151
5.000 1.0244 0.00836 0.00350 -0.1017 0.4727 0.8216
5.250 1.0470 0.00852 0.00366 -0.1009 0.4663 0.8278
5.500 1.0705 0.00865 0.00380 -0.1002 0.4597 0.8345
5.750 1.0910 0.00883 0.00397 -0.0990 0.4528 0.8413
6.000 1.1108 0.00896 0.00413 -0.0976 0.4469 0.8481
6.250 1.1292 0.00913 0.00432 -0.0960 0.4400 0.8559
6.500 1.1460 0.00936 0.00455 -0.0942 0.4337 0.8638
6.750 1.1649 0.00955 0.00477 -0.0927 0.4269 0.8724
7.000 1.1801 0.00984 0.00506 -0.0906 0.4193 0.8816
7.250 1.1982 0.01006 0.00531 -0.0891 0.4125 0.8919
7.500 1.2117 0.01039 0.00565 -0.0868 0.4037 0.9041
7.750 1.2259 0.01070 0.00599 -0.0847 0.3940 0.9195
8.000 1.2358 0.01113 0.00643 -0.0819 0.3804 0.9468
8.250 1.2540 0.01176 0.00700 -0.0812 0.3600 1.0000
8.500 1.2642 0.01246 0.00762 -0.0790 0.3427 1.0000
8.750 1.2749 0.01318 0.00827 -0.0769 0.3268 1.0000
9.000 1.2860 0.01391 0.00894 -0.0749 0.3124 1.0000
9.250 1.2952 0.01475 0.00972 -0.0727 0.2968 1.0000
9.500 1.3031 0.01569 0.01059 -0.0705 0.2802 1.0000
9.750 1.3102 0.01672 0.01153 -0.0683 0.2631 1.0000
10.000 1.3167 0.01781 0.01255 -0.0661 0.2465 1.0000
10.250 1.3206 0.01908 0.01374 -0.0637 0.2287 1.0000
10.500 1.3245 0.02042 0.01499 -0.0614 0.2110 1.0000
10.750 1.3292 0.02174 0.01624 -0.0593 0.1948 1.0000
11.000 1.3349 0.02308 0.01752 -0.0575 0.1812 1.0000
11.250 1.3373 0.02467 0.01903 -0.0554 0.1640 1.0000
11.500 1.3433 0.02609 0.02041 -0.0538 0.1522 1.0000
11.750 1.3467 0.02773 0.02199 -0.0521 0.1375 1.0000
12.000 1.3465 0.02970 0.02387 -0.0502 0.1200 1.0000
12.250 1.3516 0.03136 0.02549 -0.0488 0.1098 1.0000
12.500 1.3554 0.03316 0.02725 -0.0474 0.0985 1.0000
12.750 1.3599 0.03496 0.02902 -0.0463 0.0901 1.0000
13.000 1.3653 0.03673 0.03078 -0.0452 0.0820 1.0000
13.250 1.3709 0.03855 0.03258 -0.0442 0.0747 1.0000
13.500 1.3755 0.04050 0.03451 -0.0433 0.0681 1.0000
13.750 1.3822 0.04229 0.03631 -0.0425 0.0631 1.0000
14.000 1.3876 0.04426 0.03828 -0.0418 0.0580 1.0000
14.250 1.3927 0.04627 0.04029 -0.0412 0.0532 1.0000
14.500 1.3989 0.04824 0.04227 -0.0406 0.0496 1.0000
14.750 1.4045 0.05031 0.04434 -0.0401 0.0459 1.0000
15.000 1.4102 0.05239 0.04645 -0.0397 0.0429 1.0000
15.250 1.4158 0.05451 0.04859 -0.0393 0.0404 1.0000
15.500 1.4217 0.05666 0.05077 -0.0391 0.0380 1.0000
15.750 1.4274 0.05883 0.05297 -0.0388 0.0359 1.0000
16.000 1.4319 0.06122 0.05539 -0.0387 0.0335 1.0000
16.250 1.4373 0.06349 0.05769 -0.0386 0.0316 1.0000
16.500 1.4409 0.06603 0.06026 -0.0386 0.0299 1.0000
16.750 1.4469 0.06831 0.06258 -0.0386 0.0286 1.0000
17.000 1.4504 0.07095 0.06526 -0.0387 0.0271 1.0000
17.250 1.4544 0.07353 0.06788 -0.0389 0.0258 1.0000
17.500 1.4584 0.07617 0.07056 -0.0391 0.0247 1.0000
17.750 1.4624 0.07880 0.07324 -0.0394 0.0234 1.0000
18.000 1.4639 0.08182 0.07630 -0.0398 0.0224 1.0000
18.250 1.4683 0.08448 0.07901 -0.0402 0.0216 1.0000
18.500 1.4704 0.08749 0.08207 -0.0407 0.0205 1.0000
18.750 1.4736 0.09036 0.08499 -0.0413 0.0198 1.0000
19.000 1.4737 0.09368 0.08836 -0.0420 0.0189 1.0000
19.250 1.4769 0.09659 0.09133 -0.0427 0.0183 1.0000
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