GOE 735 AIRFOIL (goe735-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 735 AIRFOIL (goe735-il) Reynolds number: 500,000 Max Cl/Cd: 78.9 at α=8.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe735-il-500000-n5.txt Download as CSV file: xf-goe735-il-500000-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 = 0.500 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-18.500 -0.9384 0.08211 0.07822 -0.0509 1.0000 0.0357
-18.250 -0.9824 0.07230 0.06824 -0.0569 1.0000 0.0359
-18.000 -1.0217 0.06319 0.05895 -0.0626 1.0000 0.0359
-17.750 -1.0520 0.05538 0.05096 -0.0677 1.0000 0.0362
-17.500 -1.0764 0.04943 0.04487 -0.0703 0.9868 0.0363
-17.250 -1.0473 0.04361 0.03874 -0.0823 0.8921 0.0371
-17.000 -1.0536 0.04030 0.03512 -0.0836 0.8444 0.0375
-16.750 -1.0605 0.03757 0.03219 -0.0837 0.8233 0.0379
-16.500 -1.0648 0.03523 0.02969 -0.0833 0.8084 0.0383
-16.250 -1.0704 0.03300 0.02734 -0.0824 0.7963 0.0387
-16.000 -1.0725 0.03121 0.02543 -0.0812 0.7858 0.0392
-15.750 -1.0717 0.02969 0.02381 -0.0797 0.7773 0.0397
-15.500 -1.0689 0.02840 0.02242 -0.0780 0.7683 0.0404
-15.250 -1.0640 0.02728 0.02120 -0.0763 0.7610 0.0411
-15.000 -1.0576 0.02628 0.02011 -0.0744 0.7535 0.0419
-14.750 -1.0497 0.02541 0.01913 -0.0724 0.7463 0.0425
-14.500 -1.0426 0.02451 0.01817 -0.0703 0.7400 0.0433
-14.250 -1.0339 0.02371 0.01731 -0.0682 0.7331 0.0441
-14.000 -1.0236 0.02301 0.01654 -0.0661 0.7268 0.0452
-13.750 -1.0115 0.02239 0.01585 -0.0641 0.7208 0.0463
-13.500 -0.9983 0.02181 0.01520 -0.0621 0.7146 0.0476
-13.250 -0.9859 0.02122 0.01456 -0.0600 0.7084 0.0486
-13.000 -0.9719 0.02071 0.01399 -0.0580 0.7023 0.0501
-12.750 -0.9564 0.02022 0.01345 -0.0561 0.6967 0.0516
-12.500 -0.9405 0.01977 0.01294 -0.0542 0.6903 0.0530
-12.250 -0.9246 0.01933 0.01246 -0.0523 0.6840 0.0546
-12.000 -0.9073 0.01893 0.01201 -0.0505 0.6778 0.0563
-11.750 -0.8891 0.01856 0.01158 -0.0488 0.6707 0.0580
-11.500 -0.8715 0.01820 0.01117 -0.0470 0.6642 0.0597
-11.250 -0.8528 0.01787 0.01081 -0.0453 0.6578 0.0616
-11.000 -0.8334 0.01759 0.01047 -0.0437 0.6497 0.0636
-10.750 -0.8145 0.01732 0.01013 -0.0420 0.6423 0.0652
-10.500 -0.7946 0.01705 0.00984 -0.0405 0.6348 0.0670
-10.250 -0.7736 0.01680 0.00954 -0.0391 0.6265 0.0688
-10.000 -0.7513 0.01657 0.00923 -0.0380 0.6185 0.0706
-9.750 -0.7293 0.01630 0.00892 -0.0368 0.6087 0.0721
-9.500 -0.7068 0.01607 0.00864 -0.0357 0.5999 0.0738
-9.250 -0.6835 0.01586 0.00838 -0.0347 0.5902 0.0757
-9.000 -0.6599 0.01568 0.00811 -0.0337 0.5814 0.0776
-8.750 -0.6363 0.01546 0.00784 -0.0328 0.5724 0.0791
-8.500 -0.6130 0.01526 0.00759 -0.0318 0.5629 0.0808
-8.250 -0.5888 0.01506 0.00736 -0.0309 0.5540 0.0825
-8.000 -0.5645 0.01490 0.00713 -0.0301 0.5453 0.0842
-7.750 -0.5395 0.01475 0.00691 -0.0294 0.5382 0.0858
-7.500 -0.5151 0.01456 0.00668 -0.0285 0.5303 0.0876
-7.250 -0.4907 0.01440 0.00648 -0.0277 0.5227 0.0893
-7.000 -0.4655 0.01424 0.00630 -0.0271 0.5158 0.0913
-6.750 -0.4400 0.01413 0.00613 -0.0264 0.5086 0.0935
-6.500 -0.4142 0.01403 0.00596 -0.0258 0.5028 0.0954
-6.250 -0.3894 0.01383 0.00577 -0.0251 0.4970 0.0978
-6.000 -0.3641 0.01369 0.00561 -0.0244 0.4906 0.0998
-5.750 -0.3387 0.01359 0.00545 -0.0238 0.4844 0.1017
-5.500 -0.3126 0.01346 0.00529 -0.0233 0.4791 0.1036
-5.250 -0.2864 0.01336 0.00514 -0.0227 0.4736 0.1053
-5.000 -0.2614 0.01321 0.00498 -0.0220 0.4685 0.1075
-4.750 -0.2357 0.01309 0.00484 -0.0214 0.4639 0.1096
-4.500 -0.2095 0.01297 0.00472 -0.0209 0.4590 0.1120
-4.250 -0.1833 0.01289 0.00460 -0.0204 0.4536 0.1144
-4.000 -0.1572 0.01283 0.00449 -0.0199 0.4485 0.1166
-3.750 -0.1315 0.01271 0.00437 -0.0194 0.4444 0.1194
-3.500 -0.1052 0.01261 0.00428 -0.0189 0.4404 0.1225
-3.250 -0.0788 0.01254 0.00419 -0.0184 0.4360 0.1258
-3.000 -0.0525 0.01250 0.00411 -0.0180 0.4315 0.1289
-2.750 -0.0269 0.01243 0.00403 -0.0174 0.4271 0.1331
-2.500 -0.0003 0.01235 0.00397 -0.0170 0.4233 0.1375
-2.250 0.0263 0.01230 0.00391 -0.0166 0.4192 0.1415
-2.000 0.0522 0.01223 0.00385 -0.0161 0.4153 0.1472
-1.750 0.0782 0.01220 0.00381 -0.0156 0.4115 0.1536
-1.500 0.1041 0.01216 0.00377 -0.0151 0.4081 0.1607
-1.250 0.1304 0.01209 0.00374 -0.0147 0.4049 0.1693
-1.000 0.1564 0.01202 0.00371 -0.0142 0.4012 0.1793
-0.750 0.1821 0.01197 0.00369 -0.0137 0.3972 0.1922
-0.500 0.2071 0.01191 0.00368 -0.0131 0.3934 0.2115
-0.250 0.2316 0.01184 0.00368 -0.0125 0.3901 0.2375
0.000 0.2568 0.01173 0.00368 -0.0119 0.3875 0.2671
0.250 0.2815 0.01162 0.00369 -0.0112 0.3845 0.3009
0.500 0.3057 0.01152 0.00371 -0.0105 0.3813 0.3375
0.750 0.3293 0.01142 0.00373 -0.0097 0.3781 0.3771
1.000 0.3518 0.01131 0.00375 -0.0087 0.3748 0.4218
1.250 0.3713 0.01110 0.00378 -0.0071 0.3718 0.4962
1.500 0.3889 0.01080 0.00381 -0.0051 0.3692 0.5898
1.750 0.4064 0.01056 0.00385 -0.0029 0.3664 0.6646
2.000 0.4230 0.01032 0.00394 -0.0005 0.3638 0.7546
2.250 0.4481 0.01026 0.00409 0.0003 0.3608 0.8197
2.500 0.4851 0.01036 0.00430 -0.0015 0.3577 0.8655
2.750 0.5274 0.01057 0.00452 -0.0044 0.3545 0.8952
3.000 0.5767 0.01079 0.00477 -0.0087 0.3517 0.9158
3.250 0.6147 0.01101 0.00499 -0.0106 0.3487 0.9309
3.500 0.6590 0.01129 0.00524 -0.0139 0.3452 0.9382
3.750 0.6814 0.01151 0.00543 -0.0128 0.3424 0.9485
4.000 0.7195 0.01178 0.00565 -0.0150 0.3395 0.9509
4.250 0.7565 0.01204 0.00588 -0.0169 0.3369 0.9542
4.500 0.7911 0.01225 0.00610 -0.0183 0.3347 0.9594
4.750 0.8194 0.01246 0.00630 -0.0185 0.3324 0.9651
5.000 0.8553 0.01266 0.00648 -0.0203 0.3295 0.9668
5.250 0.8894 0.01287 0.00667 -0.0218 0.3267 0.9691
5.500 0.9207 0.01310 0.00688 -0.0229 0.3239 0.9719
5.750 0.9474 0.01336 0.00710 -0.0230 0.3214 0.9756
6.000 0.9730 0.01357 0.00732 -0.0229 0.3194 0.9790
6.250 1.0058 0.01374 0.00751 -0.0242 0.3172 0.9803
6.500 1.0371 0.01393 0.00771 -0.0253 0.3148 0.9819
6.750 1.0675 0.01415 0.00793 -0.0263 0.3121 0.9838
7.000 1.0967 0.01440 0.00816 -0.0270 0.3095 0.9863
7.250 1.1236 0.01469 0.00843 -0.0274 0.3069 0.9890
7.500 1.1472 0.01504 0.00876 -0.0273 0.3041 0.9917
7.750 1.1780 0.01523 0.00899 -0.0284 0.3018 0.9932
8.000 1.2080 0.01545 0.00924 -0.0295 0.2993 0.9951
8.250 1.2369 0.01572 0.00952 -0.0304 0.2967 0.9972
8.500 1.2639 0.01602 0.00983 -0.0310 0.2939 0.9992
8.750 1.2733 0.01634 0.01016 -0.0284 0.2920 1.0000
9.000 1.2682 0.01676 0.01060 -0.0234 0.2903 1.0000
9.250 1.2672 0.01732 0.01116 -0.0194 0.2883 1.0000
9.500 1.2739 0.01780 0.01168 -0.0167 0.2868 1.0000
9.750 1.2825 0.01830 0.01222 -0.0143 0.2849 1.0000
10.000 1.2913 0.01886 0.01282 -0.0122 0.2829 1.0000
10.250 1.3000 0.01949 0.01348 -0.0102 0.2805 1.0000
10.500 1.3089 0.02018 0.01418 -0.0083 0.2784 1.0000
10.750 1.3175 0.02094 0.01495 -0.0065 0.2763 1.0000
11.000 1.3255 0.02178 0.01581 -0.0048 0.2743 1.0000
11.250 1.3336 0.02268 0.01671 -0.0032 0.2721 1.0000
11.500 1.3459 0.02340 0.01749 -0.0020 0.2705 1.0000
11.750 1.3570 0.02421 0.01835 -0.0008 0.2684 1.0000
12.000 1.3673 0.02511 0.01929 0.0003 0.2661 1.0000
12.250 1.3761 0.02613 0.02035 0.0014 0.2635 1.0000
12.500 1.3842 0.02723 0.02147 0.0025 0.2611 1.0000
12.750 1.3903 0.02850 0.02275 0.0037 0.2586 1.0000
13.000 1.3983 0.02968 0.02396 0.0046 0.2565 1.0000
13.250 1.4081 0.03080 0.02514 0.0054 0.2545 1.0000
13.500 1.4171 0.03200 0.02640 0.0061 0.2522 1.0000
13.750 1.4242 0.03338 0.02783 0.0068 0.2497 1.0000
14.000 1.4302 0.03490 0.02939 0.0074 0.2471 1.0000
14.250 1.4345 0.03660 0.03111 0.0080 0.2444 1.0000
14.500 1.4381 0.03842 0.03295 0.0085 0.2417 1.0000
14.750 1.4457 0.03997 0.03457 0.0089 0.2393 1.0000
15.000 1.4484 0.04202 0.03669 0.0091 0.2355 1.0000
15.250 1.4493 0.04426 0.03896 0.0094 0.2319 1.0000
15.500 1.4481 0.04671 0.04141 0.0096 0.2283 1.0000
15.750 1.4494 0.04904 0.04382 0.0097 0.2246 1.0000
16.000 1.4483 0.05163 0.04647 0.0097 0.2205 1.0000
16.250 1.4425 0.05471 0.04957 0.0097 0.2157 1.0000
16.500 1.4397 0.05754 0.05243 0.0096 0.2123 1.0000
16.750 1.4374 0.06038 0.05534 0.0094 0.2082 1.0000
17.000 1.4291 0.06389 0.05888 0.0092 0.2030 1.0000
17.250 1.4217 0.06736 0.06237 0.0088 0.1991 1.0000
17.500 1.4195 0.07030 0.06538 0.0085 0.1955 1.0000
17.750 1.4134 0.07371 0.06884 0.0080 0.1915 1.0000
18.000 1.4027 0.07768 0.07281 0.0075 0.1872 1.0000
18.250 1.3998 0.08079 0.07598 0.0069 0.1836 1.0000
18.500 1.3923 0.08450 0.07975 0.0063 0.1796 1.0000
18.750 1.3865 0.08801 0.08328 0.0056 0.1759 1.0000
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