GOE 703 AIRFOIL (goe703-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: GOE 703 AIRFOIL (goe703-il) Reynolds number: 1,000,000 Max Cl/Cd: 75.51 at α=8° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-goe703-il-1000000.txt Download as CSV file: xf-goe703-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: GOE 703 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 -1.0395 0.07966 0.07579 -0.0760 1.0000 0.0286
-19.500 -1.0481 0.07534 0.07138 -0.0779 1.0000 0.0286
-19.250 -1.0560 0.07115 0.06710 -0.0797 1.0000 0.0288
-19.000 -1.0625 0.06720 0.06305 -0.0813 1.0000 0.0289
-18.750 -1.0689 0.06344 0.05921 -0.0826 1.0000 0.0289
-18.500 -1.0732 0.05999 0.05567 -0.0837 1.0000 0.0291
-18.250 -1.0774 0.05667 0.05227 -0.0846 1.0000 0.0292
-18.000 -1.0802 0.05367 0.04918 -0.0852 1.0000 0.0293
-17.750 -1.0822 0.05083 0.04626 -0.0856 1.0000 0.0294
-17.500 -1.0840 0.04814 0.04350 -0.0857 1.0000 0.0294
-17.250 -1.0839 0.04575 0.04103 -0.0855 1.0000 0.0295
-17.000 -1.0829 0.04357 0.03877 -0.0852 1.0000 0.0297
-16.750 -1.0820 0.04149 0.03662 -0.0846 1.0000 0.0298
-16.500 -1.0804 0.03957 0.03463 -0.0837 1.0000 0.0298
-16.250 -1.0755 0.03802 0.03301 -0.0828 1.0000 0.0300
-16.000 -1.0733 0.03635 0.03128 -0.0815 1.0000 0.0300
-15.750 -1.0741 0.03455 0.02941 -0.0798 1.0000 0.0302
-15.500 -1.0761 0.03276 0.02757 -0.0778 1.0000 0.0304
-15.250 -1.0769 0.03117 0.02593 -0.0756 1.0000 0.0307
-15.000 -1.0750 0.02986 0.02458 -0.0734 1.0000 0.0309
-14.750 -1.0708 0.02877 0.02345 -0.0712 1.0000 0.0310
-14.500 -1.0668 0.02774 0.02239 -0.0688 1.0000 0.0312
-14.250 -1.0625 0.02680 0.02141 -0.0662 1.0000 0.0314
-14.000 -1.0579 0.02596 0.02054 -0.0635 1.0000 0.0316
-13.750 -1.0536 0.02519 0.01974 -0.0606 1.0000 0.0318
-13.500 -1.0300 0.02423 0.01874 -0.0614 0.9989 0.0320
-13.250 -1.0033 0.02339 0.01787 -0.0626 0.9972 0.0324
-13.000 -0.9750 0.02258 0.01702 -0.0640 0.9948 0.0327
-12.750 -0.9492 0.02179 0.01620 -0.0648 0.9913 0.0331
-12.500 -0.9250 0.02100 0.01538 -0.0653 0.9872 0.0334
-12.250 -0.8981 0.02027 0.01461 -0.0661 0.9827 0.0337
-12.000 -0.8741 0.01966 0.01396 -0.0662 0.9749 0.0339
-11.750 -0.8515 0.01883 0.01310 -0.0663 0.9653 0.0343
-11.500 -0.8260 0.01792 0.01216 -0.0670 0.9542 0.0349
-11.250 -0.7890 0.01719 0.01141 -0.0698 0.9441 0.0355
-11.000 -0.7449 0.01656 0.01075 -0.0739 0.9331 0.0362
-10.750 -0.6965 0.01600 0.01013 -0.0790 0.9185 0.0370
-10.500 -0.6469 0.01554 0.00960 -0.0842 0.9047 0.0379
-10.250 -0.6002 0.01507 0.00905 -0.0888 0.8911 0.0385
-10.000 -0.5647 0.01454 0.00844 -0.0912 0.8753 0.0398
-9.750 -0.5355 0.01421 0.00804 -0.0921 0.8601 0.0410
-9.500 -0.5111 0.01393 0.00770 -0.0918 0.8467 0.0417
-9.250 -0.4871 0.01370 0.00739 -0.0914 0.8340 0.0427
-9.000 -0.4667 0.01341 0.00705 -0.0902 0.8225 0.0437
-8.750 -0.4468 0.01311 0.00672 -0.0890 0.8116 0.0454
-8.500 -0.4268 0.01289 0.00645 -0.0877 0.8002 0.0471
-8.250 -0.4076 0.01263 0.00616 -0.0862 0.7896 0.0492
-8.000 -0.3890 0.01239 0.00589 -0.0845 0.7768 0.0517
-7.750 -0.3699 0.01216 0.00563 -0.0829 0.7653 0.0552
-7.500 -0.3517 0.01194 0.00538 -0.0811 0.7522 0.0595
-7.250 -0.3342 0.01166 0.00511 -0.0792 0.7384 0.0668
-7.000 -0.3182 0.01137 0.00485 -0.0771 0.7236 0.0797
-6.750 -0.3028 0.01110 0.00460 -0.0747 0.7078 0.0971
-6.500 -0.2864 0.01087 0.00441 -0.0726 0.6925 0.1128
-6.250 -0.2681 0.01069 0.00424 -0.0708 0.6792 0.1265
-6.000 -0.2497 0.01054 0.00410 -0.0689 0.6674 0.1378
-5.750 -0.2305 0.01042 0.00396 -0.0672 0.6566 0.1477
-5.500 -0.2111 0.01031 0.00384 -0.0656 0.6474 0.1568
-5.250 -0.1918 0.01017 0.00372 -0.0639 0.6391 0.1662
-5.000 -0.1726 0.01009 0.00361 -0.0621 0.6309 0.1751
-4.750 -0.1521 0.00995 0.00351 -0.0607 0.6250 0.1858
-4.500 -0.1322 0.00983 0.00341 -0.0591 0.6185 0.1969
-4.000 -0.0926 0.00962 0.00323 -0.0558 0.6065 0.2195
-3.750 -0.0728 0.00950 0.00315 -0.0542 0.6011 0.2330
-3.500 -0.0535 0.00941 0.00307 -0.0524 0.5954 0.2462
-3.250 -0.0348 0.00932 0.00300 -0.0505 0.5895 0.2619
-3.000 -0.0150 0.00916 0.00292 -0.0489 0.5854 0.2811
-2.750 0.0029 0.00899 0.00284 -0.0468 0.5806 0.3056
-2.500 0.0185 0.00880 0.00274 -0.0443 0.5756 0.3351
-2.250 0.0291 0.00855 0.00264 -0.0408 0.5701 0.3839
-2.000 0.0329 0.00810 0.00251 -0.0359 0.5669 0.4625
-1.750 0.0365 0.00774 0.00240 -0.0308 0.5631 0.5290
-1.500 0.0349 0.00742 0.00230 -0.0245 0.5592 0.5886
-1.250 0.0279 0.00714 0.00223 -0.0169 0.5549 0.6480
-1.000 0.0173 0.00696 0.00222 -0.0084 0.5506 0.7012
-0.750 0.0158 0.00681 0.00224 -0.0018 0.5475 0.7467
-0.500 0.0273 0.00671 0.00227 0.0019 0.5441 0.7807
-0.250 0.0433 0.00669 0.00231 0.0047 0.5399 0.8053
0.000 0.0619 0.00671 0.00235 0.0069 0.5354 0.8228
0.250 0.0830 0.00678 0.00241 0.0085 0.5301 0.8353
0.500 0.0998 0.00679 0.00243 0.0111 0.5271 0.8467
0.750 0.1283 0.00683 0.00250 0.0110 0.5231 0.8555
1.000 0.1399 0.00685 0.00250 0.0147 0.5189 0.8646
1.250 0.1715 0.00697 0.00261 0.0140 0.5135 0.8718
1.500 0.1799 0.00702 0.00264 0.0184 0.5093 0.8808
1.750 0.2122 0.00709 0.00273 0.0175 0.5056 0.8863
2.000 0.2365 0.00718 0.00282 0.0184 0.5000 0.8920
2.250 0.2363 0.00720 0.00281 0.0247 0.4947 0.9001
2.500 0.2752 0.00737 0.00297 0.0223 0.4888 0.9040
2.750 0.3085 0.00753 0.00314 0.0212 0.4832 0.9087
3.000 0.3167 0.00761 0.00321 0.0256 0.4786 0.9163
3.250 0.3487 0.00783 0.00339 0.0248 0.4727 0.9203
3.500 0.3901 0.00801 0.00359 0.0219 0.4672 0.9223
3.750 0.4249 0.00820 0.00375 0.0203 0.4602 0.9243
4.000 0.4552 0.00843 0.00394 0.0197 0.4533 0.9271
4.250 0.4508 0.00841 0.00394 0.0268 0.4494 0.9352
4.500 0.4917 0.00863 0.00414 0.0239 0.4418 0.9363
4.750 0.5269 0.00885 0.00431 0.0221 0.4331 0.9372
5.000 0.5624 0.00901 0.00445 0.0203 0.4238 0.9378
5.250 0.5945 0.00921 0.00460 0.0191 0.4147 0.9386
5.500 0.6257 0.00938 0.00475 0.0182 0.4054 0.9396
5.750 0.6545 0.00960 0.00493 0.0178 0.3971 0.9409
6.000 0.6828 0.00976 0.00508 0.0175 0.3891 0.9424
6.250 0.6692 0.00978 0.00509 0.0261 0.3839 0.9511
6.500 0.7024 0.00998 0.00526 0.0246 0.3748 0.9517
7.000 0.7636 0.01046 0.00568 0.0227 0.3559 0.9531
7.500 0.8202 0.01098 0.00615 0.0216 0.3381 0.9547
7.750 0.8461 0.01132 0.00644 0.0215 0.3282 0.9558
8.000 0.8736 0.01157 0.00667 0.0211 0.3194 0.9571
8.250 0.8954 0.01191 0.00698 0.0217 0.3107 0.9591
8.500 0.8935 0.01207 0.00715 0.0275 0.3055 0.9660
8.750 0.9208 0.01242 0.00747 0.0268 0.2959 0.9667
9.000 0.9492 0.01274 0.00777 0.0260 0.2867 0.9674
9.250 0.9748 0.01320 0.00817 0.0256 0.2742 0.9683
9.500 0.9991 0.01367 0.00860 0.0253 0.2621 0.9693
9.750 1.0212 0.01419 0.00907 0.0254 0.2479 0.9707
10.000 1.0402 0.01479 0.00961 0.0259 0.2332 0.9724
10.250 1.0548 0.01550 0.01025 0.0271 0.2179 0.9750
10.500 1.0557 0.01634 0.01103 0.0309 0.2029 0.9801
10.750 1.0737 0.01731 0.01190 0.0308 0.1853 0.9810
11.000 1.0917 0.01826 0.01279 0.0307 0.1717 0.9819
11.250 1.1101 0.01916 0.01366 0.0305 0.1620 0.9830
11.500 1.1271 0.02014 0.01461 0.0305 0.1534 0.9843
11.750 1.1441 0.02109 0.01554 0.0304 0.1471 0.9857
12.000 1.1606 0.02208 0.01654 0.0305 0.1423 0.9875
12.250 1.1778 0.02296 0.01744 0.0306 0.1386 0.9893
12.500 1.1898 0.02403 0.01851 0.0314 0.1356 0.9915
12.750 1.2029 0.02520 0.01969 0.0317 0.1319 0.9928
13.000 1.2220 0.02618 0.02071 0.0310 0.1295 0.9936
13.250 1.2403 0.02721 0.02177 0.0305 0.1265 0.9945
13.500 1.2561 0.02843 0.02299 0.0300 0.1235 0.9956
13.750 1.2694 0.02993 0.02451 0.0295 0.1200 0.9969
14.000 1.2870 0.03111 0.02573 0.0288 0.1176 0.9980
14.250 1.3030 0.03243 0.02709 0.0282 0.1146 0.9989
14.500 1.3149 0.03413 0.02879 0.0277 0.1110 0.9997
14.750 1.3203 0.03570 0.03039 0.0285 0.1077 1.0000
15.000 1.3226 0.03707 0.03180 0.0303 0.1044 1.0000
15.250 1.3186 0.03899 0.03371 0.0323 0.1000 1.0000
15.500 1.3193 0.04059 0.03534 0.0339 0.0956 1.0000
15.750 1.3147 0.04267 0.03740 0.0356 0.0883 1.0000
16.000 1.3066 0.04513 0.03983 0.0373 0.0782 1.0000
16.250 1.2941 0.04809 0.04274 0.0390 0.0695 1.0000
16.500 1.2840 0.05093 0.04557 0.0404 0.0649 1.0000
16.750 1.2776 0.05350 0.04817 0.0415 0.0624 1.0000
17.000 1.2703 0.05628 0.05097 0.0425 0.0601 1.0000
17.250 1.2675 0.05869 0.05344 0.0433 0.0590 1.0000
17.500 1.2650 0.06111 0.05590 0.0440 0.0580 1.0000
17.750 1.2590 0.06397 0.05881 0.0446 0.0569 1.0000
18.000 1.2534 0.06686 0.06174 0.0450 0.0558 1.0000
18.250 1.2457 0.07005 0.06498 0.0453 0.0545 1.0000
18.500 1.2443 0.07261 0.06760 0.0456 0.0539 1.0000
18.750 1.2428 0.07519 0.07024 0.0458 0.0532 1.0000
19.000 1.2402 0.07796 0.07307 0.0458 0.0525 1.0000
19.250 1.2372 0.08081 0.07597 0.0458 0.0518 1.0000
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