GOE 735 AIRFOIL (goe735-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: GOE 735 AIRFOIL (goe735-il) Reynolds number: 500,000 Max Cl/Cd: 82.17 at α=7.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-goe735-il-500000.txt Download as CSV file: xf-goe735-il-500000.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 = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.250 -0.9242 0.09342 0.08983 -0.0458 1.0000 0.0419
-19.000 -0.9475 0.08623 0.08251 -0.0503 1.0000 0.0422
-18.750 -0.9709 0.07913 0.07528 -0.0548 1.0000 0.0426
-18.500 -0.9917 0.07269 0.06871 -0.0588 1.0000 0.0429
-18.250 -1.0108 0.06650 0.06238 -0.0627 1.0000 0.0433
-18.000 -1.0273 0.06080 0.05654 -0.0663 1.0000 0.0437
-17.750 -1.0404 0.05565 0.05124 -0.0695 1.0000 0.0440
-17.500 -1.0503 0.05115 0.04658 -0.0722 1.0000 0.0443
-17.250 -1.0582 0.04735 0.04274 -0.0738 1.0000 0.0448
-17.000 -1.0640 0.04387 0.03922 -0.0754 1.0000 0.0453
-16.750 -1.0673 0.04081 0.03611 -0.0765 1.0000 0.0458
-16.500 -1.0686 0.03816 0.03340 -0.0772 1.0000 0.0463
-16.250 -1.0680 0.03587 0.03104 -0.0774 1.0000 0.0470
-16.000 -1.0653 0.03389 0.02899 -0.0773 1.0000 0.0477
-15.750 -1.0408 0.03185 0.02679 -0.0811 0.9312 0.0489
-15.500 -1.0248 0.03016 0.02483 -0.0827 0.8750 0.0498
-15.250 -1.0252 0.02886 0.02340 -0.0806 0.8502 0.0505
-15.000 -1.0219 0.02778 0.02221 -0.0786 0.8344 0.0513
-14.750 -1.0159 0.02688 0.02119 -0.0766 0.8222 0.0522
-14.500 -1.0088 0.02600 0.02020 -0.0746 0.8115 0.0532
-14.250 -0.9997 0.02526 0.01931 -0.0726 0.8024 0.0543
-14.000 -0.9933 0.02435 0.01835 -0.0703 0.7936 0.0554
-13.750 -0.9849 0.02365 0.01760 -0.0680 0.7858 0.0566
-13.500 -0.9730 0.02306 0.01696 -0.0660 0.7782 0.0579
-13.250 -0.9600 0.02252 0.01633 -0.0640 0.7708 0.0594
-13.000 -0.9471 0.02199 0.01566 -0.0618 0.7641 0.0608
-12.750 -0.9358 0.02136 0.01506 -0.0596 0.7573 0.0623
-12.500 -0.9206 0.02096 0.01461 -0.0576 0.7503 0.0639
-12.250 -0.9045 0.02061 0.01415 -0.0557 0.7437 0.0658
-12.000 -0.8891 0.02012 0.01362 -0.0537 0.7370 0.0676
-11.750 -0.8735 0.01974 0.01322 -0.0517 0.7304 0.0694
-11.500 -0.8560 0.01950 0.01290 -0.0498 0.7240 0.0713
-11.250 -0.8373 0.01922 0.01255 -0.0481 0.7171 0.0733
-11.000 -0.8213 0.01875 0.01205 -0.0461 0.7101 0.0751
-10.750 -0.8038 0.01855 0.01181 -0.0441 0.7034 0.0769
-10.500 -0.7845 0.01834 0.01157 -0.0424 0.6966 0.0789
-10.250 -0.7643 0.01816 0.01128 -0.0409 0.6892 0.0808
-10.000 -0.7444 0.01776 0.01084 -0.0394 0.6822 0.0828
-9.750 -0.7228 0.01751 0.01061 -0.0382 0.6744 0.0846
-9.500 -0.7006 0.01736 0.01038 -0.0369 0.6665 0.0867
-9.250 -0.6776 0.01718 0.01011 -0.0358 0.6588 0.0886
-9.000 -0.6550 0.01680 0.00968 -0.0348 0.6502 0.0905
-8.750 -0.6326 0.01651 0.00937 -0.0337 0.6420 0.0924
-8.500 -0.6087 0.01631 0.00916 -0.0328 0.6326 0.0943
-8.250 -0.5848 0.01616 0.00891 -0.0318 0.6238 0.0964
-8.000 -0.5600 0.01602 0.00870 -0.0310 0.6148 0.0981
-7.750 -0.5366 0.01559 0.00823 -0.0301 0.6056 0.1002
-7.500 -0.5124 0.01534 0.00798 -0.0293 0.5965 0.1021
-7.250 -0.4878 0.01519 0.00777 -0.0285 0.5869 0.1042
-7.000 -0.4625 0.01506 0.00757 -0.0278 0.5783 0.1064
-6.750 -0.4369 0.01498 0.00739 -0.0271 0.5695 0.1082
-6.500 -0.4132 0.01459 0.00699 -0.0263 0.5615 0.1109
-6.250 -0.3880 0.01442 0.00682 -0.0256 0.5533 0.1134
-6.000 -0.3628 0.01431 0.00664 -0.0249 0.5452 0.1157
-5.750 -0.3368 0.01417 0.00646 -0.0244 0.5380 0.1179
-5.500 -0.3107 0.01407 0.00628 -0.0238 0.5307 0.1197
-5.250 -0.2873 0.01374 0.00593 -0.0229 0.5241 0.1227
-5.000 -0.2616 0.01355 0.00576 -0.0223 0.5180 0.1252
-4.750 -0.2357 0.01343 0.00561 -0.0217 0.5113 0.1279
-4.500 -0.2100 0.01339 0.00547 -0.0211 0.5048 0.1305
-4.250 -0.1845 0.01316 0.00525 -0.0205 0.4995 0.1334
-4.000 -0.1596 0.01296 0.00507 -0.0198 0.4939 0.1368
-3.750 -0.1340 0.01288 0.00494 -0.0192 0.4884 0.1404
-3.500 -0.1077 0.01283 0.00485 -0.0187 0.4834 0.1439
-3.250 -0.0825 0.01262 0.00467 -0.0180 0.4784 0.1485
-3.000 -0.0571 0.01250 0.00455 -0.0174 0.4731 0.1534
-2.750 -0.0312 0.01247 0.00446 -0.0169 0.4678 0.1583
-2.500 -0.0061 0.01232 0.00434 -0.0162 0.4636 0.1652
-2.250 0.0199 0.01221 0.00426 -0.0157 0.4592 0.1729
-2.000 0.0451 0.01208 0.00417 -0.0150 0.4547 0.1827
-1.750 0.0703 0.01201 0.00409 -0.0144 0.4503 0.1949
-1.500 0.0949 0.01191 0.00405 -0.0137 0.4460 0.2135
-1.250 0.1195 0.01170 0.00400 -0.0130 0.4420 0.2442
-1.000 0.1432 0.01149 0.00396 -0.0122 0.4379 0.2883
-0.750 0.1661 0.01129 0.00393 -0.0112 0.4338 0.3381
-0.500 0.1884 0.01116 0.00391 -0.0101 0.4297 0.3891
-0.250 0.2089 0.01088 0.00390 -0.0087 0.4265 0.4564
0.000 0.2243 0.01043 0.00390 -0.0062 0.4234 0.5681
0.250 0.2390 0.01005 0.00390 -0.0034 0.4201 0.6674
0.500 0.2563 0.00976 0.00399 -0.0009 0.4166 0.7722
0.750 0.2862 0.00977 0.00415 -0.0009 0.4126 0.8369
1.000 0.3249 0.00993 0.00437 -0.0028 0.4086 0.8762
1.250 0.3671 0.01009 0.00456 -0.0055 0.4049 0.8979
1.500 0.4015 0.01027 0.00473 -0.0065 0.4013 0.9139
1.750 0.4464 0.01054 0.00494 -0.0098 0.3975 0.9223
2.000 0.4756 0.01081 0.00513 -0.0098 0.3940 0.9324
2.250 0.5201 0.01113 0.00541 -0.0130 0.3904 0.9363
2.500 0.5591 0.01138 0.00565 -0.0151 0.3872 0.9417
2.750 0.5954 0.01166 0.00591 -0.0165 0.3837 0.9495
3.000 0.6494 0.01203 0.00622 -0.0215 0.3798 0.9534
3.250 0.6916 0.01240 0.00650 -0.0243 0.3762 0.9597
3.500 0.7267 0.01269 0.00675 -0.0257 0.3731 0.9650
3.750 0.7690 0.01283 0.00689 -0.0287 0.3704 0.9671
4.000 0.8118 0.01300 0.00706 -0.0317 0.3672 0.9705
4.250 0.8483 0.01320 0.00724 -0.0336 0.3642 0.9756
4.500 0.8833 0.01337 0.00736 -0.0352 0.3611 0.9794
4.750 0.9202 0.01356 0.00747 -0.0373 0.3576 0.9812
5.000 0.9558 0.01369 0.00761 -0.0391 0.3551 0.9834
5.250 0.9904 0.01379 0.00773 -0.0407 0.3527 0.9862
5.500 1.0246 0.01391 0.00786 -0.0423 0.3499 0.9898
5.750 1.0613 0.01402 0.00796 -0.0444 0.3470 0.9928
6.000 1.0992 0.01410 0.00801 -0.0468 0.3441 0.9953
6.250 1.1335 0.01428 0.00814 -0.0485 0.3411 0.9978
6.500 1.1666 0.01448 0.00832 -0.0500 0.3384 0.9997
6.750 1.1885 0.01460 0.00849 -0.0493 0.3362 1.0000
7.000 1.2070 0.01475 0.00868 -0.0479 0.3339 1.0000
7.250 1.2250 0.01493 0.00887 -0.0465 0.3314 1.0000
7.500 1.2424 0.01512 0.00906 -0.0449 0.3290 1.0000
7.750 1.2590 0.01535 0.00928 -0.0433 0.3267 1.0000
8.000 1.2749 0.01566 0.00954 -0.0415 0.3239 1.0000
8.250 1.2910 0.01596 0.00985 -0.0398 0.3218 1.0000
8.500 1.3051 0.01618 0.01013 -0.0377 0.3201 1.0000
8.750 1.3182 0.01642 0.01042 -0.0355 0.3181 1.0000
9.000 1.3298 0.01667 0.01070 -0.0330 0.3159 1.0000
9.250 1.3395 0.01693 0.01099 -0.0302 0.3137 1.0000
9.500 1.3442 0.01720 0.01127 -0.0265 0.3117 1.0000
9.750 1.3449 0.01750 0.01157 -0.0222 0.3098 1.0000
10.000 1.3510 0.01790 0.01194 -0.0190 0.3076 1.0000
10.250 1.3596 0.01832 0.01237 -0.0163 0.3055 1.0000
10.500 1.3630 0.01878 0.01290 -0.0131 0.3039 1.0000
10.750 1.3688 0.01929 0.01348 -0.0104 0.3020 1.0000
11.000 1.3765 0.01985 0.01408 -0.0082 0.2998 1.0000
11.250 1.3854 0.02043 0.01469 -0.0062 0.2976 1.0000
11.500 1.3948 0.02105 0.01533 -0.0044 0.2953 1.0000
11.750 1.4058 0.02168 0.01595 -0.0028 0.2929 1.0000
12.000 1.4226 0.02219 0.01641 -0.0018 0.2901 1.0000
12.250 1.4294 0.02305 0.01736 -0.0001 0.2885 1.0000
12.500 1.4371 0.02393 0.01832 0.0014 0.2865 1.0000
12.750 1.4457 0.02483 0.01928 0.0027 0.2841 1.0000
13.000 1.4550 0.02574 0.02023 0.0038 0.2818 1.0000
13.250 1.4643 0.02667 0.02119 0.0049 0.2794 1.0000
13.500 1.4756 0.02753 0.02203 0.0058 0.2769 1.0000
13.750 1.4911 0.02817 0.02264 0.0066 0.2741 1.0000
14.000 1.4927 0.02970 0.02430 0.0077 0.2719 1.0000
14.250 1.4969 0.03113 0.02582 0.0086 0.2692 1.0000
14.500 1.5029 0.03248 0.02722 0.0094 0.2665 1.0000
14.750 1.5083 0.03391 0.02867 0.0100 0.2635 1.0000
15.000 1.5185 0.03497 0.02970 0.0106 0.2602 1.0000
15.250 1.5202 0.03685 0.03166 0.0112 0.2571 1.0000
15.500 1.5190 0.03908 0.03399 0.0116 0.2537 1.0000
15.750 1.5195 0.04124 0.03621 0.0118 0.2501 1.0000
16.000 1.5236 0.04306 0.03800 0.0121 0.2462 1.0000
16.250 1.5258 0.04511 0.04009 0.0123 0.2427 1.0000
16.500 1.5203 0.04809 0.04320 0.0122 0.2390 1.0000
16.750 1.5189 0.05069 0.04584 0.0122 0.2354 1.0000
17.000 1.5207 0.05290 0.04804 0.0122 0.2316 1.0000
17.250 1.5195 0.05548 0.05066 0.0121 0.2281 1.0000
17.500 1.5125 0.05883 0.05413 0.0117 0.2245 1.0000
17.750 1.5082 0.06188 0.05722 0.0114 0.2204 1.0000
18.000 1.5089 0.06433 0.05967 0.0112 0.2172 1.0000
18.250 1.5062 0.06720 0.06259 0.0109 0.2137 1.0000
18.500 1.4955 0.07117 0.06667 0.0102 0.2100 1.0000
18.750 1.4896 0.07455 0.07008 0.0096 0.2060 1.0000
19.000 1.4915 0.07693 0.07243 0.0093 0.2026 1.0000
19.250 1.4813 0.08091 0.07651 0.0085 0.1990 1.0000
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