GOE 735 AIRFOIL (goe735-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 735 AIRFOIL (goe735-il) Reynolds number: 1,000,000 Max Cl/Cd: 97.29 at α=8.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe735-il-1000000-n5.txt Download as CSV file: xf-goe735-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: GOE 735 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 = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -0.9685 0.09799 0.09488 -0.0399 1.0000 0.0283
-19.500 -1.0758 0.07901 0.07557 -0.0514 1.0000 0.0280
-19.250 -1.1656 0.06273 0.05896 -0.0616 1.0000 0.0277
-18.750 -1.2271 0.04650 0.04234 -0.0728 0.9597 0.0281
-18.500 -1.1821 0.04106 0.03651 -0.0866 0.8691 0.0287
-18.250 -1.1936 0.03803 0.03322 -0.0866 0.8248 0.0288
-17.750 -1.2046 0.03316 0.02805 -0.0858 0.7900 0.0292
-17.500 -1.2045 0.03139 0.02616 -0.0850 0.7797 0.0297
-17.250 -1.2035 0.02979 0.02446 -0.0838 0.7700 0.0299
-17.000 -1.2003 0.02844 0.02301 -0.0824 0.7620 0.0301
-16.750 -1.1983 0.02708 0.02157 -0.0807 0.7541 0.0305
-16.500 -1.1953 0.02588 0.02028 -0.0788 0.7465 0.0309
-16.250 -1.1904 0.02481 0.01914 -0.0769 0.7404 0.0312
-16.000 -1.1838 0.02388 0.01814 -0.0749 0.7336 0.0316
-15.750 -1.1759 0.02305 0.01725 -0.0728 0.7268 0.0322
-15.500 -1.1665 0.02231 0.01645 -0.0707 0.7212 0.0326
-15.250 -1.1559 0.02164 0.01572 -0.0687 0.7157 0.0332
-15.000 -1.1441 0.02104 0.01506 -0.0666 0.7094 0.0337
-14.500 -1.1201 0.01988 0.01378 -0.0624 0.6985 0.0347
-14.250 -1.1072 0.01933 0.01319 -0.0602 0.6928 0.0354
-14.000 -1.0937 0.01882 0.01263 -0.0581 0.6868 0.0363
-13.750 -1.0786 0.01838 0.01214 -0.0561 0.6816 0.0371
-13.500 -1.0627 0.01796 0.01167 -0.0542 0.6766 0.0379
-13.250 -1.0468 0.01753 0.01120 -0.0522 0.6699 0.0387
-13.000 -1.0311 0.01710 0.01073 -0.0501 0.6638 0.0398
-12.750 -1.0142 0.01671 0.01031 -0.0482 0.6581 0.0409
-12.500 -0.9965 0.01635 0.00991 -0.0464 0.6518 0.0421
-12.250 -0.9791 0.01599 0.00951 -0.0445 0.6446 0.0435
-12.000 -0.9612 0.01564 0.00914 -0.0426 0.6381 0.0452
-11.750 -0.9424 0.01535 0.00881 -0.0408 0.6296 0.0468
-11.500 -0.9239 0.01507 0.00849 -0.0390 0.6215 0.0486
-11.250 -0.9042 0.01479 0.00819 -0.0374 0.6140 0.0505
-11.000 -0.8829 0.01456 0.00791 -0.0360 0.6048 0.0524
-10.750 -0.8610 0.01429 0.00762 -0.0348 0.5954 0.0543
-10.500 -0.8386 0.01406 0.00734 -0.0336 0.5844 0.0565
-10.250 -0.8152 0.01386 0.00710 -0.0326 0.5753 0.0583
-10.000 -0.7922 0.01364 0.00685 -0.0315 0.5656 0.0605
-9.750 -0.7684 0.01344 0.00662 -0.0306 0.5573 0.0627
-9.500 -0.7441 0.01329 0.00641 -0.0297 0.5469 0.0644
-9.250 -0.7200 0.01309 0.00619 -0.0288 0.5384 0.0661
-9.000 -0.6955 0.01292 0.00599 -0.0280 0.5298 0.0680
-8.750 -0.6705 0.01278 0.00580 -0.0272 0.5226 0.0696
-8.500 -0.6451 0.01264 0.00562 -0.0265 0.5159 0.0710
-8.250 -0.6202 0.01248 0.00544 -0.0257 0.5079 0.0726
-8.000 -0.5949 0.01233 0.00527 -0.0250 0.5013 0.0744
-7.750 -0.5691 0.01220 0.00511 -0.0244 0.4948 0.0762
-7.500 -0.5432 0.01209 0.00496 -0.0238 0.4886 0.0777
-7.250 -0.5172 0.01198 0.00480 -0.0232 0.4831 0.0789
-7.000 -0.4914 0.01183 0.00465 -0.0226 0.4775 0.0806
-6.750 -0.4654 0.01171 0.00451 -0.0220 0.4710 0.0823
-6.500 -0.4392 0.01162 0.00438 -0.0215 0.4649 0.0840
-6.250 -0.4124 0.01151 0.00426 -0.0210 0.4608 0.0856
-6.000 -0.3859 0.01141 0.00413 -0.0205 0.4560 0.0874
-5.750 -0.3596 0.01130 0.00402 -0.0200 0.4507 0.0900
-5.500 -0.3331 0.01121 0.00392 -0.0195 0.4455 0.0923
-5.250 -0.3061 0.01113 0.00381 -0.0191 0.4412 0.0941
-5.000 -0.2790 0.01106 0.00371 -0.0187 0.4361 0.0952
-4.750 -0.2525 0.01097 0.00360 -0.0182 0.4315 0.0974
-4.500 -0.2259 0.01089 0.00351 -0.0178 0.4270 0.0996
-4.250 -0.1988 0.01080 0.00343 -0.0174 0.4239 0.1016
-4.000 -0.1716 0.01074 0.00335 -0.0171 0.4197 0.1035
-3.750 -0.1444 0.01070 0.00327 -0.0167 0.4152 0.1051
-3.500 -0.1178 0.01064 0.00320 -0.0163 0.4104 0.1079
-3.250 -0.0907 0.01057 0.00314 -0.0159 0.4070 0.1107
-3.000 -0.0634 0.01051 0.00308 -0.0156 0.4039 0.1133
-2.750 -0.0360 0.01047 0.00303 -0.0153 0.4004 0.1156
-2.500 -0.0090 0.01042 0.00298 -0.0150 0.3967 0.1189
-2.250 0.0178 0.01038 0.00294 -0.0146 0.3926 0.1232
-2.000 0.0450 0.01035 0.00290 -0.0143 0.3891 0.1269
-1.750 0.0723 0.01031 0.00287 -0.0141 0.3859 0.1308
-1.500 0.0994 0.01026 0.00284 -0.0137 0.3824 0.1360
-1.250 0.1266 0.01025 0.00282 -0.0135 0.3790 0.1406
-1.000 0.1533 0.01022 0.00280 -0.0131 0.3755 0.1470
-0.750 0.1800 0.01021 0.00280 -0.0128 0.3721 0.1542
-0.500 0.2071 0.01016 0.00278 -0.0125 0.3699 0.1625
-0.250 0.2341 0.01013 0.00278 -0.0122 0.3671 0.1714
0.000 0.2605 0.01008 0.00277 -0.0118 0.3638 0.1841
0.250 0.2866 0.01005 0.00278 -0.0114 0.3600 0.2014
0.500 0.3120 0.01000 0.00280 -0.0109 0.3564 0.2257
0.750 0.3374 0.00992 0.00281 -0.0104 0.3539 0.2548
1.000 0.3633 0.00985 0.00283 -0.0099 0.3518 0.2834
1.250 0.3886 0.00976 0.00286 -0.0094 0.3493 0.3177
1.500 0.4138 0.00970 0.00289 -0.0088 0.3466 0.3502
1.750 0.4385 0.00964 0.00293 -0.0082 0.3437 0.3856
2.000 0.4623 0.00957 0.00297 -0.0074 0.3408 0.4286
2.250 0.4823 0.00937 0.00302 -0.0060 0.3374 0.5133
2.500 0.5040 0.00919 0.00306 -0.0047 0.3356 0.5823
2.750 0.5249 0.00905 0.00311 -0.0033 0.3334 0.6413
3.000 0.5407 0.00880 0.00316 -0.0008 0.3311 0.7304
3.250 0.5575 0.00864 0.00325 0.0016 0.3289 0.8060
3.500 0.5807 0.00861 0.00338 0.0026 0.3263 0.8579
3.750 0.6168 0.00870 0.00359 0.0010 0.3234 0.9041
4.000 0.6599 0.00889 0.00380 -0.0022 0.3204 0.9274
4.250 0.7028 0.00906 0.00398 -0.0054 0.3186 0.9379
4.500 0.7321 0.00921 0.00413 -0.0057 0.3163 0.9489
4.750 0.7738 0.00940 0.00430 -0.0087 0.3134 0.9517
5.000 0.8089 0.00960 0.00448 -0.0103 0.3107 0.9556
5.250 0.8339 0.00981 0.00467 -0.0098 0.3084 0.9626
5.500 0.8661 0.01004 0.00488 -0.0108 0.3056 0.9656
5.750 0.9002 0.01024 0.00507 -0.0123 0.3033 0.9669
6.000 0.9337 0.01040 0.00523 -0.0137 0.3014 0.9683
6.250 0.9660 0.01058 0.00540 -0.0148 0.2992 0.9701
6.500 0.9961 0.01076 0.00558 -0.0155 0.2966 0.9723
6.750 1.0224 0.01097 0.00577 -0.0156 0.2936 0.9751
7.000 1.0433 0.01122 0.00600 -0.0145 0.2906 0.9789
7.250 1.0748 0.01146 0.00623 -0.0157 0.2875 0.9798
7.500 1.1063 0.01163 0.00641 -0.0168 0.2857 0.9807
7.750 1.1369 0.01183 0.00662 -0.0178 0.2838 0.9819
8.000 1.1670 0.01205 0.00684 -0.0187 0.2817 0.9833
8.250 1.1957 0.01229 0.00709 -0.0194 0.2792 0.9851
8.500 1.2222 0.01257 0.00736 -0.0197 0.2767 0.9872
8.750 1.2433 0.01290 0.00767 -0.0191 0.2738 0.9902
9.000 1.2660 0.01318 0.00798 -0.0188 0.2718 0.9924
9.250 1.2944 0.01341 0.00822 -0.0196 0.2704 0.9938
9.500 1.3217 0.01368 0.00851 -0.0203 0.2686 0.9954
9.750 1.3483 0.01399 0.00886 -0.0210 0.2666 0.9972
10.000 1.3737 0.01439 0.00926 -0.0217 0.2641 0.9987
10.250 1.3988 0.01487 0.00975 -0.0225 0.2615 0.9998
10.500 1.4038 0.01548 0.01038 -0.0197 0.2592 1.0000
10.750 1.4074 0.01618 0.01109 -0.0168 0.2570 1.0000
11.000 1.4172 0.01673 0.01168 -0.0148 0.2555 1.0000
11.250 1.4273 0.01733 0.01232 -0.0130 0.2539 1.0000
11.500 1.4375 0.01799 0.01301 -0.0113 0.2520 1.0000
11.750 1.4471 0.01873 0.01377 -0.0096 0.2499 1.0000
12.000 1.4559 0.01957 0.01463 -0.0080 0.2477 1.0000
12.250 1.4636 0.02053 0.01560 -0.0065 0.2453 1.0000
12.500 1.4703 0.02160 0.01669 -0.0049 0.2428 1.0000
12.750 1.4808 0.02248 0.01761 -0.0038 0.2411 1.0000
13.000 1.4918 0.02337 0.01853 -0.0028 0.2388 1.0000
13.250 1.4999 0.02446 0.01965 -0.0016 0.2349 1.0000
13.500 1.5039 0.02589 0.02108 -0.0004 0.2311 1.0000
13.750 1.5061 0.02749 0.02269 0.0009 0.2276 1.0000
14.000 1.5150 0.02865 0.02389 0.0017 0.2241 1.0000
14.250 1.5169 0.03038 0.02563 0.0027 0.2188 1.0000
14.500 1.5161 0.03242 0.02769 0.0037 0.2148 1.0000
14.750 1.5204 0.03412 0.02942 0.0043 0.2105 1.0000
15.000 1.5236 0.03598 0.03132 0.0049 0.2071 1.0000
15.250 1.5195 0.03855 0.03390 0.0055 0.2021 1.0000
15.500 1.5190 0.04086 0.03624 0.0059 0.1988 1.0000
15.750 1.5181 0.04324 0.03865 0.0063 0.1936 1.0000
16.000 1.5134 0.04605 0.04149 0.0066 0.1899 1.0000
16.250 1.5040 0.04939 0.04485 0.0068 0.1850 1.0000
16.500 1.5035 0.05188 0.04739 0.0069 0.1821 1.0000
16.750 1.4968 0.05503 0.05057 0.0070 0.1777 1.0000
17.000 1.4833 0.05897 0.05454 0.0069 0.1735 1.0000
17.250 1.4814 0.06175 0.05737 0.0068 0.1710 1.0000
17.500 1.4738 0.06515 0.06081 0.0066 0.1661 1.0000
17.750 1.4588 0.06946 0.06515 0.0062 0.1620 1.0000
18.000 1.4541 0.07266 0.06840 0.0059 0.1598 1.0000
18.250 1.4510 0.07572 0.07150 0.0055 0.1565 1.0000
18.500 1.4362 0.08019 0.07600 0.0048 0.1517 1.0000
18.750 1.4283 0.08387 0.07971 0.0042 0.1488 1.0000
19.000 1.4250 0.08707 0.08298 0.0036 0.1468 1.0000
19.250 1.4205 0.09044 0.08638 0.0029 0.1427 1.0000
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