GOE 676 (= M 12) AIRFOIL (goe676-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 676 (= M 12) AIRFOIL (goe676-il) Reynolds number: 1,000,000 Max Cl/Cd: 85.93 at α=7.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe676-il-1000000-n5.txt Download as CSV file: xf-goe676-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: GOE 676 (= M 12) 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
------ -------- --------- --------- -------- -------- --------
-17.000 -1.3002 0.05011 0.04712 -0.0501 1.0000 0.0078
-16.750 -1.3239 0.04369 0.04049 -0.0538 1.0000 0.0078
-16.500 -1.3383 0.03950 0.03612 -0.0547 1.0000 0.0079
-16.250 -1.3472 0.03637 0.03285 -0.0543 1.0000 0.0081
-16.000 -1.3518 0.03392 0.03027 -0.0531 1.0000 0.0082
-15.750 -1.3529 0.03193 0.02815 -0.0515 1.0000 0.0084
-15.500 -1.3511 0.03027 0.02637 -0.0496 1.0000 0.0087
-15.250 -1.3469 0.02884 0.02484 -0.0474 1.0000 0.0089
-15.000 -1.3408 0.02761 0.02349 -0.0452 1.0000 0.0091
-14.750 -1.3317 0.02651 0.02228 -0.0431 1.0000 0.0094
-14.500 -1.3186 0.02548 0.02115 -0.0416 1.0000 0.0096
-14.250 -1.3036 0.02454 0.02011 -0.0403 1.0000 0.0099
-14.000 -1.2884 0.02352 0.01899 -0.0390 1.0000 0.0104
-13.750 -1.2718 0.02258 0.01798 -0.0378 1.0000 0.0109
-13.500 -1.2538 0.02174 0.01707 -0.0368 1.0000 0.0115
-13.250 -1.2346 0.02098 0.01624 -0.0358 1.0000 0.0120
-13.000 -1.2146 0.02029 0.01546 -0.0349 1.0000 0.0126
-12.750 -1.1941 0.01961 0.01473 -0.0341 1.0000 0.0133
-12.500 -1.1729 0.01900 0.01409 -0.0333 1.0000 0.0142
-12.250 -1.1510 0.01846 0.01350 -0.0326 1.0000 0.0152
-12.000 -1.1288 0.01795 0.01294 -0.0319 1.0000 0.0160
-11.750 -1.1064 0.01745 0.01239 -0.0312 1.0000 0.0167
-11.500 -1.0836 0.01703 0.01195 -0.0306 1.0000 0.0175
-11.250 -1.0607 0.01665 0.01154 -0.0299 1.0000 0.0184
-11.000 -1.0378 0.01627 0.01113 -0.0291 0.9997 0.0191
-10.750 -1.0079 0.01587 0.01068 -0.0299 0.9952 0.0198
-10.500 -0.9781 0.01551 0.01025 -0.0306 0.9901 0.0204
-10.250 -0.9484 0.01504 0.00975 -0.0314 0.9843 0.0212
-10.000 -0.9197 0.01469 0.00939 -0.0318 0.9767 0.0220
-9.750 -0.8917 0.01437 0.00904 -0.0321 0.9685 0.0227
-9.500 -0.8651 0.01408 0.00870 -0.0319 0.9594 0.0233
-9.250 -0.8399 0.01381 0.00838 -0.0315 0.9493 0.0240
-9.000 -0.8148 0.01355 0.00806 -0.0310 0.9394 0.0246
-8.750 -0.7900 0.01330 0.00773 -0.0304 0.9291 0.0250
-8.500 -0.7645 0.01307 0.00744 -0.0299 0.9180 0.0253
-8.250 -0.7403 0.01266 0.00696 -0.0293 0.9063 0.0261
-8.000 -0.7155 0.01232 0.00657 -0.0287 0.8938 0.0269
-7.750 -0.6900 0.01207 0.00627 -0.0283 0.8813 0.0276
-7.500 -0.6641 0.01185 0.00599 -0.0279 0.8696 0.0283
-7.250 -0.6378 0.01161 0.00569 -0.0276 0.8596 0.0289
-7.000 -0.6115 0.01139 0.00540 -0.0273 0.8502 0.0295
-6.750 -0.5848 0.01117 0.00512 -0.0271 0.8407 0.0301
-6.500 -0.5581 0.01095 0.00484 -0.0269 0.8323 0.0305
-6.250 -0.5312 0.01075 0.00457 -0.0267 0.8240 0.0309
-6.000 -0.5041 0.01056 0.00433 -0.0266 0.8164 0.0312
-5.750 -0.4775 0.01030 0.00401 -0.0263 0.8082 0.0320
-5.500 -0.4504 0.01006 0.00374 -0.0262 0.8006 0.0330
-5.250 -0.4232 0.00988 0.00353 -0.0261 0.7920 0.0340
-5.000 -0.3958 0.00971 0.00333 -0.0260 0.7833 0.0352
-4.750 -0.3684 0.00956 0.00314 -0.0259 0.7730 0.0362
-4.500 -0.3408 0.00942 0.00295 -0.0258 0.7607 0.0372
-4.250 -0.3132 0.00930 0.00278 -0.0257 0.7469 0.0380
-4.000 -0.2858 0.00916 0.00259 -0.0256 0.7308 0.0401
-3.750 -0.2585 0.00906 0.00244 -0.0255 0.7103 0.0426
-3.500 -0.2311 0.00899 0.00230 -0.0254 0.6870 0.0452
-3.250 -0.2035 0.00894 0.00217 -0.0253 0.6676 0.0477
-3.000 -0.1759 0.00885 0.00206 -0.0253 0.6535 0.0521
-2.750 -0.1480 0.00878 0.00196 -0.0253 0.6417 0.0558
-2.500 -0.1201 0.00871 0.00186 -0.0253 0.6315 0.0607
-2.250 -0.0921 0.00863 0.00178 -0.0254 0.6220 0.0656
-2.000 -0.0639 0.00858 0.00170 -0.0254 0.6140 0.0685
-1.750 -0.0359 0.00851 0.00162 -0.0255 0.6053 0.0743
-1.500 -0.0077 0.00844 0.00154 -0.0255 0.5982 0.0800
-1.250 0.0204 0.00836 0.00148 -0.0256 0.5906 0.0894
-1.000 0.0481 0.00822 0.00143 -0.0256 0.5832 0.1177
-0.750 0.0759 0.00813 0.00139 -0.0257 0.5725 0.1431
-0.500 0.1038 0.00804 0.00135 -0.0257 0.5603 0.1669
-0.250 0.1311 0.00788 0.00130 -0.0257 0.5496 0.2110
0.000 0.1569 0.00749 0.00124 -0.0255 0.5387 0.3250
0.250 0.1824 0.00712 0.00120 -0.0253 0.5247 0.4431
0.500 0.2078 0.00679 0.00116 -0.0250 0.5086 0.5510
0.750 0.2322 0.00643 0.00115 -0.0245 0.4919 0.6751
1.000 0.2575 0.00625 0.00118 -0.0240 0.4750 0.7509
1.250 0.2823 0.00615 0.00126 -0.0232 0.4576 0.8242
1.500 0.3083 0.00619 0.00134 -0.0227 0.4405 0.8629
1.750 0.3355 0.00629 0.00141 -0.0225 0.4254 0.8787
2.000 0.3625 0.00640 0.00149 -0.0223 0.4081 0.8917
2.250 0.3889 0.00653 0.00158 -0.0219 0.3910 0.9070
2.500 0.4153 0.00665 0.00168 -0.0215 0.3770 0.9205
2.750 0.4423 0.00677 0.00176 -0.0214 0.3642 0.9291
3.000 0.4694 0.00690 0.00185 -0.0212 0.3528 0.9351
3.250 0.4967 0.00701 0.00193 -0.0211 0.3420 0.9414
3.500 0.5239 0.00713 0.00203 -0.0209 0.3323 0.9472
3.750 0.5505 0.00728 0.00214 -0.0206 0.3209 0.9549
4.000 0.5774 0.00745 0.00226 -0.0204 0.3065 0.9624
4.250 0.6052 0.00761 0.00238 -0.0205 0.2931 0.9676
4.500 0.6327 0.00775 0.00248 -0.0205 0.2830 0.9717
4.750 0.6624 0.00792 0.00262 -0.0210 0.2706 0.9744
5.000 0.6914 0.00822 0.00279 -0.0215 0.2445 0.9778
5.250 0.7180 0.00869 0.00305 -0.0216 0.1996 0.9820
5.500 0.7444 0.00935 0.00343 -0.0219 0.1428 0.9850
5.750 0.7744 0.00967 0.00367 -0.0227 0.1272 0.9867
6.250 0.8347 0.01017 0.00412 -0.0242 0.1123 0.9906
6.500 0.8642 0.01044 0.00436 -0.0248 0.1059 0.9926
6.750 0.8940 0.01067 0.00459 -0.0255 0.1002 0.9942
7.000 0.9248 0.01089 0.00481 -0.0264 0.0951 0.9953
7.250 0.9547 0.01119 0.00507 -0.0273 0.0877 0.9967
7.500 0.9847 0.01146 0.00532 -0.0281 0.0790 0.9983
7.750 1.0126 0.01197 0.00569 -0.0286 0.0574 1.0000
8.000 1.0294 0.01247 0.00608 -0.0268 0.0420 1.0000
8.250 1.0483 0.01287 0.00645 -0.0253 0.0352 1.0000
8.500 1.0683 0.01323 0.00680 -0.0240 0.0313 1.0000
8.750 1.0894 0.01357 0.00714 -0.0230 0.0284 1.0000
9.000 1.1107 0.01394 0.00751 -0.0221 0.0257 1.0000
9.250 1.1320 0.01434 0.00791 -0.0211 0.0230 1.0000
9.500 1.1538 0.01471 0.00829 -0.0203 0.0208 1.0000
9.750 1.1746 0.01516 0.00873 -0.0194 0.0184 1.0000
10.000 1.1960 0.01555 0.00916 -0.0186 0.0170 1.0000
10.250 1.2164 0.01602 0.00963 -0.0177 0.0154 1.0000
10.500 1.2363 0.01650 0.01013 -0.0167 0.0141 1.0000
10.750 1.2562 0.01696 0.01061 -0.0157 0.0131 1.0000
11.000 1.2750 0.01747 0.01115 -0.0146 0.0122 1.0000
11.250 1.2923 0.01804 0.01174 -0.0132 0.0114 1.0000
11.500 1.3071 0.01861 0.01235 -0.0115 0.0108 1.0000
11.750 1.3223 0.01917 0.01296 -0.0098 0.0105 1.0000
12.000 1.3369 0.01979 0.01363 -0.0082 0.0100 1.0000
12.250 1.3509 0.02049 0.01437 -0.0067 0.0096 1.0000
12.500 1.3640 0.02127 0.01520 -0.0052 0.0092 1.0000
12.750 1.3762 0.02216 0.01613 -0.0037 0.0088 1.0000
13.000 1.3869 0.02319 0.01721 -0.0022 0.0084 1.0000
13.250 1.3983 0.02421 0.01830 -0.0010 0.0081 1.0000
13.500 1.4100 0.02526 0.01942 0.0001 0.0079 1.0000
13.750 1.4205 0.02645 0.02067 0.0011 0.0077 1.0000
14.000 1.4302 0.02775 0.02203 0.0021 0.0075 1.0000
14.250 1.4390 0.02919 0.02354 0.0029 0.0073 1.0000
14.500 1.4467 0.03077 0.02519 0.0037 0.0071 1.0000
14.750 1.4533 0.03251 0.02700 0.0043 0.0069 1.0000
15.000 1.4588 0.03442 0.02898 0.0048 0.0067 1.0000
15.250 1.4625 0.03656 0.03120 0.0052 0.0065 1.0000
15.500 1.4647 0.03896 0.03368 0.0054 0.0064 1.0000
15.750 1.4646 0.04170 0.03652 0.0055 0.0062 1.0000
16.000 1.4638 0.04459 0.03949 0.0053 0.0061 1.0000
16.250 1.4641 0.04744 0.04244 0.0050 0.0060 1.0000
16.500 1.4629 0.05053 0.04563 0.0046 0.0060 1.0000
16.750 1.4603 0.05386 0.04906 0.0040 0.0059 1.0000
17.000 1.4563 0.05747 0.05278 0.0032 0.0058 1.0000
17.250 1.4512 0.06135 0.05676 0.0023 0.0058 1.0000
17.500 1.4445 0.06551 0.06103 0.0011 0.0057 1.0000
17.750 1.4365 0.06998 0.06560 -0.0003 0.0057 1.0000
18.000 1.4275 0.07471 0.07044 -0.0018 0.0056 1.0000
18.250 1.4172 0.07972 0.07556 -0.0036 0.0055 1.0000
18.500 1.4052 0.08506 0.08102 -0.0056 0.0055 1.0000
18.750 1.3928 0.09060 0.08667 -0.0077 0.0055 1.0000
19.000 1.3793 0.09638 0.09256 -0.0100 0.0054 1.0000
19.250 1.3643 0.10244 0.09873 -0.0125 0.0054 1.0000
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