GOE 738 AIRFOIL (goe738-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: GOE 738 AIRFOIL (goe738-il) Reynolds number: 500,000 Max Cl/Cd: 87.31 at α=6° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-goe738-il-500000.txt Download as CSV file: xf-goe738-il-500000.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 = 0.500 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-17.500 -1.0146 0.09199 0.08861 -0.0225 1.0000 0.0353
-17.250 -1.0588 0.08027 0.07663 -0.0311 1.0000 0.0353
-17.000 -1.0896 0.07171 0.06785 -0.0372 1.0000 0.0353
-16.750 -1.1133 0.06490 0.06083 -0.0417 1.0000 0.0354
-16.500 -1.1333 0.05904 0.05482 -0.0448 1.0000 0.0357
-16.250 -1.1419 0.05494 0.05062 -0.0466 1.0000 0.0359
-16.000 -1.1475 0.05141 0.04700 -0.0479 1.0000 0.0361
-15.750 -1.1476 0.04872 0.04426 -0.0487 1.0000 0.0364
-15.500 -1.1499 0.04593 0.04139 -0.0493 1.0000 0.0366
-15.250 -1.1501 0.04356 0.03894 -0.0496 1.0000 0.0369
-15.000 -1.1511 0.04122 0.03651 -0.0495 1.0000 0.0372
-14.750 -1.1512 0.03914 0.03433 -0.0491 1.0000 0.0375
-14.500 -1.1507 0.03722 0.03230 -0.0483 1.0000 0.0378
-14.250 -1.1493 0.03548 0.03046 -0.0471 1.0000 0.0382
-14.000 -1.1462 0.03405 0.02893 -0.0457 1.0000 0.0387
-13.750 -1.1426 0.03265 0.02742 -0.0441 1.0000 0.0391
-13.500 -1.1380 0.03142 0.02607 -0.0422 1.0000 0.0395
-13.250 -1.1322 0.03031 0.02483 -0.0400 1.0000 0.0398
-13.000 -1.1252 0.02934 0.02374 -0.0378 1.0000 0.0401
-12.750 -1.1156 0.02781 0.02213 -0.0360 1.0000 0.0406
-12.500 -1.1030 0.02666 0.02098 -0.0344 1.0000 0.0411
-12.250 -1.0896 0.02582 0.02014 -0.0326 1.0000 0.0416
-12.000 -1.0753 0.02509 0.01940 -0.0309 1.0000 0.0421
-11.750 -1.0438 0.02443 0.01856 -0.0325 0.8950 0.0430
-11.500 -1.0305 0.02393 0.01788 -0.0301 0.8651 0.0436
-11.250 -1.0150 0.02338 0.01717 -0.0282 0.8470 0.0443
-11.000 -0.9981 0.02280 0.01644 -0.0265 0.8333 0.0449
-10.750 -0.9797 0.02228 0.01578 -0.0250 0.8213 0.0454
-10.500 -0.9621 0.02128 0.01470 -0.0236 0.8113 0.0462
-10.250 -0.9434 0.02058 0.01396 -0.0222 0.8018 0.0470
-10.000 -0.9230 0.02006 0.01340 -0.0210 0.7930 0.0478
-9.750 -0.9020 0.01961 0.01289 -0.0199 0.7846 0.0487
-9.500 -0.8803 0.01918 0.01238 -0.0188 0.7769 0.0498
-9.250 -0.8579 0.01875 0.01186 -0.0178 0.7691 0.0508
-9.000 -0.8357 0.01832 0.01131 -0.0168 0.7621 0.0517
-8.750 -0.8156 0.01751 0.01053 -0.0156 0.7548 0.0530
-8.500 -0.7930 0.01709 0.01007 -0.0146 0.7479 0.0542
-8.250 -0.7696 0.01672 0.00964 -0.0138 0.7413 0.0556
-8.000 -0.7456 0.01635 0.00922 -0.0130 0.7344 0.0571
-7.750 -0.7221 0.01596 0.00874 -0.0121 0.7281 0.0586
-7.500 -0.6996 0.01543 0.00823 -0.0111 0.7219 0.0607
-7.250 -0.6751 0.01510 0.00788 -0.0104 0.7150 0.0628
-7.000 -0.6502 0.01484 0.00753 -0.0097 0.7089 0.0648
-6.750 -0.6268 0.01435 0.00703 -0.0089 0.7028 0.0673
-6.500 -0.6022 0.01399 0.00668 -0.0082 0.6964 0.0701
-6.250 -0.5768 0.01376 0.00636 -0.0075 0.6903 0.0730
-6.000 -0.5526 0.01334 0.00595 -0.0068 0.6840 0.0766
-5.750 -0.5272 0.01303 0.00565 -0.0062 0.6776 0.0805
-5.500 -0.5020 0.01276 0.00531 -0.0055 0.6718 0.0847
-5.250 -0.4768 0.01243 0.00502 -0.0049 0.6659 0.0901
-5.000 -0.4511 0.01213 0.00473 -0.0043 0.6594 0.0967
-4.750 -0.4255 0.01187 0.00447 -0.0037 0.6533 0.1057
-4.500 -0.3999 0.01158 0.00427 -0.0032 0.6470 0.1202
-4.250 -0.3739 0.01131 0.00409 -0.0027 0.6407 0.1392
-4.000 -0.3476 0.01112 0.00391 -0.0022 0.6349 0.1569
-3.750 -0.3210 0.01093 0.00377 -0.0018 0.6289 0.1725
-3.500 -0.2943 0.01073 0.00363 -0.0015 0.6224 0.1869
-3.250 -0.2678 0.01057 0.00347 -0.0010 0.6163 0.2015
-3.000 -0.2411 0.01040 0.00335 -0.0007 0.6102 0.2177
-2.750 -0.2144 0.01020 0.00322 -0.0003 0.6038 0.2365
-2.500 -0.1881 0.01003 0.00309 0.0002 0.5981 0.2599
-2.250 -0.1621 0.00981 0.00298 0.0006 0.5923 0.2904
-2.000 -0.1363 0.00955 0.00287 0.0011 0.5860 0.3293
-1.750 -0.1115 0.00928 0.00275 0.0018 0.5795 0.3789
-1.500 -0.0872 0.00896 0.00266 0.0026 0.5729 0.4406
-1.250 -0.0635 0.00864 0.00259 0.0036 0.5661 0.5090
-1.000 -0.0402 0.00841 0.00254 0.0047 0.5599 0.5754
-0.750 -0.0157 0.00819 0.00253 0.0056 0.5534 0.6284
-0.500 0.0090 0.00803 0.00252 0.0065 0.5473 0.6762
-0.250 0.0337 0.00795 0.00253 0.0075 0.5414 0.7196
0.000 0.0595 0.00784 0.00257 0.0083 0.5353 0.7576
0.250 0.0859 0.00780 0.00258 0.0089 0.5290 0.7863
0.500 0.1127 0.00781 0.00259 0.0095 0.5228 0.8093
0.750 0.1406 0.00776 0.00261 0.0098 0.5162 0.8307
1.000 0.1688 0.00776 0.00263 0.0101 0.5101 0.8511
1.250 0.1982 0.00779 0.00268 0.0101 0.5045 0.8713
1.500 0.2301 0.00780 0.00275 0.0096 0.4987 0.8908
1.750 0.2642 0.00787 0.00282 0.0086 0.4929 0.9074
2.000 0.2991 0.00799 0.00290 0.0074 0.4873 0.9211
2.250 0.3384 0.00809 0.00303 0.0053 0.4813 0.9335
2.500 0.3802 0.00827 0.00318 0.0028 0.4750 0.9455
2.750 0.4188 0.00848 0.00334 0.0009 0.4691 0.9551
3.000 0.4610 0.00863 0.00350 -0.0018 0.4625 0.9607
3.250 0.4963 0.00880 0.00362 -0.0031 0.4561 0.9681
3.500 0.5373 0.00893 0.00372 -0.0057 0.4495 0.9710
3.750 0.5758 0.00902 0.00381 -0.0078 0.4418 0.9751
4.000 0.6096 0.00918 0.00392 -0.0089 0.4341 0.9809
4.250 0.6500 0.00923 0.00397 -0.0115 0.4247 0.9833
4.500 0.6887 0.00934 0.00403 -0.0138 0.4149 0.9866
4.750 0.7256 0.00945 0.00411 -0.0157 0.4038 0.9905
5.000 0.7631 0.00954 0.00419 -0.0177 0.3921 0.9938
5.250 0.8017 0.00964 0.00424 -0.0201 0.3779 0.9968
5.500 0.8398 0.00977 0.00431 -0.0224 0.3608 0.9997
5.750 0.8633 0.00993 0.00441 -0.0218 0.3446 1.0000
6.000 0.8844 0.01013 0.00455 -0.0207 0.3284 1.0000
6.250 0.9053 0.01038 0.00472 -0.0196 0.3125 1.0000
6.500 0.9260 0.01066 0.00493 -0.0185 0.2975 1.0000
6.750 0.9464 0.01099 0.00519 -0.0173 0.2839 1.0000
7.000 0.9675 0.01127 0.00543 -0.0162 0.2738 1.0000
7.250 0.9882 0.01158 0.00571 -0.0151 0.2655 1.0000
7.500 1.0091 0.01188 0.00598 -0.0140 0.2576 1.0000
7.750 1.0294 0.01223 0.00630 -0.0128 0.2503 1.0000
8.000 1.0506 0.01250 0.00658 -0.0117 0.2439 1.0000
8.250 1.0701 0.01288 0.00692 -0.0104 0.2377 1.0000
8.500 1.0909 0.01316 0.00723 -0.0093 0.2321 1.0000
8.750 1.1110 0.01348 0.00756 -0.0081 0.2259 1.0000
9.000 1.1288 0.01394 0.00797 -0.0066 0.2196 1.0000
9.250 1.1498 0.01418 0.00827 -0.0056 0.2142 1.0000
9.500 1.1679 0.01457 0.00865 -0.0041 0.2077 1.0000
9.750 1.1857 0.01496 0.00905 -0.0027 0.2015 1.0000
10.000 1.2038 0.01531 0.00942 -0.0012 0.1940 1.0000
10.250 1.2193 0.01577 0.00987 0.0005 0.1861 1.0000
10.500 1.2338 0.01624 0.01033 0.0023 0.1758 1.0000
10.750 1.2458 0.01681 0.01087 0.0044 0.1630 1.0000
11.000 1.2480 0.01755 0.01155 0.0080 0.1495 1.0000
11.250 1.2452 0.01862 0.01257 0.0115 0.1371 1.0000
11.500 1.2445 0.02001 0.01391 0.0138 0.1258 1.0000
11.750 1.2455 0.02158 0.01544 0.0156 0.1161 1.0000
12.000 1.2457 0.02336 0.01719 0.0170 0.1080 1.0000
12.250 1.2494 0.02500 0.01884 0.0181 0.1009 1.0000
12.500 1.2522 0.02680 0.02065 0.0191 0.0955 1.0000
12.750 1.2560 0.02859 0.02245 0.0198 0.0906 1.0000
13.000 1.2560 0.03075 0.02461 0.0205 0.0871 1.0000
13.250 1.2630 0.03237 0.02629 0.0210 0.0845 1.0000
13.500 1.2672 0.03426 0.02822 0.0215 0.0819 1.0000
13.750 1.2688 0.03644 0.03041 0.0218 0.0797 1.0000
14.000 1.2666 0.03902 0.03301 0.0221 0.0775 1.0000
14.250 1.2730 0.04084 0.03490 0.0223 0.0760 1.0000
14.500 1.2764 0.04296 0.03708 0.0224 0.0743 1.0000
14.750 1.2788 0.04529 0.03945 0.0224 0.0727 1.0000
15.000 1.2792 0.04789 0.04208 0.0223 0.0712 1.0000
15.250 1.2787 0.05060 0.04484 0.0221 0.0703 1.0000
15.500 1.2768 0.05353 0.04780 0.0218 0.0688 1.0000
15.750 1.2812 0.05586 0.05021 0.0215 0.0679 1.0000
16.000 1.2843 0.05832 0.05275 0.0212 0.0669 1.0000
16.250 1.2863 0.06097 0.05547 0.0207 0.0659 1.0000
16.500 1.2883 0.06363 0.05818 0.0203 0.0650 1.0000
16.750 1.2877 0.06666 0.06125 0.0196 0.0638 1.0000
17.000 1.2866 0.06970 0.06432 0.0190 0.0627 1.0000
17.250 1.2858 0.07267 0.06731 0.0185 0.0617 1.0000
17.500 1.2875 0.07540 0.07010 0.0179 0.0609 1.0000
17.750 1.2894 0.07827 0.07306 0.0172 0.0602 1.0000
18.000 1.2911 0.08115 0.07602 0.0164 0.0594 1.0000
18.250 1.2921 0.08414 0.07909 0.0156 0.0587 1.0000
18.500 1.2932 0.08713 0.08214 0.0147 0.0578 1.0000
18.750 1.2930 0.09034 0.08541 0.0137 0.0570 1.0000
19.000 1.2925 0.09354 0.08865 0.0126 0.0559 1.0000
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