NASA SC(2)-0712 AIRFOIL (sc20712-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: NASA SC(2)-0712 AIRFOIL (sc20712-il) Reynolds number: 1,000,000 Max Cl/Cd: 85.25 at α=-0.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-sc20712-il-1000000.txt Download as CSV file: xf-sc20712-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: NASA SC(2)-0712 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
------ -------- --------- --------- -------- -------- --------
-19.500 -1.0650 0.10551 0.10270 -0.0395 1.0000 0.0179
-19.250 -1.0958 0.09582 0.09285 -0.0450 1.0000 0.0179
-19.000 -1.1211 0.08727 0.08416 -0.0499 1.0000 0.0179
-18.750 -1.1417 0.07980 0.07656 -0.0542 1.0000 0.0180
-18.500 -1.1580 0.07318 0.06981 -0.0580 1.0000 0.0180
-18.250 -1.1709 0.06736 0.06386 -0.0613 1.0000 0.0181
-18.000 -1.1800 0.06233 0.05873 -0.0641 1.0000 0.0182
-17.750 -1.1860 0.05795 0.05425 -0.0664 1.0000 0.0183
-17.500 -1.1900 0.05408 0.05028 -0.0683 1.0000 0.0184
-17.250 -1.1914 0.05071 0.04683 -0.0699 1.0000 0.0186
-17.000 -1.1917 0.04764 0.04368 -0.0711 1.0000 0.0187
-16.750 -1.1910 0.04487 0.04082 -0.0720 1.0000 0.0189
-16.500 -1.1894 0.04236 0.03822 -0.0726 1.0000 0.0191
-16.250 -1.1874 0.04004 0.03582 -0.0729 1.0000 0.0192
-16.000 -1.1845 0.03791 0.03361 -0.0730 1.0000 0.0194
-15.750 -1.1811 0.03596 0.03158 -0.0728 1.0000 0.0196
-15.500 -1.1771 0.03421 0.02974 -0.0723 1.0000 0.0198
-15.250 -1.1732 0.03262 0.02808 -0.0715 1.0000 0.0200
-15.000 -1.1692 0.03118 0.02657 -0.0703 1.0000 0.0201
-14.750 -1.1660 0.02989 0.02520 -0.0687 1.0000 0.0203
-14.500 -1.1640 0.02875 0.02400 -0.0666 1.0000 0.0205
-14.250 -1.1650 0.02775 0.02295 -0.0637 1.0000 0.0206
-14.000 -1.1731 0.02690 0.02205 -0.0594 1.0000 0.0207
-13.750 -1.1796 0.02581 0.02089 -0.0556 1.0000 0.0208
-13.500 -1.1806 0.02423 0.01924 -0.0535 1.0000 0.0212
-13.250 -1.1710 0.02307 0.01805 -0.0526 1.0000 0.0216
-13.000 -1.1419 0.02208 0.01702 -0.0549 0.9990 0.0220
-12.750 -1.1115 0.02125 0.01616 -0.0572 0.9980 0.0225
-12.500 -1.0804 0.02048 0.01534 -0.0594 0.9970 0.0231
-12.250 -1.0488 0.01976 0.01457 -0.0617 0.9960 0.0236
-12.000 -1.0167 0.01913 0.01387 -0.0638 0.9952 0.0242
-11.750 -0.9842 0.01861 0.01330 -0.0658 0.9945 0.0246
-11.500 -0.9517 0.01742 0.01209 -0.0688 0.9939 0.0257
-11.250 -0.9183 0.01690 0.01155 -0.0709 0.9934 0.0266
-11.000 -0.8881 0.01642 0.01104 -0.0723 0.9919 0.0274
-10.750 -0.8567 0.01596 0.01055 -0.0738 0.9905 0.0282
-10.500 -0.8244 0.01559 0.01014 -0.0753 0.9893 0.0289
-10.250 -0.7913 0.01476 0.00929 -0.0776 0.9883 0.0303
-10.000 -0.7582 0.01432 0.00885 -0.0795 0.9873 0.0314
-9.750 -0.7247 0.01394 0.00845 -0.0813 0.9865 0.0326
-9.500 -0.6907 0.01361 0.00809 -0.0831 0.9857 0.0336
-9.250 -0.6558 0.01305 0.00753 -0.0853 0.9851 0.0352
-9.000 -0.6210 0.01269 0.00719 -0.0873 0.9845 0.0369
-8.750 -0.5863 0.01241 0.00690 -0.0892 0.9839 0.0385
-8.500 -0.5510 0.01205 0.00653 -0.0913 0.9834 0.0402
-8.250 -0.5154 0.01169 0.00619 -0.0934 0.9830 0.0425
-8.000 -0.4801 0.01144 0.00594 -0.0954 0.9826 0.0446
-7.750 -0.4443 0.01112 0.00563 -0.0975 0.9823 0.0473
-7.500 -0.4144 0.01083 0.00537 -0.0982 0.9796 0.0503
-7.250 -0.3819 0.01063 0.00516 -0.0995 0.9779 0.0529
-7.000 -0.3469 0.01027 0.00484 -0.1014 0.9768 0.0579
-6.750 -0.3124 0.01006 0.00463 -0.1031 0.9759 0.0614
-6.500 -0.2766 0.00974 0.00438 -0.1051 0.9752 0.0676
-6.250 -0.2411 0.00952 0.00417 -0.1070 0.9745 0.0729
-6.000 -0.2050 0.00925 0.00395 -0.1091 0.9738 0.0810
-5.750 -0.1691 0.00897 0.00374 -0.1111 0.9731 0.0922
-5.500 -0.1332 0.00869 0.00354 -0.1131 0.9723 0.1080
-5.250 -0.0964 0.00833 0.00333 -0.1154 0.9717 0.1387
-5.000 -0.0591 0.00792 0.00312 -0.1180 0.9710 0.1843
-4.750 -0.0207 0.00743 0.00290 -0.1208 0.9704 0.2518
-4.500 0.0189 0.00686 0.00266 -0.1241 0.9699 0.3426
-4.250 0.0607 0.00614 0.00241 -0.1280 0.9694 0.4699
-4.000 0.0939 0.00585 0.00237 -0.1294 0.9664 0.5455
-3.750 0.1251 0.00577 0.00234 -0.1300 0.9628 0.5705
-3.500 0.1568 0.00570 0.00228 -0.1306 0.9594 0.5845
-3.250 0.1884 0.00563 0.00222 -0.1312 0.9556 0.5953
-3.000 0.2161 0.00557 0.00216 -0.1308 0.9475 0.6032
-2.750 0.2456 0.00551 0.00209 -0.1308 0.9400 0.6111
-2.500 0.2735 0.00550 0.00207 -0.1305 0.9307 0.6192
-2.250 0.3028 0.00551 0.00208 -0.1304 0.9232 0.6280
-2.000 0.3312 0.00554 0.00205 -0.1302 0.9107 0.6339
-1.750 0.3594 0.00554 0.00207 -0.1300 0.8974 0.6405
-1.500 0.3880 0.00560 0.00210 -0.1298 0.8840 0.6468
-1.250 0.4169 0.00567 0.00211 -0.1297 0.8700 0.6507
-1.000 0.4457 0.00570 0.00212 -0.1297 0.8550 0.6548
-0.750 0.4741 0.00577 0.00216 -0.1295 0.8367 0.6585
-0.500 0.5017 0.00590 0.00218 -0.1291 0.8044 0.6612
-0.250 0.5277 0.00619 0.00222 -0.1284 0.7443 0.6641
0.000 0.5494 0.00696 0.00240 -0.1270 0.6112 0.6671
0.250 0.5710 0.00792 0.00270 -0.1259 0.4585 0.6701
0.500 0.5944 0.00868 0.00296 -0.1251 0.3355 0.6729
0.750 0.6197 0.00925 0.00318 -0.1247 0.2529 0.6748
1.000 0.6458 0.00972 0.00338 -0.1244 0.1923 0.6766
1.250 0.6726 0.01009 0.00357 -0.1242 0.1496 0.6785
1.500 0.6998 0.01041 0.00374 -0.1240 0.1225 0.6804
1.750 0.7274 0.01066 0.00391 -0.1239 0.1054 0.6824
2.000 0.7551 0.01091 0.00408 -0.1238 0.0913 0.6843
2.250 0.7828 0.01117 0.00427 -0.1236 0.0804 0.6861
2.500 0.8102 0.01141 0.00446 -0.1235 0.0710 0.6884
2.750 0.8378 0.01160 0.00465 -0.1233 0.0656 0.6905
3.000 0.8651 0.01186 0.00487 -0.1231 0.0598 0.6923
3.250 0.8923 0.01211 0.00509 -0.1228 0.0550 0.6942
3.500 0.9194 0.01236 0.00534 -0.1226 0.0512 0.6961
3.750 0.9466 0.01261 0.00557 -0.1223 0.0482 0.6982
4.000 0.9732 0.01294 0.00588 -0.1220 0.0451 0.7002
4.250 1.0005 0.01316 0.00611 -0.1218 0.0432 0.7020
4.500 1.0273 0.01344 0.00637 -0.1215 0.0413 0.7036
4.750 1.0530 0.01384 0.00676 -0.1210 0.0390 0.7059
5.000 1.0799 0.01405 0.00701 -0.1206 0.0378 0.7081
5.250 1.1063 0.01431 0.00729 -0.1203 0.0364 0.7101
5.500 1.1322 0.01464 0.00762 -0.1198 0.0350 0.7121
5.750 1.1567 0.01515 0.00814 -0.1190 0.0334 0.7142
6.000 1.1829 0.01542 0.00844 -0.1186 0.0326 0.7164
6.250 1.2087 0.01573 0.00878 -0.1181 0.0316 0.7185
6.500 1.2341 0.01607 0.00912 -0.1176 0.0306 0.7204
6.750 1.2587 0.01651 0.00956 -0.1169 0.0295 0.7225
7.000 1.2815 0.01712 0.01022 -0.1159 0.0284 0.7251
7.250 1.3066 0.01743 0.01058 -0.1152 0.0278 0.7274
7.500 1.3313 0.01778 0.01097 -0.1146 0.0270 0.7297
7.750 1.3557 0.01814 0.01136 -0.1138 0.0262 0.7322
8.000 1.3796 0.01855 0.01178 -0.1130 0.0255 0.7347
8.250 1.4010 0.01923 0.01248 -0.1118 0.0246 0.7371
8.500 1.4225 0.01990 0.01320 -0.1106 0.0240 0.7389
8.750 1.4457 0.02029 0.01366 -0.1097 0.0236 0.7417
9.000 1.4680 0.02076 0.01419 -0.1087 0.0231 0.7440
9.250 1.4899 0.02125 0.01474 -0.1075 0.0226 0.7462
9.500 1.5112 0.02176 0.01530 -0.1063 0.0221 0.7486
9.750 1.5321 0.02229 0.01587 -0.1050 0.0217 0.7510
10.000 1.5516 0.02291 0.01652 -0.1036 0.0213 0.7534
10.250 1.5677 0.02384 0.01749 -0.1016 0.0207 0.7555
10.500 1.5806 0.02497 0.01873 -0.0991 0.0203 0.7579
10.750 1.5980 0.02556 0.01940 -0.0972 0.0201 0.7603
11.000 1.6138 0.02622 0.02015 -0.0951 0.0199 0.7627
11.250 1.6277 0.02695 0.02097 -0.0928 0.0197 0.7652
11.500 1.6376 0.02772 0.02183 -0.0897 0.0194 0.7678
11.750 1.6483 0.02858 0.02278 -0.0869 0.0192 0.7704
12.000 1.6592 0.02948 0.02375 -0.0842 0.0189 0.7727
12.250 1.6701 0.03039 0.02475 -0.0817 0.0187 0.7755
12.500 1.6799 0.03138 0.02583 -0.0791 0.0185 0.7780
12.750 1.6900 0.03236 0.02688 -0.0767 0.0183 0.7805
13.000 1.6984 0.03348 0.02808 -0.0742 0.0180 0.7831
13.250 1.7058 0.03472 0.02940 -0.0717 0.0179 0.7856
13.500 1.7105 0.03621 0.03097 -0.0691 0.0177 0.7878
13.750 1.7122 0.03799 0.03285 -0.0663 0.0175 0.7903
14.000 1.7093 0.04024 0.03523 -0.0634 0.0173 0.7926
14.250 1.7022 0.04298 0.03812 -0.0605 0.0171 0.7948
14.500 1.6896 0.04645 0.04177 -0.0578 0.0170 0.7969
14.750 1.6894 0.04879 0.04424 -0.0562 0.0169 0.7993
15.000 1.6859 0.05161 0.04719 -0.0547 0.0168 0.8015
15.250 1.6829 0.05454 0.05025 -0.0538 0.0168 0.8034
15.500 1.6762 0.05807 0.05392 -0.0531 0.0167 0.8055
15.750 1.6671 0.06209 0.05810 -0.0530 0.0167 0.8074
16.000 1.6563 0.06673 0.06290 -0.0536 0.0166 0.8093
16.250 1.6426 0.07220 0.06853 -0.0551 0.0166 0.8111
16.500 1.6251 0.07876 0.07527 -0.0578 0.0165 0.8128
16.750 1.6035 0.08657 0.08326 -0.0616 0.0165 0.8144
17.000 1.5782 0.09567 0.09255 -0.0667 0.0165 0.8156
17.250 1.5461 0.10656 0.10364 -0.0733 0.0165 0.8165
17.500 1.5051 0.11955 0.11685 -0.0813 0.0165 0.8169
17.750 1.4568 0.13457 0.13209 -0.0911 0.0166 0.8169
18.000 1.3922 0.15415 0.15192 -0.1045 0.0167 0.8160
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