FX 77-W-270S (fx77w270s-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: FX 77-W-270S (fx77w270s-il) Reynolds number: 1,000,000 Max Cl/Cd: 106.51 at α=10.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx77w270s-il-1000000-n5.txt Download as CSV file: xf-fx77w270s-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: FX 77-W-270S
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
------ -------- --------- --------- -------- -------- --------
-19.750 -1.0104 0.09889 0.09298 -0.0370 0.4849 0.0046
-19.500 -1.0203 0.09376 0.08775 -0.0392 0.4823 0.0045
-19.250 -1.0287 0.08898 0.08285 -0.0412 0.4794 0.0045
-19.000 -1.0352 0.08456 0.07833 -0.0429 0.4763 0.0045
-18.750 -1.0394 0.08056 0.07422 -0.0443 0.4730 0.0045
-18.250 -1.0441 0.07323 0.06669 -0.0465 0.4675 0.0045
-18.000 -1.0441 0.06999 0.06338 -0.0474 0.4656 0.0045
-17.750 -1.0427 0.06699 0.06030 -0.0480 0.4636 0.0045
-17.500 -1.0411 0.06406 0.05729 -0.0486 0.4615 0.0046
-17.250 -1.0371 0.06148 0.05463 -0.0489 0.4593 0.0046
-17.000 -1.0328 0.05896 0.05204 -0.0492 0.4571 0.0046
-16.750 -1.0277 0.05661 0.04961 -0.0494 0.4549 0.0046
-16.500 -1.0212 0.05446 0.04738 -0.0495 0.4525 0.0046
-16.250 -1.0140 0.05242 0.04528 -0.0495 0.4501 0.0046
-16.000 -1.0061 0.05049 0.04328 -0.0495 0.4481 0.0046
-15.750 -0.9971 0.04869 0.04143 -0.0493 0.4472 0.0046
-15.500 -0.9886 0.04689 0.03958 -0.0491 0.4463 0.0046
-15.250 -0.9783 0.04530 0.03794 -0.0488 0.4452 0.0046
-15.000 -0.9673 0.04381 0.03640 -0.0486 0.4440 0.0046
-14.750 -0.9571 0.04226 0.03480 -0.0482 0.4426 0.0047
-14.500 -0.9452 0.04089 0.03339 -0.0478 0.4412 0.0047
-14.250 -0.9328 0.03962 0.03206 -0.0474 0.4397 0.0047
-14.000 -0.9208 0.03834 0.03074 -0.0469 0.4382 0.0047
-13.750 -0.9089 0.03709 0.02944 -0.0464 0.4368 0.0047
-13.500 -0.8952 0.03599 0.02829 -0.0459 0.4355 0.0047
-13.250 -0.8816 0.03490 0.02715 -0.0454 0.4341 0.0048
-13.000 -0.8682 0.03380 0.02601 -0.0448 0.4328 0.0048
-12.750 -0.8539 0.03278 0.02495 -0.0442 0.4313 0.0048
-12.500 -0.8388 0.03182 0.02395 -0.0437 0.4300 0.0048
-12.250 -0.8236 0.03087 0.02296 -0.0432 0.4286 0.0048
-12.000 -0.8084 0.02991 0.02197 -0.0426 0.4282 0.0049
-11.750 -0.7923 0.02902 0.02106 -0.0420 0.4278 0.0049
-11.500 -0.7762 0.02815 0.02015 -0.0415 0.4273 0.0049
-11.250 -0.7597 0.02727 0.01925 -0.0410 0.4267 0.0049
-11.000 -0.7426 0.02645 0.01840 -0.0404 0.4261 0.0050
-10.750 -0.7254 0.02563 0.01757 -0.0399 0.4255 0.0050
-10.500 -0.7079 0.02483 0.01674 -0.0395 0.4248 0.0051
-10.250 -0.6898 0.02407 0.01596 -0.0390 0.4241 0.0051
-10.000 -0.6715 0.02332 0.01518 -0.0386 0.4234 0.0051
-9.750 -0.6529 0.02258 0.01441 -0.0381 0.4227 0.0052
-9.500 -0.6341 0.02186 0.01366 -0.0378 0.4219 0.0052
-9.250 -0.6151 0.02115 0.01293 -0.0374 0.4211 0.0053
-9.000 -0.5960 0.02046 0.01222 -0.0370 0.4202 0.0053
-8.750 -0.5770 0.01979 0.01153 -0.0365 0.4193 0.0054
-8.500 -0.5583 0.01917 0.01088 -0.0359 0.4184 0.0054
-8.250 -0.5399 0.01861 0.01028 -0.0350 0.4174 0.0055
-8.000 -0.5218 0.01809 0.00974 -0.0340 0.4166 0.0056
-7.750 -0.5060 0.01763 0.00925 -0.0325 0.4158 0.0057
-7.500 -0.4955 0.01729 0.00889 -0.0298 0.4151 0.0057
-7.250 -0.4783 0.01699 0.00857 -0.0282 0.4142 0.0059
-7.000 -0.4574 0.01670 0.00827 -0.0272 0.4133 0.0061
-6.750 -0.4354 0.01644 0.00798 -0.0264 0.4123 0.0064
-6.500 -0.4128 0.01617 0.00771 -0.0257 0.4113 0.0069
-6.250 -0.3905 0.01587 0.00742 -0.0250 0.4103 0.0088
-6.000 -0.3664 0.01560 0.00718 -0.0245 0.4098 0.0156
-5.750 -0.3408 0.01538 0.00697 -0.0243 0.4095 0.0169
-5.500 -0.3147 0.01518 0.00678 -0.0242 0.4092 0.0183
-5.250 -0.2881 0.01498 0.00659 -0.0241 0.4088 0.0195
-5.000 -0.2612 0.01479 0.00641 -0.0242 0.4083 0.0211
-4.750 -0.2340 0.01460 0.00624 -0.0242 0.4078 0.0232
-4.500 -0.2065 0.01442 0.00607 -0.0243 0.4071 0.0257
-4.250 -0.1789 0.01423 0.00591 -0.0245 0.4065 0.0296
-4.000 -0.1515 0.01401 0.00574 -0.0246 0.4059 0.0373
-3.750 -0.1245 0.01375 0.00555 -0.0247 0.4053 0.0517
-3.500 -0.0969 0.01352 0.00540 -0.0249 0.4047 0.0674
-3.250 -0.0689 0.01331 0.00525 -0.0251 0.4040 0.0832
-3.000 -0.0411 0.01305 0.00510 -0.0254 0.4033 0.1045
-2.750 -0.0144 0.01267 0.00489 -0.0256 0.4026 0.1457
-2.500 0.0109 0.01208 0.00460 -0.0256 0.4017 0.2203
-2.250 0.0351 0.01126 0.00424 -0.0257 0.4009 0.3312
-2.000 0.0602 0.01043 0.00386 -0.0259 0.4001 0.4478
-1.750 0.0872 0.00985 0.00369 -0.0262 0.3994 0.5542
-1.500 0.1181 0.00989 0.00383 -0.0269 0.3986 0.5934
-1.250 0.1498 0.01006 0.00398 -0.0276 0.3978 0.6106
-1.000 0.1812 0.01022 0.00418 -0.0283 0.3970 0.6206
-0.750 0.2127 0.01038 0.00431 -0.0291 0.3960 0.6262
-0.500 0.2441 0.01051 0.00439 -0.0299 0.3949 0.6288
-0.250 0.2753 0.01062 0.00445 -0.0306 0.3936 0.6300
0.000 0.3064 0.01069 0.00449 -0.0314 0.3925 0.6312
0.250 0.3377 0.01069 0.00449 -0.0322 0.3922 0.6325
0.500 0.3691 0.01071 0.00450 -0.0331 0.3918 0.6337
0.750 0.4004 0.01075 0.00454 -0.0339 0.3914 0.6351
1.000 0.4316 0.01080 0.00459 -0.0347 0.3909 0.6365
1.250 0.4629 0.01084 0.00462 -0.0355 0.3903 0.6374
1.500 0.4942 0.01088 0.00465 -0.0364 0.3896 0.6381
1.750 0.5254 0.01092 0.00469 -0.0372 0.3888 0.6387
2.000 0.5565 0.01096 0.00472 -0.0381 0.3879 0.6393
2.250 0.5875 0.01101 0.00476 -0.0389 0.3871 0.6399
2.500 0.6185 0.01106 0.00481 -0.0397 0.3863 0.6405
2.750 0.6494 0.01112 0.00486 -0.0406 0.3855 0.6412
3.000 0.6803 0.01117 0.00491 -0.0414 0.3847 0.6420
3.250 0.7110 0.01124 0.00497 -0.0422 0.3838 0.6427
3.500 0.7416 0.01130 0.00502 -0.0430 0.3830 0.6434
3.750 0.7722 0.01136 0.00507 -0.0438 0.3820 0.6440
4.000 0.8026 0.01143 0.00513 -0.0446 0.3809 0.6445
4.250 0.8328 0.01150 0.00519 -0.0453 0.3798 0.6451
4.500 0.8627 0.01159 0.00526 -0.0461 0.3786 0.6456
4.750 0.8925 0.01169 0.00536 -0.0468 0.3774 0.6461
5.000 0.9220 0.01182 0.00548 -0.0474 0.3761 0.6466
5.250 0.9521 0.01189 0.00557 -0.0482 0.3757 0.6471
5.500 0.9821 0.01197 0.00566 -0.0490 0.3751 0.6476
5.750 1.0120 0.01205 0.00575 -0.0497 0.3744 0.6480
6.000 1.0418 0.01213 0.00586 -0.0504 0.3737 0.6484
6.250 1.0714 0.01222 0.00596 -0.0511 0.3728 0.6489
6.500 1.1009 0.01231 0.00607 -0.0518 0.3718 0.6494
6.750 1.1302 0.01240 0.00617 -0.0525 0.3706 0.6499
7.000 1.1593 0.01249 0.00628 -0.0532 0.3693 0.6502
7.250 1.1882 0.01259 0.00639 -0.0538 0.3681 0.6505
7.500 1.2167 0.01270 0.00651 -0.0544 0.3670 0.6508
7.750 1.2450 0.01280 0.00662 -0.0549 0.3658 0.6514
8.000 1.2728 0.01291 0.00674 -0.0553 0.3646 0.6522
8.250 1.3001 0.01304 0.00688 -0.0557 0.3633 0.6529
8.500 1.3268 0.01318 0.00704 -0.0560 0.3617 0.6537
8.750 1.3532 0.01335 0.00722 -0.0563 0.3603 0.6544
9.000 1.3807 0.01346 0.00738 -0.0567 0.3594 0.6551
9.250 1.4076 0.01359 0.00756 -0.0571 0.3584 0.6558
9.500 1.4342 0.01373 0.00773 -0.0573 0.3572 0.6565
9.750 1.4602 0.01388 0.00792 -0.0575 0.3557 0.6572
10.000 1.4854 0.01403 0.00811 -0.0576 0.3541 0.6579
10.250 1.5097 0.01420 0.00831 -0.0575 0.3523 0.6586
10.500 1.5326 0.01439 0.00852 -0.0572 0.3503 0.6593
10.750 1.5520 0.01462 0.00876 -0.0562 0.3482 0.6600
11.000 1.5665 0.01491 0.00907 -0.0544 0.3459 0.6607
11.250 1.5871 0.01518 0.00938 -0.0538 0.3440 0.6615
11.500 1.6085 0.01546 0.00971 -0.0533 0.3417 0.6624
11.750 1.6282 0.01580 0.01008 -0.0527 0.3381 0.6633
12.000 1.6446 0.01628 0.01057 -0.0517 0.3339 0.6641
12.250 1.6583 0.01690 0.01119 -0.0503 0.3301 0.6649
12.500 1.6774 0.01735 0.01169 -0.0499 0.3271 0.6657
12.750 1.6930 0.01797 0.01234 -0.0491 0.3227 0.6664
13.000 1.7024 0.01894 0.01331 -0.0476 0.3176 0.6670
13.250 1.7130 0.01994 0.01433 -0.0466 0.3127 0.6677
13.500 1.7229 0.02106 0.01549 -0.0456 0.3074 0.6683
13.750 1.7233 0.02290 0.01735 -0.0442 0.3018 0.6689
14.000 1.7293 0.02455 0.01904 -0.0435 0.2973 0.6695
14.250 1.7290 0.02682 0.02137 -0.0428 0.2918 0.6701
14.500 1.7140 0.03058 0.02518 -0.0418 0.2865 0.6705
14.750 1.7072 0.03373 0.02840 -0.0413 0.2824 0.6709
15.000 1.6811 0.03873 0.03349 -0.0404 0.2770 0.6713
15.250 1.6377 0.04535 0.04021 -0.0389 0.2731 0.6719
15.500 1.6037 0.05108 0.04604 -0.0378 0.2693 0.6726
15.750 1.5643 0.05749 0.05253 -0.0367 0.2637 0.6732
16.000 1.5153 0.06506 0.06017 -0.0356 0.2579 0.6737
16.250 1.5019 0.06910 0.06425 -0.0354 0.2529 0.6746
16.500 1.4689 0.07531 0.07049 -0.0350 0.2455 0.6752
16.750 1.4516 0.07991 0.07513 -0.0350 0.2400 0.6759
17.000 1.4280 0.08525 0.08046 -0.0349 0.2310 0.6766
17.250 1.4114 0.08994 0.08516 -0.0351 0.2232 0.6773
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