GOE 290 (MVA 290) AIRFOIL (goe290-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 290 (MVA 290) AIRFOIL (goe290-il) Reynolds number: 1,000,000 Max Cl/Cd: 92.44 at α=6.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe290-il-1000000-n5.txt Download as CSV file: xf-goe290-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: GOE 290 (MVA 290) 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 -1.0257 0.10916 0.10624 -0.0362 1.0000 0.0257
-19.500 -1.0527 0.10093 0.09789 -0.0409 1.0000 0.0258
-19.250 -1.0770 0.09331 0.09016 -0.0453 1.0000 0.0259
-19.000 -1.0998 0.08614 0.08287 -0.0494 1.0000 0.0260
-18.750 -1.1200 0.07956 0.07618 -0.0532 1.0000 0.0261
-18.500 -1.1397 0.07335 0.06986 -0.0568 1.0000 0.0262
-18.250 -1.1592 0.06742 0.06382 -0.0601 1.0000 0.0263
-18.000 -1.1776 0.06169 0.05799 -0.0634 1.0000 0.0264
-17.750 -1.1936 0.05624 0.05242 -0.0666 1.0000 0.0265
-17.500 -1.2059 0.05119 0.04727 -0.0696 1.0000 0.0266
-17.250 -1.2147 0.04644 0.04240 -0.0726 1.0000 0.0267
-17.000 -1.2194 0.04208 0.03794 -0.0756 1.0000 0.0269
-16.750 -1.2203 0.03819 0.03393 -0.0785 1.0000 0.0270
-16.500 -1.2187 0.03476 0.03040 -0.0811 1.0000 0.0271
-16.250 -1.2148 0.03190 0.02743 -0.0830 1.0000 0.0272
-16.000 -1.2094 0.02959 0.02503 -0.0842 1.0000 0.0273
-15.750 -1.2027 0.02775 0.02309 -0.0845 1.0000 0.0274
-15.500 -1.1963 0.02619 0.02145 -0.0841 1.0000 0.0275
-15.250 -1.1924 0.02475 0.01995 -0.0829 1.0000 0.0277
-15.000 -1.1885 0.02368 0.01882 -0.0807 1.0000 0.0279
-14.750 -1.1734 0.02275 0.01784 -0.0800 0.9934 0.0282
-14.500 -1.1521 0.02192 0.01697 -0.0800 0.9849 0.0285
-14.250 -1.1307 0.02120 0.01620 -0.0798 0.9763 0.0288
-14.000 -1.1105 0.02055 0.01550 -0.0792 0.9688 0.0290
-13.750 -1.0914 0.01996 0.01486 -0.0782 0.9608 0.0292
-13.500 -1.0720 0.01942 0.01425 -0.0771 0.9520 0.0295
-13.250 -1.0518 0.01890 0.01368 -0.0761 0.9423 0.0297
-13.000 -1.0307 0.01840 0.01312 -0.0752 0.9324 0.0300
-12.750 -1.0096 0.01793 0.01259 -0.0743 0.9168 0.0302
-12.500 -0.9901 0.01754 0.01204 -0.0728 0.8748 0.0305
-12.250 -0.9691 0.01724 0.01153 -0.0716 0.8316 0.0307
-12.000 -0.9456 0.01691 0.01106 -0.0710 0.8083 0.0310
-11.750 -0.9212 0.01660 0.01064 -0.0705 0.7908 0.0312
-11.500 -0.8974 0.01617 0.01013 -0.0700 0.7746 0.0317
-11.250 -0.8729 0.01579 0.00966 -0.0696 0.7577 0.0321
-11.000 -0.8478 0.01545 0.00924 -0.0692 0.7394 0.0325
-10.750 -0.8223 0.01515 0.00886 -0.0689 0.7195 0.0329
-10.500 -0.7966 0.01488 0.00848 -0.0686 0.6954 0.0333
-10.250 -0.7707 0.01465 0.00813 -0.0683 0.6680 0.0337
-10.000 -0.7445 0.01443 0.00779 -0.0681 0.6416 0.0342
-9.750 -0.7180 0.01422 0.00747 -0.0679 0.6182 0.0346
-9.500 -0.6912 0.01402 0.00716 -0.0677 0.5983 0.0350
-9.250 -0.6642 0.01382 0.00687 -0.0676 0.5819 0.0354
-9.000 -0.6374 0.01356 0.00654 -0.0674 0.5683 0.0361
-8.750 -0.6101 0.01333 0.00626 -0.0673 0.5578 0.0368
-8.500 -0.5826 0.01312 0.00601 -0.0673 0.5493 0.0376
-8.250 -0.5547 0.01292 0.00577 -0.0673 0.5427 0.0384
-8.000 -0.5267 0.01274 0.00554 -0.0672 0.5361 0.0393
-7.750 -0.4986 0.01257 0.00532 -0.0672 0.5301 0.0400
-7.500 -0.4706 0.01235 0.00509 -0.0672 0.5254 0.0411
-7.250 -0.4423 0.01217 0.00488 -0.0673 0.5203 0.0423
-7.000 -0.4139 0.01201 0.00469 -0.0673 0.5154 0.0435
-6.500 -0.3568 0.01170 0.00434 -0.0675 0.5083 0.0462
-6.250 -0.3280 0.01154 0.00417 -0.0676 0.5053 0.0479
-6.000 -0.2991 0.01141 0.00402 -0.0677 0.5020 0.0495
-5.750 -0.2703 0.01128 0.00388 -0.0678 0.4985 0.0513
-5.500 -0.2415 0.01116 0.00375 -0.0679 0.4949 0.0535
-5.250 -0.2125 0.01106 0.00363 -0.0680 0.4909 0.0554
-5.000 -0.1834 0.01094 0.00350 -0.0682 0.4881 0.0573
-4.750 -0.1542 0.01082 0.00339 -0.0683 0.4848 0.0594
-4.500 -0.1250 0.01073 0.00328 -0.0685 0.4817 0.0615
-4.250 -0.0958 0.01065 0.00318 -0.0687 0.4790 0.0632
-4.000 -0.0667 0.01055 0.00308 -0.0688 0.4757 0.0657
-3.750 -0.0376 0.01048 0.00300 -0.0690 0.4720 0.0682
-3.500 -0.0081 0.01040 0.00291 -0.0692 0.4698 0.0702
-3.250 0.0212 0.01030 0.00281 -0.0694 0.4669 0.0727
-3.000 0.0505 0.01021 0.00273 -0.0696 0.4636 0.0754
-2.750 0.0799 0.01015 0.00265 -0.0698 0.4604 0.0781
-2.500 0.1091 0.01008 0.00258 -0.0700 0.4577 0.0817
-2.250 0.1383 0.01000 0.00251 -0.0702 0.4549 0.0866
-2.000 0.1675 0.00991 0.00245 -0.0704 0.4525 0.0946
-1.750 0.1966 0.00973 0.00238 -0.0706 0.4503 0.1192
-1.500 0.2256 0.00954 0.00230 -0.0708 0.4479 0.1517
-1.250 0.2539 0.00924 0.00220 -0.0710 0.4453 0.2065
-1.000 0.2824 0.00901 0.00217 -0.0712 0.4421 0.2694
-0.750 0.3115 0.00896 0.00217 -0.0714 0.4385 0.2917
-0.500 0.3408 0.00897 0.00218 -0.0717 0.4353 0.3032
-0.250 0.3704 0.00893 0.00219 -0.0719 0.4332 0.3153
0.000 0.4000 0.00892 0.00219 -0.0722 0.4302 0.3260
0.250 0.4294 0.00891 0.00221 -0.0724 0.4257 0.3363
0.500 0.4585 0.00895 0.00222 -0.0726 0.4197 0.3451
0.750 0.4877 0.00895 0.00225 -0.0729 0.4145 0.3561
1.000 0.5171 0.00897 0.00227 -0.0731 0.4097 0.3641
1.250 0.5462 0.00900 0.00230 -0.0733 0.4040 0.3738
1.500 0.5752 0.00904 0.00234 -0.0735 0.3974 0.3843
1.750 0.6040 0.00908 0.00239 -0.0737 0.3882 0.3972
2.000 0.6327 0.00913 0.00244 -0.0739 0.3804 0.4103
2.250 0.6613 0.00916 0.00250 -0.0740 0.3725 0.4293
2.500 0.6895 0.00923 0.00258 -0.0742 0.3623 0.4476
2.750 0.7171 0.00936 0.00268 -0.0742 0.3460 0.4661
3.000 0.7439 0.00954 0.00283 -0.0741 0.3248 0.4914
3.250 0.7697 0.00977 0.00303 -0.0739 0.2991 0.5275
3.500 0.7937 0.01012 0.00333 -0.0735 0.2642 0.5780
3.750 0.8179 0.01038 0.00362 -0.0730 0.2394 0.6385
4.000 0.8438 0.01045 0.00382 -0.0728 0.2290 0.7043
4.250 0.8694 0.01050 0.00403 -0.0724 0.2214 0.7698
4.500 0.8944 0.01052 0.00421 -0.0719 0.2164 0.8331
4.750 0.9177 0.01059 0.00441 -0.0709 0.2114 0.8907
5.000 0.9410 0.01071 0.00461 -0.0698 0.2067 0.9380
5.250 0.9712 0.01085 0.00477 -0.0703 0.2033 0.9716
5.500 1.0039 0.01108 0.00497 -0.0716 0.1981 0.9928
5.750 1.0325 0.01134 0.00518 -0.0720 0.1926 1.0000
6.000 1.0585 0.01153 0.00536 -0.0717 0.1896 1.0000
6.250 1.0843 0.01173 0.00554 -0.0715 0.1855 1.0000
6.500 1.1086 0.01202 0.00578 -0.0710 0.1785 1.0000
6.750 1.1326 0.01233 0.00603 -0.0705 0.1680 1.0000
7.000 1.1417 0.01356 0.00691 -0.0677 0.1109 1.0000
7.250 1.1617 0.01405 0.00736 -0.0666 0.1016 1.0000
7.500 1.1825 0.01447 0.00775 -0.0656 0.0950 1.0000
7.750 1.2018 0.01494 0.00819 -0.0644 0.0880 1.0000
8.000 1.2196 0.01545 0.00864 -0.0630 0.0777 1.0000
8.250 1.2153 0.01681 0.00980 -0.0580 0.0340 1.0000
8.500 1.2301 0.01738 0.01037 -0.0562 0.0306 1.0000
8.750 1.2459 0.01795 0.01095 -0.0546 0.0291 1.0000
9.000 1.2617 0.01854 0.01156 -0.0532 0.0281 1.0000
9.250 1.2779 0.01915 0.01219 -0.0518 0.0275 1.0000
9.500 1.2932 0.01983 0.01288 -0.0505 0.0269 1.0000
9.750 1.3078 0.02059 0.01366 -0.0492 0.0265 1.0000
10.000 1.3217 0.02144 0.01454 -0.0480 0.0260 1.0000
10.250 1.3347 0.02239 0.01553 -0.0468 0.0256 1.0000
10.500 1.3468 0.02348 0.01665 -0.0457 0.0252 1.0000
10.750 1.3579 0.02472 0.01793 -0.0447 0.0248 1.0000
11.000 1.3688 0.02605 0.01929 -0.0438 0.0245 1.0000
11.250 1.3801 0.02740 0.02069 -0.0432 0.0243 1.0000
11.500 1.3907 0.02889 0.02222 -0.0426 0.0241 1.0000
11.750 1.4000 0.03052 0.02390 -0.0420 0.0238 1.0000
12.000 1.4083 0.03230 0.02574 -0.0416 0.0236 1.0000
12.250 1.4155 0.03424 0.02773 -0.0411 0.0234 1.0000
12.500 1.4217 0.03634 0.02988 -0.0408 0.0232 1.0000
12.750 1.4267 0.03858 0.03218 -0.0405 0.0230 1.0000
13.000 1.4306 0.04097 0.03463 -0.0403 0.0228 1.0000
13.250 1.4335 0.04351 0.03724 -0.0401 0.0226 1.0000
13.500 1.4353 0.04620 0.03999 -0.0400 0.0225 1.0000
13.750 1.4361 0.04900 0.04286 -0.0399 0.0223 1.0000
14.000 1.4361 0.05193 0.04585 -0.0398 0.0221 1.0000
14.250 1.4352 0.05501 0.04899 -0.0398 0.0220 1.0000
14.500 1.4332 0.05822 0.05228 -0.0399 0.0218 1.0000
14.750 1.4304 0.06155 0.05568 -0.0400 0.0217 1.0000
15.000 1.4273 0.06496 0.05915 -0.0401 0.0215 1.0000
15.250 1.4222 0.06867 0.06293 -0.0404 0.0213 1.0000
15.500 1.4174 0.07235 0.06669 -0.0406 0.0212 1.0000
15.750 1.4175 0.07546 0.06986 -0.0409 0.0211 1.0000
16.000 1.4154 0.07893 0.07340 -0.0413 0.0210 1.0000
16.250 1.4145 0.08222 0.07676 -0.0417 0.0209 1.0000
16.500 1.4108 0.08592 0.08053 -0.0422 0.0208 1.0000
16.750 1.4095 0.08933 0.08400 -0.0427 0.0207 1.0000
17.000 1.4054 0.09318 0.08792 -0.0433 0.0206 1.0000
17.250 1.4030 0.09680 0.09161 -0.0440 0.0205 1.0000
17.500 1.3988 0.10071 0.09559 -0.0448 0.0204 1.0000
17.750 1.3950 0.10457 0.09953 -0.0456 0.0203 1.0000
18.000 1.3912 0.10847 0.10350 -0.0465 0.0202 1.0000
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