NASA SC(2)-0614 AIRFOIL (sc20614-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: NASA SC(2)-0614 AIRFOIL (sc20614-il) Reynolds number: 1,000,000 Max Cl/Cd: 77.63 at α=6.75° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-sc20614-il-1000000.txt Download as CSV file: xf-sc20614-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: NASA SC(2)-0614 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 -1.2076 0.08816 0.08456 -0.0487 1.0000 0.0236
-19.500 -1.2189 0.08264 0.07893 -0.0516 1.0000 0.0237
-19.250 -1.2285 0.07753 0.07371 -0.0542 1.0000 0.0238
-19.000 -1.2358 0.07282 0.06889 -0.0566 1.0000 0.0239
-18.750 -1.2407 0.06858 0.06454 -0.0586 1.0000 0.0240
-18.500 -1.2438 0.06471 0.06057 -0.0604 1.0000 0.0241
-18.250 -1.2448 0.06120 0.05696 -0.0620 1.0000 0.0242
-18.000 -1.2437 0.05804 0.05372 -0.0633 1.0000 0.0243
-17.750 -1.2535 0.05385 0.04941 -0.0646 1.0000 0.0246
-17.500 -1.2575 0.05041 0.04590 -0.0656 1.0000 0.0249
-17.250 -1.2576 0.04750 0.04293 -0.0664 1.0000 0.0251
-17.000 -1.2551 0.04497 0.04033 -0.0670 1.0000 0.0254
-16.750 -1.2508 0.04267 0.03798 -0.0675 1.0000 0.0256
-16.500 -1.2449 0.04064 0.03589 -0.0678 1.0000 0.0258
-16.250 -1.2382 0.03875 0.03394 -0.0679 1.0000 0.0260
-16.000 -1.2309 0.03697 0.03211 -0.0680 1.0000 0.0263
-15.750 -1.2227 0.03537 0.03045 -0.0679 1.0000 0.0266
-15.500 -1.2142 0.03384 0.02886 -0.0677 1.0000 0.0268
-15.250 -1.2049 0.03242 0.02739 -0.0674 1.0000 0.0271
-15.000 -1.1951 0.03110 0.02601 -0.0670 1.0000 0.0274
-14.750 -1.1849 0.02987 0.02472 -0.0665 1.0000 0.0277
-14.500 -1.1744 0.02876 0.02356 -0.0657 1.0000 0.0279
-14.250 -1.1644 0.02774 0.02249 -0.0647 1.0000 0.0281
-14.000 -1.1601 0.02654 0.02124 -0.0630 1.0000 0.0284
-13.750 -1.1614 0.02528 0.01994 -0.0604 1.0000 0.0288
-13.500 -1.1659 0.02431 0.01896 -0.0568 1.0000 0.0292
-13.250 -1.1810 0.02358 0.01820 -0.0509 1.0000 0.0294
-13.000 -1.1858 0.02280 0.01740 -0.0469 1.0000 0.0296
-12.750 -1.1615 0.02193 0.01651 -0.0481 0.9990 0.0302
-12.500 -1.1316 0.02114 0.01570 -0.0502 0.9976 0.0310
-12.250 -1.1011 0.02041 0.01493 -0.0523 0.9962 0.0317
-12.000 -1.0696 0.01973 0.01421 -0.0545 0.9949 0.0323
-11.750 -1.0377 0.01884 0.01329 -0.0570 0.9938 0.0331
-11.500 -1.0050 0.01801 0.01246 -0.0597 0.9930 0.0342
-11.250 -0.9740 0.01740 0.01184 -0.0615 0.9913 0.0352
-11.000 -0.9426 0.01685 0.01128 -0.0633 0.9894 0.0363
-10.750 -0.9098 0.01638 0.01078 -0.0653 0.9878 0.0372
-10.500 -0.8763 0.01564 0.01006 -0.0678 0.9863 0.0391
-10.250 -0.8420 0.01519 0.00961 -0.0700 0.9852 0.0408
-10.000 -0.8072 0.01483 0.00923 -0.0721 0.9843 0.0424
-9.750 -0.7717 0.01422 0.00865 -0.0747 0.9834 0.0447
-9.500 -0.7362 0.01384 0.00827 -0.0770 0.9827 0.0469
-9.250 -0.7005 0.01353 0.00794 -0.0791 0.9821 0.0485
-9.000 -0.6642 0.01298 0.00743 -0.0818 0.9816 0.0515
-8.750 -0.6283 0.01265 0.00710 -0.0840 0.9810 0.0538
-8.500 -0.5964 0.01233 0.00677 -0.0853 0.9787 0.0558
-8.250 -0.5642 0.01193 0.00641 -0.0868 0.9760 0.0588
-8.000 -0.5307 0.01166 0.00614 -0.0883 0.9740 0.0612
-7.750 -0.4966 0.01134 0.00582 -0.0901 0.9722 0.0637
-7.500 -0.4623 0.01100 0.00551 -0.0919 0.9705 0.0669
-7.250 -0.4286 0.01075 0.00526 -0.0934 0.9687 0.0696
-7.000 -0.3958 0.01046 0.00499 -0.0947 0.9663 0.0730
-6.750 -0.3650 0.01017 0.00474 -0.0957 0.9623 0.0772
-6.500 -0.3332 0.00993 0.00450 -0.0967 0.9590 0.0815
-6.250 -0.3008 0.00963 0.00426 -0.0980 0.9561 0.0881
-6.000 -0.2680 0.00936 0.00403 -0.0993 0.9534 0.0970
-5.750 -0.2364 0.00909 0.00383 -0.1003 0.9495 0.1092
-5.500 -0.2041 0.00879 0.00362 -0.1016 0.9454 0.1284
-5.250 -0.1711 0.00845 0.00340 -0.1030 0.9418 0.1540
-5.000 -0.1370 0.00807 0.00318 -0.1048 0.9385 0.1911
-4.750 -0.1024 0.00766 0.00297 -0.1067 0.9347 0.2398
-4.500 -0.0661 0.00714 0.00273 -0.1091 0.9307 0.3094
-4.000 0.0107 0.00594 0.00223 -0.1150 0.9238 0.5067
-3.750 0.0431 0.00582 0.00222 -0.1160 0.9193 0.5432
-3.500 0.0738 0.00579 0.00221 -0.1164 0.9136 0.5632
-3.250 0.1039 0.00579 0.00219 -0.1167 0.9072 0.5769
-3.000 0.1341 0.00578 0.00219 -0.1170 0.9000 0.5855
-2.750 0.1638 0.00580 0.00216 -0.1171 0.8918 0.5933
-2.500 0.1934 0.00580 0.00215 -0.1172 0.8812 0.6001
-2.250 0.2229 0.00585 0.00216 -0.1173 0.8713 0.6074
-2.000 0.2531 0.00588 0.00216 -0.1175 0.8620 0.6135
-1.750 0.2825 0.00590 0.00218 -0.1176 0.8509 0.6188
-1.500 0.3117 0.00597 0.00218 -0.1176 0.8357 0.6234
-1.250 0.3411 0.00607 0.00220 -0.1176 0.8194 0.6287
-1.000 0.3705 0.00611 0.00224 -0.1177 0.8047 0.6341
-0.750 0.3998 0.00619 0.00230 -0.1177 0.7886 0.6384
-0.500 0.4290 0.00631 0.00234 -0.1177 0.7703 0.6426
-0.250 0.4580 0.00646 0.00239 -0.1177 0.7480 0.6465
0.000 0.4862 0.00659 0.00244 -0.1175 0.7150 0.6497
0.250 0.5131 0.00688 0.00252 -0.1172 0.6561 0.6520
0.500 0.5357 0.00771 0.00276 -0.1161 0.5200 0.6542
0.750 0.5602 0.00840 0.00301 -0.1155 0.4176 0.6565
1.000 0.5858 0.00899 0.00322 -0.1152 0.3343 0.6584
1.250 0.6117 0.00953 0.00342 -0.1149 0.2603 0.6599
1.500 0.6386 0.00996 0.00361 -0.1147 0.2108 0.6613
1.750 0.6659 0.01028 0.00376 -0.1146 0.1734 0.6628
2.000 0.6932 0.01058 0.00393 -0.1145 0.1461 0.6644
2.250 0.7209 0.01084 0.00410 -0.1144 0.1261 0.6661
2.500 0.7482 0.01114 0.00430 -0.1142 0.1063 0.6678
2.750 0.7756 0.01143 0.00450 -0.1140 0.0921 0.6694
3.000 0.8033 0.01167 0.00469 -0.1139 0.0835 0.6711
3.250 0.8311 0.01190 0.00489 -0.1138 0.0772 0.6728
3.500 0.8585 0.01218 0.00511 -0.1136 0.0718 0.6744
3.750 0.8865 0.01238 0.00530 -0.1135 0.0688 0.6760
4.000 0.9141 0.01262 0.00551 -0.1133 0.0657 0.6773
4.250 0.9410 0.01290 0.00577 -0.1131 0.0624 0.6793
4.500 0.9687 0.01306 0.00596 -0.1129 0.0607 0.6810
4.750 0.9959 0.01329 0.00618 -0.1127 0.0585 0.6827
5.000 1.0224 0.01359 0.00647 -0.1123 0.0561 0.6844
5.250 1.0491 0.01386 0.00675 -0.1120 0.0544 0.6862
5.500 1.0760 0.01409 0.00699 -0.1117 0.0529 0.6881
5.750 1.1026 0.01436 0.00726 -0.1113 0.0511 0.6900
6.000 1.1280 0.01475 0.00762 -0.1108 0.0490 0.6918
6.250 1.1543 0.01503 0.00791 -0.1104 0.0477 0.6933
6.500 1.1806 0.01525 0.00817 -0.1100 0.0462 0.6956
6.750 1.2063 0.01554 0.00847 -0.1095 0.0446 0.6976
7.000 1.2302 0.01602 0.00893 -0.1087 0.0425 0.6996
7.250 1.2563 0.01624 0.00919 -0.1083 0.0414 0.7017
7.500 1.2817 0.01652 0.00950 -0.1077 0.0400 0.7040
7.750 1.3063 0.01688 0.00984 -0.1071 0.0386 0.7063
8.000 1.3292 0.01741 0.01037 -0.1061 0.0371 0.7084
8.250 1.3540 0.01769 0.01069 -0.1054 0.0362 0.7107
8.500 1.3781 0.01802 0.01106 -0.1047 0.0352 0.7130
8.750 1.4015 0.01839 0.01145 -0.1038 0.0343 0.7151
9.000 1.4238 0.01885 0.01192 -0.1028 0.0333 0.7173
9.250 1.4440 0.01948 0.01258 -0.1014 0.0323 0.7197
9.500 1.4667 0.01986 0.01300 -0.1003 0.0318 0.7222
9.750 1.4886 0.02027 0.01345 -0.0992 0.0311 0.7243
10.000 1.5098 0.02070 0.01391 -0.0980 0.0305 0.7265
10.250 1.5298 0.02116 0.01441 -0.0966 0.0299 0.7289
10.500 1.5483 0.02169 0.01498 -0.0950 0.0293 0.7311
10.750 1.5643 0.02236 0.01568 -0.0929 0.0287 0.7334
11.000 1.5745 0.02325 0.01662 -0.0899 0.0281 0.7357
11.250 1.5889 0.02378 0.01723 -0.0875 0.0279 0.7381
11.500 1.6040 0.02441 0.01791 -0.0854 0.0276 0.7403
11.750 1.6189 0.02508 0.01865 -0.0833 0.0273 0.7424
12.000 1.6334 0.02579 0.01944 -0.0812 0.0269 0.7451
12.250 1.6469 0.02656 0.02028 -0.0791 0.0266 0.7475
12.500 1.6599 0.02739 0.02117 -0.0770 0.0263 0.7501
12.750 1.6725 0.02826 0.02210 -0.0748 0.0260 0.7527
13.000 1.6840 0.02921 0.02311 -0.0727 0.0257 0.7552
13.250 1.6948 0.03025 0.02420 -0.0706 0.0254 0.7573
13.500 1.7035 0.03145 0.02546 -0.0683 0.0251 0.7595
13.750 1.7093 0.03289 0.02698 -0.0659 0.0247 0.7621
14.000 1.7092 0.03486 0.02905 -0.0631 0.0243 0.7643
14.250 1.7142 0.03647 0.03077 -0.0609 0.0241 0.7667
14.500 1.7220 0.03789 0.03228 -0.0592 0.0240 0.7691
14.750 1.7287 0.03947 0.03395 -0.0575 0.0238 0.7715
15.000 1.7341 0.04120 0.03577 -0.0558 0.0237 0.7738
15.250 1.7381 0.04309 0.03777 -0.0542 0.0235 0.7759
15.500 1.7406 0.04519 0.03998 -0.0528 0.0234 0.7785
15.750 1.7420 0.04748 0.04238 -0.0515 0.0232 0.7809
16.000 1.7421 0.04998 0.04500 -0.0503 0.0230 0.7832
16.250 1.7408 0.05271 0.04783 -0.0494 0.0229 0.7855
16.500 1.7386 0.05571 0.05095 -0.0488 0.0227 0.7879
16.750 1.7345 0.05908 0.05443 -0.0485 0.0226 0.7900
17.250 1.7223 0.06687 0.06245 -0.0490 0.0223 0.7942
17.500 1.7135 0.07146 0.06718 -0.0500 0.0222 0.7963
17.750 1.7025 0.07663 0.07248 -0.0515 0.0221 0.7983
18.000 1.6891 0.08242 0.07841 -0.0537 0.0220 0.8002
18.250 1.6730 0.08888 0.08502 -0.0564 0.0220 0.8020
18.500 1.6543 0.09604 0.09232 -0.0599 0.0219 0.8037
18.750 1.6330 0.10386 0.10029 -0.0639 0.0218 0.8051
19.000 1.6088 0.11230 0.10889 -0.0685 0.0218 0.8064
19.250 1.5833 0.12116 0.11790 -0.0736 0.0217 0.8074
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