GOE 648 AIRFOIL (goe648-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: GOE 648 AIRFOIL (goe648-il) Reynolds number: 1,000,000 Max Cl/Cd: 104.31 at α=8° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-goe648-il-1000000.txt Download as CSV file: xf-goe648-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: GOE 648 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 = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-18.750 -0.7536 0.11996 0.11747 -0.0491 1.0000 0.0186
-18.500 -0.7967 0.10831 0.10566 -0.0556 1.0000 0.0188
-18.250 -0.8228 0.10026 0.09751 -0.0601 1.0000 0.0188
-18.000 -0.8524 0.09176 0.08889 -0.0649 1.0000 0.0189
-17.750 -0.8845 0.08319 0.08019 -0.0699 1.0000 0.0190
-17.500 -0.9145 0.07540 0.07228 -0.0743 1.0000 0.0190
-17.250 -0.9449 0.06774 0.06450 -0.0787 1.0000 0.0191
-17.000 -0.9755 0.06027 0.05690 -0.0830 1.0000 0.0191
-16.750 -0.9965 0.05405 0.05055 -0.0866 1.0000 0.0191
-16.500 -1.0217 0.04750 0.04387 -0.0905 1.0000 0.0191
-16.250 -1.0460 0.04147 0.03770 -0.0939 1.0000 0.0193
-16.000 -1.0624 0.03691 0.03303 -0.0961 1.0000 0.0194
-15.750 -1.0781 0.03304 0.02905 -0.0972 1.0000 0.0196
-15.500 -1.0894 0.03035 0.02629 -0.0968 1.0000 0.0198
-15.250 -1.0990 0.02846 0.02433 -0.0950 1.0000 0.0200
-15.000 -1.1137 0.02697 0.02276 -0.0915 1.0000 0.0201
-14.750 -1.1339 0.02602 0.02175 -0.0856 1.0000 0.0202
-14.500 -1.1286 0.02527 0.02094 -0.0833 0.9989 0.0205
-14.250 -1.1018 0.02445 0.02007 -0.0844 0.9969 0.0210
-14.000 -1.0735 0.02363 0.01919 -0.0857 0.9949 0.0214
-13.750 -1.0442 0.02285 0.01833 -0.0871 0.9934 0.0219
-13.500 -1.0175 0.02213 0.01753 -0.0877 0.9912 0.0222
-13.250 -0.9943 0.02098 0.01631 -0.0881 0.9878 0.0228
-13.000 -0.9670 0.02008 0.01538 -0.0890 0.9854 0.0233
-12.750 -0.9364 0.01947 0.01474 -0.0902 0.9837 0.0239
-12.500 -0.9046 0.01886 0.01410 -0.0915 0.9825 0.0244
-12.250 -0.8703 0.01832 0.01350 -0.0932 0.9814 0.0251
-12.000 -0.8443 0.01787 0.01299 -0.0929 0.9768 0.0256
-11.750 -0.8152 0.01707 0.01214 -0.0938 0.9734 0.0264
-11.500 -0.7837 0.01637 0.01143 -0.0949 0.9714 0.0272
-11.250 -0.7503 0.01586 0.01089 -0.0963 0.9699 0.0279
-11.000 -0.7162 0.01537 0.01037 -0.0977 0.9688 0.0286
-10.750 -0.6880 0.01496 0.00992 -0.0978 0.9651 0.0293
-10.500 -0.6603 0.01445 0.00935 -0.0979 0.9606 0.0300
-10.250 -0.6284 0.01382 0.00872 -0.0990 0.9578 0.0311
-10.000 -0.5945 0.01339 0.00827 -0.1004 0.9554 0.0320
-9.750 -0.5607 0.01302 0.00787 -0.1016 0.9522 0.0330
-9.500 -0.5353 0.01273 0.00753 -0.1010 0.9445 0.0337
-9.250 -0.5034 0.01215 0.00692 -0.1019 0.9397 0.0349
-9.000 -0.4766 0.01180 0.00656 -0.1017 0.9312 0.0360
-8.750 -0.4449 0.01149 0.00621 -0.1024 0.9232 0.0372
-8.500 -0.4180 0.01127 0.00593 -0.1020 0.9123 0.0383
-8.250 -0.3912 0.01089 0.00550 -0.1017 0.9024 0.0397
-8.000 -0.3654 0.01063 0.00520 -0.1011 0.8915 0.0410
-7.750 -0.3393 0.01044 0.00497 -0.1006 0.8813 0.0426
-7.250 -0.2890 0.00999 0.00444 -0.0991 0.8594 0.0463
-7.000 -0.2634 0.00984 0.00424 -0.0984 0.8492 0.0484
-6.750 -0.2384 0.00964 0.00402 -0.0976 0.8396 0.0513
-6.500 -0.2127 0.00951 0.00386 -0.0969 0.8304 0.0542
-6.250 -0.1877 0.00935 0.00367 -0.0961 0.8200 0.0576
-6.000 -0.1620 0.00925 0.00355 -0.0954 0.8099 0.0612
-5.750 -0.1367 0.00913 0.00339 -0.0946 0.7995 0.0650
-5.500 -0.1110 0.00903 0.00328 -0.0939 0.7887 0.0686
-5.250 -0.0856 0.00894 0.00314 -0.0932 0.7775 0.0719
-5.000 -0.0606 0.00882 0.00300 -0.0923 0.7652 0.0755
-4.750 -0.0348 0.00876 0.00289 -0.0916 0.7523 0.0785
-4.500 -0.0100 0.00865 0.00274 -0.0908 0.7391 0.0821
-4.250 0.0147 0.00856 0.00261 -0.0899 0.7245 0.0859
-4.000 0.0395 0.00853 0.00250 -0.0890 0.7076 0.0887
-3.750 0.0637 0.00845 0.00237 -0.0880 0.6897 0.0932
-3.500 0.0881 0.00839 0.00227 -0.0870 0.6722 0.0982
-3.000 0.1370 0.00828 0.00210 -0.0852 0.6389 0.1156
-2.750 0.1611 0.00817 0.00203 -0.0842 0.6238 0.1379
-2.500 0.1848 0.00804 0.00196 -0.0833 0.6091 0.1702
-2.250 0.2085 0.00792 0.00191 -0.0823 0.5941 0.2058
-2.000 0.2323 0.00784 0.00188 -0.0813 0.5792 0.2411
-1.750 0.2564 0.00778 0.00186 -0.0804 0.5646 0.2719
-1.500 0.2814 0.00772 0.00184 -0.0796 0.5506 0.2997
-1.250 0.3057 0.00767 0.00183 -0.0787 0.5361 0.3314
-1.000 0.3295 0.00761 0.00183 -0.0778 0.5207 0.3697
-0.750 0.3527 0.00754 0.00184 -0.0767 0.5036 0.4169
-0.500 0.3756 0.00752 0.00187 -0.0756 0.4833 0.4662
-0.250 0.3978 0.00756 0.00192 -0.0743 0.4581 0.5077
0.250 0.4415 0.00782 0.00207 -0.0716 0.3970 0.5714
0.500 0.4633 0.00799 0.00216 -0.0702 0.3701 0.5968
0.750 0.4858 0.00810 0.00225 -0.0690 0.3529 0.6218
1.000 0.5088 0.00815 0.00234 -0.0679 0.3416 0.6535
1.250 0.5306 0.00819 0.00245 -0.0665 0.3320 0.6954
1.500 0.5534 0.00821 0.00254 -0.0652 0.3252 0.7349
1.750 0.5756 0.00828 0.00265 -0.0639 0.3181 0.7679
2.000 0.5978 0.00829 0.00275 -0.0625 0.3134 0.8066
2.250 0.6196 0.00825 0.00283 -0.0610 0.3094 0.8474
2.500 0.6518 0.00824 0.00299 -0.0617 0.3041 0.9152
2.750 0.7292 0.00854 0.00326 -0.0725 0.2970 0.9550
3.000 0.7821 0.00870 0.00340 -0.0779 0.2930 0.9780
3.250 0.8181 0.00889 0.00354 -0.0796 0.2887 0.9943
3.500 0.8594 0.00911 0.00370 -0.0825 0.2839 1.0000
3.750 0.8792 0.00927 0.00383 -0.0808 0.2803 1.0000
4.000 0.9015 0.00934 0.00390 -0.0796 0.2782 1.0000
4.250 0.9234 0.00944 0.00399 -0.0783 0.2755 1.0000
4.500 0.9450 0.00956 0.00409 -0.0769 0.2721 1.0000
4.750 0.9659 0.00972 0.00422 -0.0755 0.2689 1.0000
5.000 0.9859 0.00991 0.00438 -0.0739 0.2649 1.0000
5.250 1.0079 0.01004 0.00450 -0.0726 0.2624 1.0000
5.500 1.0304 0.01014 0.00462 -0.0715 0.2601 1.0000
5.750 1.0524 0.01027 0.00474 -0.0703 0.2570 1.0000
6.000 1.0734 0.01043 0.00488 -0.0689 0.2534 1.0000
6.250 1.0919 0.01062 0.00505 -0.0670 0.2499 1.0000
6.500 1.1106 0.01080 0.00521 -0.0652 0.2464 1.0000
6.750 1.1318 0.01091 0.00534 -0.0638 0.2438 1.0000
7.000 1.1523 0.01105 0.00548 -0.0624 0.2402 1.0000
7.250 1.1718 0.01124 0.00565 -0.0608 0.2364 1.0000
7.500 1.1897 0.01151 0.00588 -0.0589 0.2316 1.0000
7.750 1.2120 0.01163 0.00603 -0.0579 0.2281 1.0000
8.000 1.2329 0.01182 0.00621 -0.0566 0.2239 1.0000
8.250 1.2523 0.01206 0.00643 -0.0552 0.2194 1.0000
8.500 1.2718 0.01232 0.00668 -0.0538 0.2150 1.0000
8.750 1.2931 0.01252 0.00690 -0.0527 0.2113 1.0000
9.000 1.3128 0.01278 0.00715 -0.0513 0.2067 1.0000
9.250 1.3308 0.01313 0.00747 -0.0498 0.2014 1.0000
9.500 1.3517 0.01337 0.00773 -0.0487 0.1983 1.0000
9.750 1.3712 0.01367 0.00803 -0.0475 0.1936 1.0000
10.000 1.3888 0.01406 0.00839 -0.0460 0.1885 1.0000
10.250 1.4080 0.01440 0.00874 -0.0448 0.1847 1.0000
10.500 1.4269 0.01475 0.00910 -0.0436 0.1808 1.0000
10.750 1.4441 0.01519 0.00953 -0.0422 0.1761 1.0000
11.000 1.4608 0.01566 0.01000 -0.0408 0.1719 1.0000
11.250 1.4796 0.01604 0.01041 -0.0396 0.1685 1.0000
11.500 1.4968 0.01651 0.01088 -0.0384 0.1650 1.0000
11.750 1.5119 0.01710 0.01146 -0.0369 0.1608 1.0000
12.000 1.5287 0.01761 0.01200 -0.0357 0.1575 1.0000
12.250 1.5460 0.01811 0.01253 -0.0346 0.1548 1.0000
12.500 1.5615 0.01871 0.01314 -0.0333 0.1511 1.0000
12.750 1.5749 0.01945 0.01388 -0.0319 0.1473 1.0000
13.000 1.5905 0.02009 0.01454 -0.0307 0.1439 1.0000
13.250 1.6058 0.02075 0.01523 -0.0296 0.1403 1.0000
13.500 1.6184 0.02159 0.01608 -0.0283 0.1364 1.0000
13.750 1.6304 0.02249 0.01700 -0.0270 0.1324 1.0000
14.000 1.6448 0.02326 0.01780 -0.0261 0.1290 1.0000
14.250 1.6541 0.02439 0.01891 -0.0247 0.1233 1.0000
14.500 1.6653 0.02541 0.01997 -0.0236 0.1200 1.0000
14.750 1.6757 0.02652 0.02110 -0.0225 0.1149 1.0000
15.000 1.6815 0.02800 0.02257 -0.0212 0.1095 1.0000
15.250 1.6896 0.02935 0.02394 -0.0201 0.1038 1.0000
15.500 1.6920 0.03118 0.02576 -0.0189 0.0969 1.0000
15.750 1.6909 0.03339 0.02795 -0.0176 0.0888 1.0000
16.000 1.6836 0.03623 0.03075 -0.0164 0.0777 1.0000
16.250 1.6760 0.03926 0.03378 -0.0154 0.0702 1.0000
16.500 1.6727 0.04204 0.03660 -0.0149 0.0664 1.0000
16.750 1.6649 0.04537 0.03996 -0.0145 0.0625 1.0000
17.000 1.6619 0.04832 0.04298 -0.0143 0.0607 1.0000
17.250 1.6558 0.05172 0.04645 -0.0144 0.0590 1.0000
17.500 1.6463 0.05559 0.05039 -0.0146 0.0573 1.0000
17.750 1.6356 0.05970 0.05458 -0.0150 0.0557 1.0000
18.000 1.6300 0.06330 0.05828 -0.0155 0.0550 1.0000
18.250 1.6212 0.06737 0.06245 -0.0162 0.0544 1.0000
18.500 1.6089 0.07193 0.06712 -0.0171 0.0536 1.0000
18.750 1.5943 0.07692 0.07220 -0.0182 0.0528 1.0000
19.000 1.5784 0.08219 0.07758 -0.0196 0.0523 1.0000
19.250 1.5596 0.08792 0.08342 -0.0212 0.0518 1.0000
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