GOE 777 AIRFOIL (goe777-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: GOE 777 AIRFOIL (goe777-il) Reynolds number: 1,000,000 Max Cl/Cd: 109.02 at α=6° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-goe777-il-1000000.txt Download as CSV file: xf-goe777-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: GOE 777 AIRFOIL
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 -1.0143 0.08039 0.07688 -0.0642 1.0000 0.0261
-19.500 -1.0290 0.07477 0.07118 -0.0675 1.0000 0.0263
-19.250 -1.0417 0.06945 0.06577 -0.0706 1.0000 0.0265
-19.000 -1.0528 0.06441 0.06064 -0.0735 1.0000 0.0266
-18.750 -1.0610 0.05979 0.05594 -0.0762 1.0000 0.0268
-18.500 -1.0673 0.05556 0.05163 -0.0786 1.0000 0.0269
-18.250 -1.0715 0.05174 0.04774 -0.0806 1.0000 0.0271
-18.000 -1.0735 0.04834 0.04426 -0.0823 1.0000 0.0273
-17.750 -1.0740 0.04522 0.04107 -0.0838 1.0000 0.0276
-17.500 -1.0726 0.04242 0.03820 -0.0849 1.0000 0.0278
-17.250 -1.0730 0.04021 0.03565 -0.0849 0.8664 0.0280
-17.000 -1.0701 0.03818 0.03325 -0.0850 0.7859 0.0283
-16.750 -1.0640 0.03620 0.03103 -0.0855 0.7456 0.0285
-16.500 -1.0562 0.03436 0.02901 -0.0859 0.7182 0.0287
-16.250 -1.0469 0.03269 0.02718 -0.0862 0.6961 0.0289
-16.000 -1.0360 0.03121 0.02555 -0.0863 0.6757 0.0291
-15.750 -1.0294 0.02942 0.02363 -0.0863 0.6570 0.0294
-15.500 -1.0254 0.02753 0.02162 -0.0860 0.6394 0.0297
-15.250 -1.0166 0.02612 0.02011 -0.0856 0.6218 0.0301
-14.750 -0.9915 0.02404 0.01784 -0.0842 0.5935 0.0307
-14.500 -0.9771 0.02320 0.01690 -0.0833 0.5824 0.0310
-14.250 -0.9619 0.02243 0.01606 -0.0824 0.5753 0.0314
-14.000 -0.9457 0.02175 0.01530 -0.0813 0.5681 0.0318
-13.750 -0.9285 0.02116 0.01463 -0.0802 0.5613 0.0322
-13.500 -0.9099 0.02062 0.01403 -0.0791 0.5574 0.0326
-13.250 -0.8904 0.02017 0.01351 -0.0780 0.5533 0.0329
-13.000 -0.8802 0.01940 0.01268 -0.0757 0.5497 0.0335
-12.750 -0.8657 0.01885 0.01209 -0.0738 0.5458 0.0340
-12.500 -0.8461 0.01840 0.01159 -0.0726 0.5414 0.0345
-12.250 -0.8249 0.01798 0.01114 -0.0716 0.5396 0.0350
-12.000 -0.8028 0.01758 0.01071 -0.0707 0.5377 0.0355
-11.750 -0.7800 0.01721 0.01030 -0.0698 0.5357 0.0361
-11.500 -0.7563 0.01689 0.00993 -0.0690 0.5334 0.0366
-11.250 -0.7336 0.01649 0.00949 -0.0681 0.5312 0.0373
-11.000 -0.7116 0.01603 0.00901 -0.0672 0.5291 0.0382
-10.750 -0.6877 0.01571 0.00866 -0.0664 0.5268 0.0390
-10.500 -0.6630 0.01543 0.00834 -0.0658 0.5242 0.0398
-10.250 -0.6380 0.01519 0.00805 -0.0652 0.5214 0.0406
-10.000 -0.6128 0.01491 0.00774 -0.0646 0.5200 0.0414
-9.750 -0.5884 0.01454 0.00737 -0.0639 0.5191 0.0427
-9.500 -0.5626 0.01426 0.00710 -0.0634 0.5179 0.0440
-9.250 -0.5361 0.01404 0.00685 -0.0629 0.5165 0.0454
-9.000 -0.5104 0.01375 0.00657 -0.0624 0.5150 0.0472
-8.750 -0.4839 0.01352 0.00634 -0.0620 0.5136 0.0491
-8.500 -0.4571 0.01331 0.00612 -0.0616 0.5123 0.0513
-8.250 -0.4302 0.01311 0.00594 -0.0613 0.5109 0.0541
-8.000 -0.4029 0.01295 0.00577 -0.0610 0.5095 0.0570
-7.750 -0.3751 0.01283 0.00566 -0.0607 0.5081 0.0603
-7.500 -0.3474 0.01271 0.00554 -0.0605 0.5062 0.0633
-7.250 -0.3193 0.01266 0.00547 -0.0604 0.5037 0.0662
-7.000 -0.2916 0.01263 0.00540 -0.0601 0.5007 0.0687
-6.750 -0.2635 0.01249 0.00529 -0.0600 0.4998 0.0711
-6.500 -0.2347 0.01240 0.00519 -0.0599 0.4989 0.0734
-6.250 -0.2063 0.01226 0.00505 -0.0598 0.4976 0.0753
-6.000 -0.1785 0.01209 0.00489 -0.0597 0.4960 0.0777
-5.750 -0.1499 0.01199 0.00480 -0.0596 0.4946 0.0798
-5.500 -0.1211 0.01193 0.00471 -0.0596 0.4933 0.0815
-5.250 -0.0934 0.01175 0.00453 -0.0594 0.4920 0.0837
-5.000 -0.0653 0.01161 0.00440 -0.0593 0.4903 0.0857
-4.750 -0.0369 0.01150 0.00428 -0.0592 0.4883 0.0877
-4.500 -0.0083 0.01144 0.00418 -0.0592 0.4861 0.0894
-4.250 0.0195 0.01135 0.00407 -0.0590 0.4839 0.0918
-4.000 0.0474 0.01130 0.00402 -0.0589 0.4816 0.0943
-3.750 0.0760 0.01121 0.00393 -0.0589 0.4806 0.0966
-3.500 0.1051 0.01113 0.00385 -0.0590 0.4798 0.0988
-3.250 0.1334 0.01097 0.00373 -0.0589 0.4788 0.1037
-3.000 0.1621 0.01086 0.00364 -0.0590 0.4776 0.1081
-2.750 0.1905 0.01072 0.00354 -0.0590 0.4761 0.1151
-2.500 0.2187 0.01055 0.00344 -0.0589 0.4744 0.1295
-2.250 0.2430 0.01002 0.00326 -0.0584 0.4728 0.2199
-2.000 0.2688 0.00964 0.00317 -0.0581 0.4712 0.2988
-1.750 0.2963 0.00944 0.00311 -0.0580 0.4696 0.3439
-1.500 0.3239 0.00928 0.00307 -0.0580 0.4678 0.3850
-1.250 0.3509 0.00910 0.00304 -0.0578 0.4656 0.4334
-1.000 0.3764 0.00889 0.00308 -0.0574 0.4630 0.5170
-0.750 0.4042 0.00876 0.00311 -0.0574 0.4617 0.5703
-0.500 0.4333 0.00871 0.00312 -0.0575 0.4604 0.5962
-0.250 0.4625 0.00866 0.00314 -0.0576 0.4587 0.6137
0.000 0.4918 0.00864 0.00314 -0.0578 0.4566 0.6274
0.250 0.5212 0.00862 0.00314 -0.0581 0.4543 0.6400
0.500 0.5504 0.00861 0.00314 -0.0582 0.4517 0.6508
0.750 0.5793 0.00863 0.00315 -0.0584 0.4489 0.6622
1.000 0.6078 0.00869 0.00320 -0.0585 0.4454 0.6728
1.250 0.6371 0.00868 0.00323 -0.0588 0.4433 0.6828
1.500 0.6668 0.00868 0.00325 -0.0591 0.4408 0.6915
1.750 0.6958 0.00865 0.00327 -0.0593 0.4376 0.7026
2.250 0.7525 0.00869 0.00333 -0.0595 0.4296 0.7289
2.500 0.7810 0.00870 0.00338 -0.0597 0.4257 0.7439
2.750 0.8093 0.00868 0.00343 -0.0598 0.4208 0.7639
3.000 0.8366 0.00870 0.00349 -0.0597 0.4146 0.7866
3.250 0.8636 0.00873 0.00358 -0.0596 0.4081 0.8099
3.500 0.8899 0.00878 0.00367 -0.0594 0.3993 0.8372
3.750 0.9153 0.00886 0.00380 -0.0590 0.3899 0.8678
4.000 0.9389 0.00901 0.00397 -0.0582 0.3789 0.9017
4.250 0.9659 0.00918 0.00418 -0.0581 0.3688 0.9370
4.500 0.9989 0.00947 0.00443 -0.0594 0.3593 0.9614
4.750 1.0334 0.00978 0.00469 -0.0612 0.3511 0.9753
5.000 1.0685 0.01006 0.00493 -0.0631 0.3448 0.9841
5.250 1.1038 0.01032 0.00515 -0.0650 0.3400 0.9907
5.500 1.1406 0.01063 0.00541 -0.0673 0.3351 0.9943
5.750 1.1775 0.01093 0.00568 -0.0697 0.3307 0.9977
6.000 1.2134 0.01113 0.00588 -0.0718 0.3282 1.0000
6.250 1.2303 0.01131 0.00605 -0.0700 0.3258 1.0000
6.500 1.2468 0.01152 0.00625 -0.0681 0.3234 1.0000
6.750 1.2627 0.01176 0.00648 -0.0662 0.3210 1.0000
7.000 1.2770 0.01204 0.00675 -0.0640 0.3183 1.0000
7.250 1.2898 0.01238 0.00707 -0.0615 0.3155 1.0000
7.500 1.3074 0.01257 0.00728 -0.0599 0.3145 1.0000
7.750 1.3253 0.01278 0.00752 -0.0585 0.3132 1.0000
8.000 1.3439 0.01304 0.00779 -0.0573 0.3119 1.0000
8.250 1.3628 0.01333 0.00810 -0.0562 0.3103 1.0000
8.500 1.3812 0.01368 0.00847 -0.0551 0.3086 1.0000
8.750 1.3989 0.01409 0.00888 -0.0541 0.3069 1.0000
9.000 1.4156 0.01457 0.00938 -0.0530 0.3051 1.0000
9.250 1.4312 0.01515 0.00996 -0.0519 0.3033 1.0000
9.500 1.4450 0.01585 0.01066 -0.0506 0.3009 1.0000
9.750 1.4620 0.01645 0.01129 -0.0499 0.2994 1.0000
10.000 1.4818 0.01693 0.01181 -0.0496 0.2983 1.0000
10.250 1.5006 0.01749 0.01242 -0.0492 0.2971 1.0000
10.500 1.5187 0.01812 0.01309 -0.0489 0.2957 1.0000
10.750 1.5358 0.01884 0.01384 -0.0485 0.2944 1.0000
11.000 1.5520 0.01964 0.01468 -0.0481 0.2928 1.0000
11.250 1.5667 0.02058 0.01564 -0.0477 0.2911 1.0000
11.500 1.5792 0.02171 0.01680 -0.0473 0.2892 1.0000
11.750 1.5889 0.02305 0.01814 -0.0466 0.2868 1.0000
12.000 1.5986 0.02437 0.01947 -0.0460 0.2842 1.0000
12.250 1.6140 0.02541 0.02058 -0.0460 0.2832 1.0000
12.500 1.6285 0.02651 0.02174 -0.0459 0.2818 1.0000
12.750 1.6414 0.02771 0.02300 -0.0458 0.2804 1.0000
13.000 1.6529 0.02904 0.02437 -0.0455 0.2788 1.0000
13.250 1.6636 0.03041 0.02578 -0.0453 0.2771 1.0000
13.500 1.6714 0.03204 0.02746 -0.0450 0.2754 1.0000
13.750 1.6772 0.03381 0.02925 -0.0445 0.2735 1.0000
14.000 1.6824 0.03557 0.03103 -0.0440 0.2715 1.0000
14.250 1.6898 0.03711 0.03258 -0.0435 0.2692 1.0000
14.500 1.6988 0.03877 0.03432 -0.0434 0.2681 1.0000
14.750 1.7064 0.04057 0.03619 -0.0434 0.2665 1.0000
15.000 1.7140 0.04233 0.03802 -0.0433 0.2645 1.0000
15.250 1.7194 0.04433 0.04007 -0.0432 0.2623 1.0000
15.500 1.7239 0.04639 0.04216 -0.0431 0.2600 1.0000
15.750 1.7231 0.04894 0.04472 -0.0428 0.2570 1.0000
16.000 1.7280 0.05088 0.04668 -0.0426 0.2543 1.0000
16.250 1.7329 0.05302 0.04891 -0.0426 0.2524 1.0000
16.500 1.7387 0.05503 0.05099 -0.0427 0.2500 1.0000
16.750 1.7432 0.05715 0.05315 -0.0427 0.2472 1.0000
17.000 1.7403 0.06001 0.05603 -0.0426 0.2440 1.0000
17.250 1.7401 0.06253 0.05856 -0.0424 0.2406 1.0000
17.500 1.7444 0.06475 0.06087 -0.0426 0.2381 1.0000
17.750 1.7466 0.06716 0.06333 -0.0427 0.2344 1.0000
18.000 1.7449 0.06996 0.06613 -0.0427 0.2301 1.0000
18.250 1.7388 0.07323 0.06945 -0.0427 0.2262 1.0000
18.500 1.7419 0.07554 0.07182 -0.0429 0.2217 1.0000
18.750 1.7315 0.07935 0.07564 -0.0430 0.2159 1.0000
19.000 1.7271 0.08253 0.07884 -0.0432 0.2099 1.0000
19.250 1.7103 0.08710 0.08342 -0.0433 0.2022 1.0000
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