GOE 410 AIRFOIL (goe410-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: GOE 410 AIRFOIL (goe410-il) Reynolds number: 500,000 Max Cl/Cd: 62.4 at α=9.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-goe410-il-500000.txt Download as CSV file: xf-goe410-il-500000.csv |
XFOIL Version 6.96
Calculated polar for: GOE 410 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
------ -------- --------- --------- -------- -------- --------
-19.000 -1.2681 0.08888 0.08426 -0.0157 1.0000 0.0451
-18.750 -1.2754 0.08446 0.07982 -0.0177 1.0000 0.0459
-18.500 -1.2823 0.08009 0.07541 -0.0197 1.0000 0.0467
-18.250 -1.2887 0.07584 0.07111 -0.0216 1.0000 0.0477
-18.000 -1.2928 0.07197 0.06715 -0.0232 1.0000 0.0487
-17.750 -1.2956 0.06836 0.06344 -0.0246 1.0000 0.0499
-17.500 -1.3002 0.06464 0.05966 -0.0260 1.0000 0.0511
-17.250 -1.3054 0.06089 0.05589 -0.0275 1.0000 0.0523
-17.000 -1.3082 0.05751 0.05246 -0.0287 1.0000 0.0537
-16.750 -1.3081 0.05455 0.04941 -0.0296 1.0000 0.0553
-16.500 -1.3088 0.05159 0.04637 -0.0304 1.0000 0.0569
-16.250 -1.3119 0.04847 0.04324 -0.0313 1.0000 0.0585
-16.000 -1.3099 0.04590 0.04062 -0.0319 1.0000 0.0604
-15.750 -1.3043 0.04373 0.03834 -0.0324 1.0000 0.0627
-15.500 -1.3051 0.04100 0.03560 -0.0329 1.0000 0.0645
-15.250 -1.3009 0.03877 0.03334 -0.0333 1.0000 0.0665
-15.000 -1.2933 0.03691 0.03139 -0.0336 1.0000 0.0687
-14.750 -1.2862 0.03506 0.02945 -0.0337 1.0000 0.0707
-14.500 -1.2826 0.03298 0.02738 -0.0338 1.0000 0.0726
-14.250 -1.2741 0.03138 0.02574 -0.0337 1.0000 0.0746
-14.000 -1.2633 0.03002 0.02429 -0.0336 1.0000 0.0766
-13.750 -1.2527 0.02872 0.02289 -0.0332 1.0000 0.0783
-13.500 -1.2475 0.02709 0.02128 -0.0326 1.0000 0.0802
-13.250 -1.2380 0.02587 0.02003 -0.0319 1.0000 0.0819
-13.000 -1.2264 0.02486 0.01897 -0.0312 1.0000 0.0837
-12.750 -1.2141 0.02395 0.01799 -0.0303 1.0000 0.0853
-12.500 -1.2002 0.02322 0.01716 -0.0293 1.0000 0.0866
-12.250 -1.1944 0.02204 0.01600 -0.0275 1.0000 0.0885
-12.000 -1.1842 0.02126 0.01521 -0.0258 1.0000 0.0902
-11.750 -1.1715 0.02067 0.01460 -0.0241 1.0000 0.0919
-11.500 -1.1582 0.02015 0.01403 -0.0223 1.0000 0.0935
-11.250 -1.1440 0.01970 0.01353 -0.0204 1.0000 0.0950
-11.000 -1.1278 0.01930 0.01306 -0.0187 1.0000 0.0962
-10.750 -1.1150 0.01854 0.01232 -0.0168 1.0000 0.0983
-10.500 -1.0974 0.01803 0.01182 -0.0154 1.0000 0.1001
-10.250 -1.0775 0.01763 0.01142 -0.0143 1.0000 0.1020
-10.000 -1.0566 0.01727 0.01103 -0.0132 1.0000 0.1039
-9.750 -1.0350 0.01693 0.01064 -0.0123 1.0000 0.1056
-9.500 -1.0143 0.01650 0.01017 -0.0112 1.0000 0.1073
-9.250 -0.9953 0.01595 0.00967 -0.0099 1.0000 0.1098
-9.000 -0.9733 0.01561 0.00934 -0.0090 1.0000 0.1124
-8.750 -0.9503 0.01533 0.00905 -0.0082 1.0000 0.1150
-8.500 -0.9265 0.01511 0.00880 -0.0075 1.0000 0.1174
-8.250 -0.9064 0.01462 0.00834 -0.0062 1.0000 0.1204
-8.000 -0.8852 0.01423 0.00799 -0.0051 1.0000 0.1233
-7.750 -0.8633 0.01394 0.00770 -0.0041 1.0000 0.1261
-7.500 -0.8414 0.01368 0.00743 -0.0029 1.0000 0.1289
-7.250 -0.8123 0.01330 0.00704 -0.0034 0.9930 0.1325
-7.000 -0.7717 0.01281 0.00662 -0.0063 0.9757 0.1377
-6.750 -0.7281 0.01252 0.00629 -0.0095 0.9527 0.1428
-6.500 -0.6926 0.01211 0.00586 -0.0110 0.9177 0.1485
-6.250 -0.6676 0.01186 0.00553 -0.0103 0.8798 0.1538
-6.000 -0.6433 0.01175 0.00528 -0.0093 0.8490 0.1584
-5.750 -0.6205 0.01146 0.00493 -0.0082 0.8239 0.1652
-5.500 -0.5962 0.01124 0.00465 -0.0073 0.8020 0.1722
-5.250 -0.5719 0.01097 0.00436 -0.0066 0.7810 0.1816
-5.000 -0.5476 0.01065 0.00406 -0.0058 0.7601 0.1961
-4.750 -0.5247 0.01016 0.00372 -0.0050 0.7389 0.2359
-4.500 -0.5012 0.00973 0.00347 -0.0043 0.7175 0.2900
-4.250 -0.4756 0.00952 0.00331 -0.0037 0.6958 0.3224
-4.000 -0.4494 0.00938 0.00317 -0.0032 0.6751 0.3445
-3.750 -0.4225 0.00930 0.00307 -0.0028 0.6562 0.3623
-3.500 -0.3951 0.00926 0.00299 -0.0025 0.6395 0.3776
-3.250 -0.3677 0.00923 0.00292 -0.0022 0.6246 0.3911
-3.000 -0.3399 0.00919 0.00287 -0.0020 0.6111 0.4023
-2.750 -0.3116 0.00920 0.00282 -0.0018 0.5998 0.4130
-2.500 -0.2839 0.00918 0.00279 -0.0016 0.5894 0.4228
-2.250 -0.2554 0.00919 0.00276 -0.0014 0.5796 0.4331
-2.000 -0.2275 0.00919 0.00274 -0.0012 0.5694 0.4427
-1.750 -0.1990 0.00919 0.00273 -0.0010 0.5598 0.4524
-1.500 -0.1709 0.00920 0.00272 -0.0008 0.5510 0.4616
-1.250 -0.1422 0.00924 0.00271 -0.0007 0.5434 0.4694
-1.000 -0.1140 0.00919 0.00271 -0.0006 0.5357 0.4776
-0.750 -0.0856 0.00927 0.00270 -0.0004 0.5278 0.4858
-0.500 -0.0570 0.00921 0.00269 -0.0003 0.5205 0.4924
-0.250 -0.0286 0.00921 0.00268 -0.0001 0.5126 0.4991
0.000 0.0000 0.00926 0.00268 0.0000 0.5057 0.5057
0.250 0.0286 0.00921 0.00268 0.0001 0.4991 0.5126
0.500 0.0570 0.00921 0.00269 0.0003 0.4924 0.5204
0.750 0.0856 0.00927 0.00270 0.0004 0.4858 0.5278
1.000 0.1140 0.00919 0.00271 0.0005 0.4775 0.5358
1.250 0.1422 0.00924 0.00271 0.0007 0.4694 0.5434
1.500 0.1709 0.00920 0.00272 0.0008 0.4616 0.5509
1.750 0.1990 0.00920 0.00273 0.0010 0.4524 0.5597
2.000 0.2275 0.00919 0.00274 0.0012 0.4427 0.5694
2.250 0.2554 0.00918 0.00276 0.0014 0.4332 0.5797
2.500 0.2839 0.00918 0.00279 0.0016 0.4228 0.5894
2.750 0.3117 0.00920 0.00282 0.0018 0.4130 0.5998
3.000 0.3400 0.00919 0.00287 0.0020 0.4023 0.6111
3.250 0.3677 0.00923 0.00292 0.0022 0.3911 0.6246
3.500 0.3951 0.00926 0.00299 0.0025 0.3777 0.6395
3.750 0.4225 0.00930 0.00307 0.0028 0.3623 0.6562
4.000 0.4494 0.00938 0.00317 0.0032 0.3445 0.6752
4.250 0.4757 0.00952 0.00331 0.0037 0.3223 0.6958
4.500 0.5012 0.00973 0.00347 0.0042 0.2899 0.7174
4.750 0.5247 0.01016 0.00372 0.0050 0.2359 0.7389
5.000 0.5477 0.01065 0.00406 0.0058 0.1961 0.7600
5.250 0.5719 0.01096 0.00436 0.0066 0.1817 0.7810
5.500 0.5963 0.01124 0.00465 0.0073 0.1722 0.8020
5.750 0.6205 0.01146 0.00493 0.0082 0.1651 0.8239
6.000 0.6433 0.01175 0.00528 0.0093 0.1584 0.8488
6.250 0.6676 0.01186 0.00553 0.0103 0.1538 0.8797
6.500 0.6927 0.01211 0.00586 0.0110 0.1485 0.9177
6.750 0.7282 0.01252 0.00629 0.0094 0.1428 0.9528
7.000 0.7718 0.01281 0.00662 0.0062 0.1378 0.9758
7.250 0.8123 0.01329 0.00704 0.0034 0.1325 0.9930
7.500 0.8414 0.01368 0.00743 0.0029 0.1289 1.0000
7.750 0.8633 0.01394 0.00770 0.0041 0.1261 1.0000
8.000 0.8852 0.01424 0.00799 0.0051 0.1234 1.0000
8.250 0.9064 0.01462 0.00834 0.0062 0.1205 1.0000
8.500 0.9265 0.01511 0.00880 0.0075 0.1174 1.0000
8.750 0.9503 0.01532 0.00905 0.0082 0.1150 1.0000
9.000 0.9734 0.01560 0.00933 0.0090 0.1123 1.0000
9.250 0.9953 0.01595 0.00966 0.0099 0.1098 1.0000
9.500 1.0144 0.01649 0.01017 0.0112 0.1073 1.0000
9.750 1.0350 0.01692 0.01063 0.0123 0.1056 1.0000
10.000 1.0567 0.01726 0.01102 0.0132 0.1039 1.0000
10.250 1.0775 0.01763 0.01142 0.0143 0.1020 1.0000
10.500 1.0974 0.01803 0.01183 0.0154 0.1001 1.0000
10.750 1.1151 0.01853 0.01232 0.0167 0.0982 1.0000
11.000 1.1279 0.01930 0.01306 0.0187 0.0962 1.0000
11.250 1.1442 0.01969 0.01352 0.0203 0.0950 1.0000
11.500 1.1586 0.02014 0.01403 0.0222 0.0935 1.0000
11.750 1.1719 0.02066 0.01459 0.0241 0.0919 1.0000
12.000 1.1847 0.02124 0.01519 0.0257 0.0901 1.0000
12.250 1.1948 0.02203 0.01599 0.0275 0.0885 1.0000
12.500 1.2005 0.02321 0.01715 0.0293 0.0866 1.0000
12.750 1.2146 0.02394 0.01798 0.0302 0.0853 1.0000
13.000 1.2270 0.02483 0.01894 0.0311 0.0836 1.0000
13.250 1.2385 0.02585 0.02001 0.0318 0.0819 1.0000
13.500 1.2482 0.02707 0.02125 0.0325 0.0801 1.0000
13.750 1.2532 0.02871 0.02288 0.0332 0.0783 1.0000
14.000 1.2642 0.02999 0.02426 0.0335 0.0765 1.0000
14.250 1.2748 0.03136 0.02571 0.0336 0.0746 1.0000
14.500 1.2835 0.03295 0.02734 0.0337 0.0725 1.0000
14.750 1.2874 0.03500 0.02939 0.0336 0.0707 1.0000
15.000 1.2945 0.03685 0.03133 0.0335 0.0686 1.0000
15.250 1.3023 0.03870 0.03327 0.0332 0.0665 1.0000
15.500 1.3064 0.04095 0.03554 0.0328 0.0644 1.0000
15.750 1.3062 0.04363 0.03824 0.0323 0.0626 1.0000
16.000 1.3114 0.04584 0.04056 0.0318 0.0604 1.0000
16.250 1.3136 0.04840 0.04316 0.0311 0.0584 1.0000
16.500 1.3105 0.05152 0.04630 0.0303 0.0569 1.0000
16.750 1.3102 0.05444 0.04930 0.0294 0.0552 1.0000
17.000 1.3100 0.05744 0.05238 0.0285 0.0535 1.0000
17.250 1.3075 0.06078 0.05577 0.0273 0.0522 1.0000
17.500 1.3015 0.06462 0.05963 0.0258 0.0510 1.0000
17.750 1.2982 0.06818 0.06327 0.0245 0.0499 1.0000
18.000 1.2953 0.07180 0.06698 0.0231 0.0488 1.0000
18.250 1.2909 0.07571 0.07097 0.0214 0.0477 1.0000
18.500 1.2853 0.07985 0.07517 0.0196 0.0468 1.0000
18.750 1.2783 0.08424 0.07959 0.0176 0.0460 1.0000
19.000 1.2704 0.08873 0.08411 0.0156 0.0451 1.0000
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