GOE 738 AIRFOIL (goe738-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: GOE 738 AIRFOIL (goe738-il) Reynolds number: 1,000,000 Max Cl/Cd: 102.91 at α=7.75° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-goe738-il-1000000.txt Download as CSV file: xf-goe738-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: GOE 738 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
------ -------- --------- --------- -------- -------- --------
-19.750 -1.1341 0.10775 0.10483 -0.0110 1.0000 0.0267
-19.500 -1.1542 0.10020 0.09716 -0.0158 1.0000 0.0268
-19.250 -1.1720 0.09326 0.09010 -0.0201 1.0000 0.0269
-19.000 -1.1897 0.08644 0.08316 -0.0244 1.0000 0.0270
-18.750 -1.2110 0.07941 0.07601 -0.0286 1.0000 0.0272
-18.500 -1.2317 0.07276 0.06923 -0.0324 1.0000 0.0273
-18.250 -1.2501 0.06655 0.06294 -0.0360 1.0000 0.0276
-18.000 -1.2641 0.06106 0.05735 -0.0391 1.0000 0.0278
-17.750 -1.2765 0.05596 0.05214 -0.0419 1.0000 0.0279
-17.500 -1.2856 0.05148 0.04757 -0.0443 1.0000 0.0281
-17.250 -1.2919 0.04753 0.04353 -0.0462 1.0000 0.0282
-17.000 -1.2957 0.04409 0.04000 -0.0477 1.0000 0.0284
-16.750 -1.2978 0.04101 0.03684 -0.0487 1.0000 0.0286
-16.500 -1.2972 0.03842 0.03418 -0.0493 1.0000 0.0289
-16.250 -1.2966 0.03602 0.03169 -0.0496 1.0000 0.0291
-16.000 -1.2950 0.03386 0.02946 -0.0494 1.0000 0.0293
-15.750 -1.2912 0.03205 0.02758 -0.0489 1.0000 0.0296
-15.500 -1.2861 0.03047 0.02592 -0.0482 1.0000 0.0298
-15.250 -1.2803 0.02904 0.02441 -0.0472 1.0000 0.0301
-15.000 -1.2737 0.02776 0.02306 -0.0460 1.0000 0.0304
-14.750 -1.2652 0.02669 0.02192 -0.0447 1.0000 0.0306
-14.500 -1.2561 0.02572 0.02088 -0.0431 1.0000 0.0308
-14.250 -1.2462 0.02484 0.01993 -0.0415 1.0000 0.0310
-14.000 -1.2450 0.02350 0.01852 -0.0388 1.0000 0.0314
-13.750 -1.2408 0.02242 0.01740 -0.0362 1.0000 0.0317
-13.500 -1.2315 0.02165 0.01660 -0.0338 1.0000 0.0321
-13.250 -1.2193 0.02103 0.01596 -0.0317 1.0000 0.0326
-13.000 -1.1899 0.02038 0.01522 -0.0329 0.9207 0.0330
-12.750 -1.1803 0.02010 0.01470 -0.0297 0.8576 0.0334
-12.250 -1.1532 0.01928 0.01365 -0.0250 0.8189 0.0342
-12.000 -1.1356 0.01884 0.01312 -0.0234 0.8063 0.0346
-11.750 -1.1164 0.01844 0.01263 -0.0219 0.7956 0.0350
-11.500 -1.0960 0.01809 0.01219 -0.0207 0.7857 0.0353
-11.250 -1.0793 0.01744 0.01147 -0.0189 0.7769 0.0359
-11.000 -1.0609 0.01687 0.01085 -0.0174 0.7684 0.0366
-10.750 -1.0398 0.01646 0.01040 -0.0162 0.7609 0.0372
-10.500 -1.0176 0.01608 0.00998 -0.0152 0.7533 0.0378
-10.250 -0.9950 0.01575 0.00959 -0.0142 0.7460 0.0385
-10.000 -0.9718 0.01541 0.00920 -0.0134 0.7396 0.0391
-9.750 -0.9481 0.01510 0.00883 -0.0125 0.7327 0.0397
-9.500 -0.9238 0.01485 0.00851 -0.0118 0.7260 0.0402
-9.250 -0.9026 0.01428 0.00792 -0.0106 0.7202 0.0414
-9.000 -0.8786 0.01394 0.00756 -0.0098 0.7137 0.0424
-8.750 -0.8539 0.01370 0.00726 -0.0091 0.7075 0.0435
-8.500 -0.8286 0.01342 0.00697 -0.0085 0.7020 0.0445
-8.250 -0.8030 0.01319 0.00669 -0.0080 0.6957 0.0454
-8.000 -0.7792 0.01282 0.00628 -0.0071 0.6895 0.0468
-7.750 -0.7539 0.01252 0.00598 -0.0065 0.6843 0.0484
-7.500 -0.7280 0.01229 0.00574 -0.0060 0.6784 0.0499
-7.250 -0.7017 0.01212 0.00550 -0.0055 0.6722 0.0513
-7.000 -0.6765 0.01180 0.00518 -0.0049 0.6666 0.0535
-6.750 -0.6503 0.01157 0.00496 -0.0044 0.6606 0.0558
-6.500 -0.6236 0.01141 0.00475 -0.0040 0.6547 0.0577
-6.250 -0.5978 0.01115 0.00448 -0.0035 0.6492 0.0604
-6.000 -0.5712 0.01093 0.00427 -0.0031 0.6433 0.0631
-5.750 -0.5441 0.01080 0.00409 -0.0027 0.6370 0.0654
-5.500 -0.5180 0.01055 0.00385 -0.0022 0.6310 0.0690
-5.250 -0.4910 0.01036 0.00367 -0.0018 0.6251 0.0724
-5.000 -0.4643 0.01018 0.00347 -0.0014 0.6190 0.0765
-4.750 -0.4376 0.00999 0.00328 -0.0010 0.6132 0.0814
-4.500 -0.4107 0.00979 0.00310 -0.0007 0.6074 0.0875
-4.250 -0.3841 0.00958 0.00292 -0.0002 0.6009 0.0965
-4.000 -0.3579 0.00936 0.00276 0.0002 0.5947 0.1130
-3.750 -0.3311 0.00914 0.00263 0.0006 0.5887 0.1325
-3.500 -0.3040 0.00899 0.00252 0.0009 0.5826 0.1475
-3.250 -0.2767 0.00888 0.00242 0.0012 0.5766 0.1594
-3.000 -0.2492 0.00873 0.00232 0.0014 0.5709 0.1717
-2.750 -0.2218 0.00862 0.00223 0.0017 0.5638 0.1835
-2.500 -0.1943 0.00851 0.00214 0.0020 0.5567 0.1964
-2.250 -0.1669 0.00838 0.00205 0.0022 0.5494 0.2119
-2.000 -0.1399 0.00827 0.00197 0.0026 0.5425 0.2316
-1.750 -0.1127 0.00809 0.00190 0.0029 0.5369 0.2572
-1.500 -0.0859 0.00792 0.00183 0.0032 0.5305 0.2882
-1.250 -0.0595 0.00777 0.00176 0.0036 0.5241 0.3236
-1.000 -0.0331 0.00754 0.00170 0.0040 0.5188 0.3703
-0.750 -0.0077 0.00729 0.00164 0.0046 0.5124 0.4303
-0.500 0.0171 0.00705 0.00160 0.0053 0.5057 0.4945
-0.250 0.0427 0.00683 0.00157 0.0059 0.4999 0.5524
0.000 0.0685 0.00669 0.00156 0.0065 0.4928 0.6011
0.250 0.0940 0.00656 0.00156 0.0072 0.4867 0.6451
0.500 0.1197 0.00643 0.00157 0.0078 0.4816 0.6903
0.750 0.1456 0.00635 0.00159 0.0085 0.4762 0.7282
1.000 0.1721 0.00634 0.00162 0.0090 0.4705 0.7546
1.250 0.1994 0.00629 0.00165 0.0094 0.4660 0.7773
1.500 0.2266 0.00627 0.00168 0.0098 0.4607 0.7977
1.750 0.2537 0.00628 0.00171 0.0102 0.4551 0.8170
2.000 0.2813 0.00627 0.00176 0.0105 0.4504 0.8359
2.250 0.3090 0.00626 0.00180 0.0108 0.4451 0.8566
2.500 0.3370 0.00627 0.00185 0.0110 0.4395 0.8773
2.750 0.3665 0.00630 0.00192 0.0109 0.4341 0.8971
3.250 0.4424 0.00646 0.00214 0.0071 0.4204 0.9409
3.750 0.5207 0.00674 0.00238 0.0027 0.4044 0.9617
4.000 0.5538 0.00689 0.00250 0.0018 0.3962 0.9686
4.250 0.5913 0.00706 0.00262 -0.0002 0.3848 0.9712
4.500 0.6274 0.00720 0.00273 -0.0018 0.3739 0.9744
4.750 0.6591 0.00738 0.00286 -0.0025 0.3619 0.9793
5.000 0.6941 0.00758 0.00299 -0.0041 0.3462 0.9818
5.250 0.7306 0.00783 0.00313 -0.0060 0.3235 0.9836
5.500 0.7657 0.00815 0.00332 -0.0077 0.2993 0.9859
5.750 0.8000 0.00845 0.00352 -0.0092 0.2791 0.9886
6.000 0.8328 0.00875 0.00374 -0.0104 0.2638 0.9915
6.500 0.9032 0.00921 0.00410 -0.0138 0.2436 0.9951
6.750 0.9386 0.00945 0.00429 -0.0156 0.2354 0.9971
7.000 0.9742 0.00961 0.00445 -0.0174 0.2299 0.9988
7.250 1.0072 0.00985 0.00465 -0.0187 0.2229 1.0000
7.500 1.0293 0.01004 0.00484 -0.0177 0.2176 1.0000
7.750 1.0517 0.01022 0.00501 -0.0167 0.2131 1.0000
8.000 1.0735 0.01046 0.00524 -0.0157 0.2078 1.0000
8.250 1.0953 0.01070 0.00547 -0.0147 0.2029 1.0000
8.500 1.1180 0.01088 0.00566 -0.0138 0.1983 1.0000
8.750 1.1393 0.01115 0.00591 -0.0128 0.1919 1.0000
9.000 1.1609 0.01140 0.00616 -0.0118 0.1859 1.0000
9.250 1.1818 0.01169 0.00642 -0.0107 0.1772 1.0000
9.500 1.2019 0.01203 0.00672 -0.0095 0.1663 1.0000
9.750 1.2191 0.01252 0.00711 -0.0079 0.1496 1.0000
10.000 1.2330 0.01318 0.00765 -0.0060 0.1318 1.0000
10.250 1.2465 0.01381 0.00820 -0.0039 0.1192 1.0000
10.750 1.2709 0.01503 0.00934 0.0005 0.1006 1.0000
11.000 1.2810 0.01568 0.00996 0.0029 0.0922 1.0000
11.250 1.2829 0.01638 0.01063 0.0067 0.0849 1.0000
11.750 1.2860 0.01829 0.01253 0.0125 0.0740 1.0000
12.000 1.2923 0.01947 0.01370 0.0140 0.0705 1.0000
12.250 1.3011 0.02061 0.01487 0.0151 0.0677 1.0000
12.500 1.3104 0.02180 0.01608 0.0161 0.0657 1.0000
12.750 1.3178 0.02321 0.01750 0.0170 0.0638 1.0000
13.000 1.3250 0.02467 0.01899 0.0177 0.0623 1.0000
13.250 1.3319 0.02622 0.02058 0.0184 0.0611 1.0000
13.500 1.3418 0.02755 0.02197 0.0189 0.0604 1.0000
13.750 1.3506 0.02899 0.02347 0.0193 0.0595 1.0000
14.000 1.3573 0.03066 0.02519 0.0198 0.0587 1.0000
14.250 1.3631 0.03243 0.02699 0.0201 0.0576 1.0000
14.500 1.3667 0.03443 0.02903 0.0204 0.0566 1.0000
14.750 1.3691 0.03659 0.03123 0.0207 0.0558 1.0000
15.000 1.3691 0.03901 0.03372 0.0208 0.0549 1.0000
15.250 1.3679 0.04162 0.03638 0.0209 0.0541 1.0000
15.500 1.3744 0.04354 0.03837 0.0208 0.0537 1.0000
15.750 1.3803 0.04557 0.04046 0.0207 0.0532 1.0000
16.000 1.3835 0.04794 0.04290 0.0205 0.0527 1.0000
16.250 1.3876 0.05023 0.04524 0.0203 0.0519 1.0000
16.500 1.3902 0.05272 0.04780 0.0199 0.0512 1.0000
16.750 1.3906 0.05552 0.05065 0.0195 0.0505 1.0000
17.000 1.3904 0.05840 0.05358 0.0189 0.0499 1.0000
17.250 1.3884 0.06154 0.05677 0.0183 0.0493 1.0000
17.500 1.3836 0.06508 0.06038 0.0175 0.0487 1.0000
17.750 1.3761 0.06900 0.06436 0.0166 0.0479 1.0000
18.000 1.3762 0.07200 0.06743 0.0158 0.0475 1.0000
18.250 1.3808 0.07450 0.07001 0.0152 0.0469 1.0000
18.500 1.3821 0.07743 0.07300 0.0144 0.0464 1.0000
18.750 1.3809 0.08069 0.07633 0.0135 0.0458 1.0000
19.000 1.3796 0.08399 0.07969 0.0125 0.0451 1.0000
19.250 1.3779 0.08737 0.08313 0.0114 0.0445 1.0000
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