NASA SC(2)-0612 AIRFOIL (sc20612-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: NASA SC(2)-0612 AIRFOIL (sc20612-il) Reynolds number: 1,000,000 Max Cl/Cd: 77.94 at α=6.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-sc20612-il-1000000.txt Download as CSV file: xf-sc20612-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: NASA SC(2)-0612 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
------ -------- --------- --------- -------- -------- --------
-19.000 -1.0935 0.10266 0.09984 -0.0343 1.0000 0.0178
-18.750 -1.1235 0.09302 0.09005 -0.0398 1.0000 0.0178
-18.500 -1.1475 0.08463 0.08151 -0.0446 1.0000 0.0178
-18.250 -1.1660 0.07748 0.07422 -0.0488 1.0000 0.0179
-18.000 -1.1808 0.07110 0.06770 -0.0525 1.0000 0.0179
-17.750 -1.1921 0.06555 0.06203 -0.0556 1.0000 0.0180
-17.500 -1.2008 0.06065 0.05701 -0.0582 1.0000 0.0181
-17.250 -1.2070 0.05633 0.05257 -0.0603 1.0000 0.0182
-17.000 -1.2112 0.05251 0.04864 -0.0620 1.0000 0.0183
-16.750 -1.2136 0.04908 0.04511 -0.0634 1.0000 0.0184
-16.500 -1.2146 0.04603 0.04195 -0.0644 1.0000 0.0185
-16.250 -1.2142 0.04331 0.03914 -0.0651 1.0000 0.0187
-16.000 -1.2123 0.04084 0.03658 -0.0656 1.0000 0.0188
-15.750 -1.2090 0.03862 0.03425 -0.0658 1.0000 0.0190
-15.500 -1.2042 0.03659 0.03213 -0.0659 1.0000 0.0192
-15.250 -1.1982 0.03476 0.03021 -0.0659 1.0000 0.0193
-15.000 -1.1909 0.03311 0.02848 -0.0657 1.0000 0.0195
-14.750 -1.1825 0.03164 0.02693 -0.0653 1.0000 0.0196
-14.500 -1.1733 0.03031 0.02553 -0.0648 1.0000 0.0197
-14.250 -1.1691 0.02870 0.02384 -0.0637 1.0000 0.0199
-14.000 -1.1716 0.02691 0.02196 -0.0617 1.0000 0.0202
-13.750 -1.1742 0.02561 0.02062 -0.0589 1.0000 0.0205
-13.500 -1.1808 0.02460 0.01958 -0.0549 1.0000 0.0206
-13.250 -1.1762 0.02360 0.01854 -0.0528 1.0000 0.0209
-13.000 -1.1673 0.02269 0.01759 -0.0513 1.0000 0.0212
-12.750 -1.1547 0.02185 0.01671 -0.0503 1.0000 0.0215
-12.500 -1.1392 0.02105 0.01587 -0.0497 1.0000 0.0218
-12.250 -1.1213 0.02030 0.01506 -0.0494 1.0000 0.0222
-12.000 -1.1014 0.01961 0.01432 -0.0493 1.0000 0.0226
-11.750 -1.0727 0.01898 0.01364 -0.0507 0.9994 0.0231
-11.500 -1.0406 0.01843 0.01303 -0.0526 0.9986 0.0235
-11.250 -1.0096 0.01727 0.01183 -0.0550 0.9976 0.0244
-11.000 -0.9777 0.01661 0.01115 -0.0569 0.9968 0.0252
-10.750 -0.9453 0.01608 0.01059 -0.0587 0.9959 0.0260
-10.500 -0.9123 0.01559 0.01007 -0.0606 0.9952 0.0268
-10.250 -0.8790 0.01516 0.00961 -0.0624 0.9945 0.0275
-10.000 -0.8455 0.01450 0.00892 -0.0645 0.9940 0.0288
-9.750 -0.8117 0.01404 0.00847 -0.0664 0.9935 0.0301
-9.500 -0.7802 0.01367 0.00808 -0.0678 0.9923 0.0314
-9.250 -0.7481 0.01332 0.00771 -0.0691 0.9909 0.0326
-9.000 -0.7149 0.01285 0.00727 -0.0709 0.9897 0.0349
-8.750 -0.6814 0.01256 0.00698 -0.0725 0.9885 0.0370
-8.500 -0.6471 0.01217 0.00661 -0.0743 0.9875 0.0397
-8.250 -0.6129 0.01191 0.00636 -0.0760 0.9865 0.0425
-8.000 -0.5782 0.01159 0.00605 -0.0779 0.9857 0.0455
-7.750 -0.5434 0.01132 0.00580 -0.0797 0.9850 0.0487
-7.500 -0.5087 0.01115 0.00563 -0.0814 0.9843 0.0509
-7.250 -0.4729 0.01076 0.00528 -0.0836 0.9838 0.0550
-7.000 -0.4375 0.01053 0.00505 -0.0854 0.9833 0.0577
-6.750 -0.4019 0.01028 0.00480 -0.0874 0.9828 0.0606
-6.500 -0.3660 0.00999 0.00455 -0.0895 0.9824 0.0646
-6.250 -0.3343 0.00980 0.00436 -0.0904 0.9803 0.0673
-6.000 -0.3009 0.00954 0.00413 -0.0919 0.9785 0.0715
-5.750 -0.2662 0.00929 0.00392 -0.0936 0.9773 0.0769
-5.500 -0.2311 0.00903 0.00371 -0.0954 0.9762 0.0848
-5.250 -0.1960 0.00877 0.00351 -0.0972 0.9750 0.0967
-5.000 -0.1604 0.00845 0.00330 -0.0991 0.9739 0.1190
-4.750 -0.1235 0.00802 0.00308 -0.1015 0.9730 0.1605
-4.500 -0.0859 0.00752 0.00284 -0.1042 0.9720 0.2222
-4.250 -0.0474 0.00695 0.00260 -0.1071 0.9710 0.3044
-4.000 -0.0085 0.00636 0.00235 -0.1102 0.9700 0.3993
-3.750 0.0286 0.00575 0.00215 -0.1127 0.9670 0.5166
-3.500 0.0606 0.00557 0.00211 -0.1136 0.9621 0.5635
-3.250 0.0918 0.00550 0.00207 -0.1141 0.9580 0.5845
-3.000 0.1219 0.00547 0.00205 -0.1144 0.9532 0.5968
-2.750 0.1503 0.00544 0.00200 -0.1142 0.9454 0.6063
-2.500 0.1784 0.00540 0.00197 -0.1139 0.9353 0.6144
-2.250 0.2068 0.00540 0.00192 -0.1136 0.9249 0.6231
-2.000 0.2352 0.00541 0.00194 -0.1134 0.9136 0.6311
-1.750 0.2637 0.00545 0.00192 -0.1132 0.8994 0.6381
-1.500 0.2921 0.00547 0.00194 -0.1130 0.8847 0.6442
-1.250 0.3208 0.00556 0.00200 -0.1129 0.8705 0.6516
-1.000 0.3493 0.00564 0.00203 -0.1127 0.8527 0.6579
-0.750 0.3776 0.00574 0.00208 -0.1125 0.8338 0.6620
-0.500 0.4061 0.00584 0.00211 -0.1124 0.8104 0.6651
-0.250 0.4341 0.00599 0.00215 -0.1121 0.7786 0.6683
0.000 0.4615 0.00624 0.00220 -0.1118 0.7328 0.6708
0.250 0.4864 0.00670 0.00228 -0.1111 0.6376 0.6736
0.500 0.5090 0.00756 0.00253 -0.1101 0.4886 0.6759
0.750 0.5334 0.00830 0.00277 -0.1096 0.3693 0.6779
1.000 0.5588 0.00890 0.00298 -0.1092 0.2760 0.6798
1.250 0.5852 0.00938 0.00318 -0.1090 0.2094 0.6817
1.500 0.6119 0.00981 0.00337 -0.1088 0.1573 0.6838
1.750 0.6392 0.01017 0.00355 -0.1087 0.1221 0.6859
2.000 0.6669 0.01047 0.00373 -0.1086 0.0991 0.6878
2.250 0.6947 0.01075 0.00391 -0.1085 0.0846 0.6893
2.500 0.7228 0.01090 0.00405 -0.1085 0.0782 0.6919
2.750 0.7505 0.01114 0.00425 -0.1084 0.0720 0.6939
3.000 0.7786 0.01130 0.00443 -0.1083 0.0687 0.6957
3.250 0.8063 0.01154 0.00463 -0.1082 0.0646 0.6975
3.500 0.8339 0.01177 0.00485 -0.1080 0.0616 0.6993
3.750 0.8618 0.01195 0.00504 -0.1079 0.0593 0.7012
4.000 0.8893 0.01219 0.00526 -0.1078 0.0563 0.7030
4.250 0.9165 0.01246 0.00552 -0.1076 0.0532 0.7048
4.500 0.9443 0.01265 0.00571 -0.1074 0.0510 0.7064
4.750 0.9714 0.01291 0.00594 -0.1072 0.0482 0.7081
5.000 0.9984 0.01316 0.00620 -0.1070 0.0454 0.7107
5.250 1.0257 0.01334 0.00640 -0.1068 0.0428 0.7129
5.500 1.0519 0.01368 0.00672 -0.1064 0.0397 0.7150
5.750 1.0789 0.01389 0.00695 -0.1061 0.0377 0.7171
6.000 1.1052 0.01420 0.00724 -0.1058 0.0354 0.7192
6.250 1.1312 0.01456 0.00761 -0.1053 0.0336 0.7212
6.500 1.1574 0.01485 0.00791 -0.1049 0.0321 0.7233
6.750 1.1832 0.01521 0.00826 -0.1045 0.0307 0.7252
7.000 1.2078 0.01571 0.00877 -0.1038 0.0292 0.7270
7.250 1.2335 0.01601 0.00912 -0.1033 0.0284 0.7296
7.500 1.2588 0.01635 0.00950 -0.1028 0.0275 0.7318
7.750 1.2836 0.01674 0.00991 -0.1022 0.0265 0.7339
8.000 1.3072 0.01727 0.01046 -0.1013 0.0255 0.7360
8.250 1.3300 0.01789 0.01113 -0.1004 0.0248 0.7381
8.500 1.3542 0.01830 0.01159 -0.0996 0.0243 0.7403
8.750 1.3779 0.01876 0.01209 -0.0988 0.0238 0.7424
9.000 1.4012 0.01925 0.01262 -0.0980 0.0232 0.7442
9.250 1.4240 0.01974 0.01315 -0.0971 0.0227 0.7464
9.500 1.4461 0.02028 0.01374 -0.0961 0.0223 0.7489
9.750 1.4664 0.02098 0.01449 -0.0947 0.0217 0.7512
10.000 1.4825 0.02211 0.01570 -0.0928 0.0211 0.7536
10.250 1.5028 0.02274 0.01640 -0.0915 0.0209 0.7561
10.500 1.5231 0.02332 0.01706 -0.0902 0.0207 0.7585
10.750 1.5425 0.02397 0.01778 -0.0887 0.0204 0.7609
11.000 1.5608 0.02467 0.01855 -0.0871 0.0201 0.7629
11.250 1.5780 0.02538 0.01935 -0.0854 0.0198 0.7656
11.500 1.5939 0.02611 0.02016 -0.0834 0.0195 0.7681
11.750 1.6088 0.02681 0.02094 -0.0813 0.0192 0.7705
12.000 1.6217 0.02756 0.02175 -0.0789 0.0189 0.7730
12.250 1.6300 0.02837 0.02263 -0.0758 0.0187 0.7756
12.500 1.6393 0.02933 0.02365 -0.0729 0.0185 0.7781
12.750 1.6471 0.03044 0.02483 -0.0701 0.0183 0.7802
13.000 1.6524 0.03177 0.02626 -0.0671 0.0181 0.7831
13.250 1.6538 0.03345 0.02806 -0.0638 0.0179 0.7857
13.500 1.6480 0.03581 0.03059 -0.0601 0.0176 0.7881
13.750 1.6483 0.03775 0.03266 -0.0573 0.0175 0.7907
14.000 1.6528 0.03934 0.03437 -0.0551 0.0174 0.7934
14.250 1.6564 0.04109 0.03623 -0.0530 0.0174 0.7959
14.500 1.6581 0.04309 0.03835 -0.0511 0.0173 0.7984
14.750 1.6577 0.04535 0.04076 -0.0494 0.0172 0.8011
15.000 1.6559 0.04789 0.04344 -0.0479 0.0171 0.8038
15.250 1.6524 0.05076 0.04644 -0.0467 0.0170 0.8064
15.500 1.6464 0.05406 0.04988 -0.0459 0.0169 0.8090
15.750 1.6388 0.05779 0.05375 -0.0457 0.0168 0.8115
16.000 1.6287 0.06213 0.05823 -0.0460 0.0167 0.8136
16.250 1.6154 0.06723 0.06350 -0.0472 0.0167 0.8161
16.500 1.5994 0.07326 0.06971 -0.0494 0.0166 0.8183
16.750 1.5797 0.08050 0.07713 -0.0528 0.0166 0.8203
17.000 1.5561 0.08898 0.08580 -0.0575 0.0166 0.8221
17.250 1.5257 0.09934 0.09636 -0.0636 0.0166 0.8234
17.500 1.4878 0.11156 0.10880 -0.0711 0.0166 0.8242
17.750 1.4409 0.12597 0.12342 -0.0801 0.0167 0.8244
18.000 1.3801 0.14414 0.14184 -0.0920 0.0168 0.8237
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