GOE 775 AIRFOIL (goe775-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 775 AIRFOIL (goe775-il) Reynolds number: 1,000,000 Max Cl/Cd: 69.78 at α=8.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe775-il-1000000-n5.txt Download as CSV file: xf-goe775-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: GOE 775 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 -1.3278 0.08126 0.07646 -0.0368 1.0000 0.0440
-19.500 -1.3365 0.07705 0.07218 -0.0381 1.0000 0.0447
-19.250 -1.3433 0.07314 0.06821 -0.0392 1.0000 0.0454
-19.000 -1.3490 0.06940 0.06439 -0.0402 1.0000 0.0460
-18.750 -1.3535 0.06581 0.06073 -0.0412 1.0000 0.0467
-18.500 -1.3567 0.06243 0.05727 -0.0420 1.0000 0.0473
-18.250 -1.3593 0.05918 0.05395 -0.0427 1.0000 0.0479
-18.000 -1.3631 0.05586 0.05057 -0.0433 1.0000 0.0487
-17.750 -1.3651 0.05276 0.04742 -0.0438 1.0000 0.0495
-17.500 -1.3655 0.04990 0.04450 -0.0442 1.0000 0.0504
-17.250 -1.3643 0.04727 0.04181 -0.0444 1.0000 0.0513
-17.000 -1.3615 0.04484 0.03932 -0.0446 1.0000 0.0522
-16.750 -1.3578 0.04254 0.03697 -0.0447 1.0000 0.0530
-16.500 -1.3552 0.04019 0.03458 -0.0447 1.0000 0.0541
-16.250 -1.3510 0.03805 0.03239 -0.0446 1.0000 0.0553
-16.000 -1.3450 0.03611 0.03041 -0.0444 1.0000 0.0566
-15.750 -1.3375 0.03435 0.02860 -0.0441 1.0000 0.0578
-15.500 -1.3308 0.03257 0.02680 -0.0437 1.0000 0.0592
-15.250 -1.3235 0.03090 0.02511 -0.0432 1.0000 0.0609
-15.000 -1.3144 0.02944 0.02361 -0.0427 1.0000 0.0625
-14.750 -1.3039 0.02813 0.02226 -0.0421 1.0000 0.0640
-14.500 -1.2950 0.02674 0.02087 -0.0413 1.0000 0.0658
-14.250 -1.2843 0.02555 0.01965 -0.0405 1.0000 0.0677
-14.000 -1.2721 0.02452 0.01859 -0.0396 1.0000 0.0696
-13.750 -1.2605 0.02349 0.01755 -0.0385 1.0000 0.0714
-13.500 -1.2489 0.02252 0.01657 -0.0374 1.0000 0.0736
-13.250 -1.2358 0.02170 0.01574 -0.0362 1.0000 0.0757
-13.000 -1.2231 0.02094 0.01496 -0.0348 1.0000 0.0777
-12.750 -1.2120 0.02017 0.01420 -0.0331 1.0000 0.0801
-12.500 -1.2012 0.01954 0.01356 -0.0311 1.0000 0.0826
-12.250 -1.1892 0.01899 0.01299 -0.0292 0.9995 0.0845
-12.000 -1.1659 0.01828 0.01230 -0.0296 0.9963 0.0874
-11.750 -1.1401 0.01769 0.01170 -0.0303 0.9931 0.0902
-11.500 -1.1147 0.01718 0.01117 -0.0307 0.9882 0.0923
-11.250 -1.0912 0.01660 0.01061 -0.0308 0.9816 0.0951
-11.000 -1.0675 0.01609 0.01010 -0.0308 0.9755 0.0980
-10.750 -1.0448 0.01567 0.00966 -0.0304 0.9673 0.1005
-10.500 -1.0240 0.01520 0.00920 -0.0297 0.9591 0.1034
-10.250 -1.0045 0.01478 0.00877 -0.0286 0.9494 0.1064
-10.000 -0.9844 0.01443 0.00839 -0.0275 0.9407 0.1093
-9.750 -0.9654 0.01405 0.00801 -0.0261 0.9315 0.1127
-9.500 -0.9460 0.01369 0.00764 -0.0248 0.9234 0.1168
-9.250 -0.9257 0.01339 0.00731 -0.0236 0.9147 0.1205
-9.000 -0.9061 0.01304 0.00697 -0.0223 0.9069 0.1253
-8.750 -0.8850 0.01274 0.00667 -0.0212 0.8984 0.1300
-8.500 -0.8651 0.01243 0.00635 -0.0199 0.8893 0.1357
-8.250 -0.8438 0.01216 0.00609 -0.0187 0.8801 0.1418
-8.000 -0.8247 0.01188 0.00581 -0.0171 0.8688 0.1489
-7.750 -0.8042 0.01165 0.00559 -0.0158 0.8574 0.1557
-7.500 -0.7829 0.01141 0.00535 -0.0146 0.8447 0.1637
-7.250 -0.7602 0.01119 0.00512 -0.0136 0.8291 0.1711
-7.000 -0.7371 0.01100 0.00491 -0.0127 0.8101 0.1792
-6.750 -0.7145 0.01082 0.00469 -0.0117 0.7865 0.1870
-6.500 -0.6908 0.01071 0.00450 -0.0109 0.7630 0.1940
-6.250 -0.6673 0.01057 0.00432 -0.0101 0.7415 0.2010
-6.000 -0.6427 0.01046 0.00417 -0.0094 0.7240 0.2075
-5.750 -0.6176 0.01034 0.00402 -0.0089 0.7098 0.2135
-5.500 -0.5931 0.01022 0.00388 -0.0082 0.6961 0.2210
-5.250 -0.5670 0.01012 0.00376 -0.0078 0.6839 0.2269
-5.000 -0.5420 0.00999 0.00362 -0.0073 0.6727 0.2343
-4.750 -0.5160 0.00988 0.00351 -0.0069 0.6610 0.2419
-4.500 -0.4905 0.00976 0.00339 -0.0064 0.6501 0.2500
-4.250 -0.4642 0.00965 0.00328 -0.0060 0.6395 0.2581
-4.000 -0.4382 0.00957 0.00318 -0.0056 0.6283 0.2654
-3.750 -0.4120 0.00946 0.00308 -0.0052 0.6175 0.2748
-3.500 -0.3860 0.00938 0.00299 -0.0048 0.6066 0.2839
-3.250 -0.3595 0.00928 0.00291 -0.0045 0.5956 0.2940
-3.000 -0.3332 0.00922 0.00283 -0.0041 0.5840 0.3023
-2.750 -0.3066 0.00913 0.00276 -0.0038 0.5727 0.3131
-2.500 -0.2808 0.00904 0.00269 -0.0033 0.5607 0.3265
-2.250 -0.2546 0.00896 0.00262 -0.0030 0.5479 0.3405
-2.000 -0.2282 0.00891 0.00257 -0.0026 0.5344 0.3530
-1.750 -0.2022 0.00888 0.00253 -0.0022 0.5192 0.3634
-1.500 -0.1753 0.00887 0.00249 -0.0019 0.5044 0.3728
-1.250 -0.1486 0.00883 0.00246 -0.0016 0.4919 0.3819
-0.750 -0.0942 0.00882 0.00241 -0.0011 0.4695 0.3979
-0.250 -0.0403 0.00882 0.00239 -0.0006 0.4467 0.4168
0.000 -0.0138 0.00881 0.00238 -0.0002 0.4362 0.4271
0.250 0.0140 0.00881 0.00238 -0.0001 0.4280 0.4355
0.500 0.0406 0.00881 0.00239 0.0002 0.4179 0.4458
0.750 0.0680 0.00882 0.00240 0.0004 0.4089 0.4566
1.000 0.0945 0.00882 0.00241 0.0007 0.3989 0.4685
1.500 0.1488 0.00883 0.00245 0.0012 0.3828 0.4911
1.750 0.1755 0.00887 0.00249 0.0015 0.3736 0.5035
2.000 0.2024 0.00887 0.00252 0.0018 0.3644 0.5185
2.250 0.2284 0.00891 0.00257 0.0022 0.3537 0.5335
2.500 0.2549 0.00895 0.00262 0.0026 0.3418 0.5472
2.750 0.2811 0.00903 0.00268 0.0030 0.3279 0.5601
3.000 0.3068 0.00913 0.00276 0.0034 0.3142 0.5721
3.250 0.3334 0.00921 0.00283 0.0037 0.3034 0.5836
3.500 0.3597 0.00927 0.00291 0.0041 0.2949 0.5950
3.750 0.3863 0.00937 0.00299 0.0044 0.2852 0.6062
4.000 0.4122 0.00945 0.00308 0.0048 0.2759 0.6171
4.250 0.4386 0.00956 0.00318 0.0052 0.2665 0.6280
4.500 0.4645 0.00965 0.00328 0.0056 0.2589 0.6391
4.750 0.4908 0.00975 0.00338 0.0060 0.2509 0.6498
5.000 0.5163 0.00987 0.00350 0.0064 0.2427 0.6607
5.250 0.5423 0.00998 0.00362 0.0068 0.2352 0.6724
5.500 0.5673 0.01011 0.00375 0.0074 0.2276 0.6837
5.750 0.5934 0.01021 0.00387 0.0078 0.2219 0.6959
6.000 0.6180 0.01033 0.00402 0.0084 0.2144 0.7097
6.250 0.6431 0.01045 0.00417 0.0090 0.2083 0.7238
6.500 0.6677 0.01056 0.00432 0.0096 0.2018 0.7413
6.750 0.6912 0.01070 0.00450 0.0104 0.1947 0.7628
7.000 0.7150 0.01081 0.00468 0.0112 0.1881 0.7865
7.250 0.7375 0.01099 0.00490 0.0122 0.1801 0.8101
7.500 0.7609 0.01117 0.00511 0.0131 0.1724 0.8292
7.750 0.7835 0.01140 0.00534 0.0140 0.1648 0.8447
8.000 0.8051 0.01164 0.00557 0.0152 0.1568 0.8573
8.250 0.8256 0.01187 0.00580 0.0165 0.1499 0.8688
8.750 0.8660 0.01241 0.00634 0.0192 0.1367 0.8893
9.000 0.8858 0.01273 0.00666 0.0206 0.1308 0.8984
9.250 0.9070 0.01302 0.00695 0.0217 0.1260 0.9069
9.500 0.9267 0.01337 0.00730 0.0230 0.1212 0.9148
9.750 0.9469 0.01368 0.00763 0.0242 0.1174 0.9235
10.000 0.9665 0.01403 0.00799 0.0255 0.1133 0.9316
10.250 0.9853 0.01442 0.00838 0.0268 0.1097 0.9408
10.500 1.0055 0.01477 0.00875 0.0279 0.1069 0.9495
10.750 1.0252 0.01518 0.00918 0.0290 0.1039 0.9592
11.000 1.0458 0.01566 0.00965 0.0297 0.1009 0.9675
11.250 1.0687 0.01607 0.01008 0.0301 0.0984 0.9757
11.500 1.0927 0.01657 0.01058 0.0300 0.0956 0.9818
11.750 1.1162 0.01714 0.01114 0.0299 0.0928 0.9884
12.000 1.1417 0.01766 0.01168 0.0294 0.0906 0.9932
12.250 1.1676 0.01825 0.01227 0.0288 0.0879 0.9965
12.500 1.1911 0.01894 0.01295 0.0283 0.0850 0.9997
12.750 1.2018 0.01950 0.01352 0.0305 0.0831 1.0000
13.000 1.2133 0.02012 0.01415 0.0324 0.0807 1.0000
13.250 1.2249 0.02087 0.01490 0.0340 0.0782 1.0000
13.500 1.2374 0.02166 0.01569 0.0354 0.0762 1.0000
13.750 1.2509 0.02245 0.01650 0.0365 0.0742 1.0000
14.000 1.2629 0.02340 0.01747 0.0377 0.0720 1.0000
14.250 1.2742 0.02445 0.01853 0.0387 0.0700 1.0000
14.500 1.2867 0.02547 0.01957 0.0395 0.0682 1.0000
14.750 1.2978 0.02663 0.02075 0.0404 0.0663 1.0000
15.000 1.3070 0.02800 0.02213 0.0411 0.0645 1.0000
15.250 1.3173 0.02933 0.02350 0.0417 0.0629 1.0000
15.500 1.3268 0.03077 0.02497 0.0422 0.0612 1.0000
15.750 1.3343 0.03241 0.02663 0.0427 0.0595 1.0000
16.000 1.3408 0.03421 0.02846 0.0431 0.0581 1.0000
16.250 1.3485 0.03596 0.03025 0.0434 0.0568 1.0000
16.500 1.3548 0.03787 0.03221 0.0435 0.0556 1.0000
16.750 1.3595 0.03997 0.03435 0.0436 0.0544 1.0000
17.000 1.3623 0.04229 0.03671 0.0437 0.0532 1.0000
17.250 1.3657 0.04463 0.03910 0.0436 0.0523 1.0000
17.500 1.3687 0.04705 0.04158 0.0434 0.0514 1.0000
17.750 1.3701 0.04966 0.04425 0.0431 0.0505 1.0000
18.000 1.3701 0.05248 0.04712 0.0427 0.0496 1.0000
18.250 1.3684 0.05553 0.05024 0.0422 0.0487 1.0000
18.500 1.3648 0.05885 0.05361 0.0416 0.0480 1.0000
18.750 1.3620 0.06211 0.05694 0.0409 0.0473 1.0000
19.000 1.3590 0.06548 0.06039 0.0401 0.0467 1.0000
19.250 1.3547 0.06904 0.06402 0.0392 0.0460 1.0000
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