NASA SC(2)-0714 AIRFOIL (sc20714-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
Details | Polar file |
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Airfoil: NASA SC(2)-0714 AIRFOIL (sc20714-il) Reynolds number: 1,000,000 Max Cl/Cd: 79.99 at α=7° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-sc20714-il-1000000-n5.txt Download as CSV file: xf-sc20714-il-1000000-n5.csv |
XFOIL Version 6.96 Calculated polar for: NASA SC(2)-0714 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 = 5.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------ -------- --------- --------- -------- -------- -------- -19.750 -1.2574 0.07089 0.06684 -0.0687 1.0000 0.0193 -19.500 -1.2653 0.06638 0.06222 -0.0708 1.0000 0.0194 -19.250 -1.2703 0.06238 0.05813 -0.0726 1.0000 0.0196 -19.000 -1.2730 0.05881 0.05447 -0.0741 1.0000 0.0197 -18.750 -1.2740 0.05560 0.05117 -0.0753 1.0000 0.0199 -18.500 -1.2734 0.05269 0.04818 -0.0763 1.0000 0.0200 -18.250 -1.2713 0.05005 0.04546 -0.0770 1.0000 0.0202 -18.000 -1.2683 0.04761 0.04295 -0.0776 1.0000 0.0203 -17.750 -1.2643 0.04542 0.04067 -0.0779 1.0000 0.0205 -17.500 -1.2595 0.04339 0.03858 -0.0780 1.0000 0.0206 -17.250 -1.2549 0.04148 0.03660 -0.0779 1.0000 0.0207 -17.000 -1.2526 0.03950 0.03456 -0.0776 1.0000 0.0209 -16.750 -1.2504 0.03766 0.03267 -0.0769 1.0000 0.0212 -16.500 -1.2473 0.03605 0.03102 -0.0760 1.0000 0.0214 -16.250 -1.2442 0.03463 0.02955 -0.0748 1.0000 0.0216 -16.000 -1.2419 0.03334 0.02822 -0.0731 1.0000 0.0218 -15.750 -1.2404 0.03218 0.02702 -0.0711 1.0000 0.0220 -15.500 -1.2314 0.03098 0.02579 -0.0705 0.9995 0.0223 -15.250 -1.2144 0.02975 0.02451 -0.0713 0.9986 0.0226 -15.000 -1.1959 0.02861 0.02332 -0.0721 0.9974 0.0229 -14.750 -1.1765 0.02750 0.02217 -0.0731 0.9960 0.0232 -14.500 -1.1557 0.02648 0.02110 -0.0741 0.9948 0.0236 -14.250 -1.1340 0.02552 0.02010 -0.0752 0.9937 0.0239 -14.000 -1.1117 0.02460 0.01913 -0.0763 0.9928 0.0242 -13.750 -1.0945 0.02373 0.01823 -0.0763 0.9904 0.0245 -13.500 -1.0756 0.02282 0.01730 -0.0767 0.9881 0.0250 -13.250 -1.0546 0.02199 0.01645 -0.0773 0.9861 0.0255 -13.000 -1.0313 0.02123 0.01568 -0.0782 0.9845 0.0261 -12.750 -1.0051 0.02052 0.01494 -0.0795 0.9834 0.0268 -12.500 -0.9778 0.01984 0.01424 -0.0810 0.9825 0.0274 -12.250 -0.9498 0.01919 0.01356 -0.0825 0.9815 0.0279 -12.000 -0.9249 0.01859 0.01293 -0.0834 0.9796 0.0284 -11.750 -0.9012 0.01797 0.01231 -0.0840 0.9769 0.0292 -11.500 -0.8745 0.01740 0.01173 -0.0850 0.9749 0.0300 -11.250 -0.8462 0.01686 0.01119 -0.0863 0.9733 0.0308 -11.000 -0.8169 0.01636 0.01068 -0.0877 0.9719 0.0317 -10.750 -0.7870 0.01590 0.01019 -0.0892 0.9705 0.0325 -10.500 -0.7566 0.01538 0.00967 -0.0908 0.9693 0.0336 -10.250 -0.7255 0.01491 0.00921 -0.0924 0.9682 0.0349 -10.000 -0.6970 0.01450 0.00880 -0.0935 0.9662 0.0359 -9.750 -0.6683 0.01413 0.00841 -0.0944 0.9639 0.0369 -9.500 -0.6384 0.01374 0.00801 -0.0957 0.9620 0.0379 -9.250 -0.6076 0.01332 0.00762 -0.0971 0.9603 0.0393 -9.000 -0.5763 0.01295 0.00725 -0.0986 0.9586 0.0407 -8.750 -0.5445 0.01262 0.00691 -0.1000 0.9571 0.0421 -8.500 -0.5122 0.01227 0.00656 -0.1016 0.9557 0.0436 -8.250 -0.4794 0.01192 0.00623 -0.1033 0.9545 0.0454 -8.000 -0.4465 0.01161 0.00593 -0.1049 0.9533 0.0472 -7.750 -0.4152 0.01135 0.00566 -0.1062 0.9515 0.0487 -7.500 -0.3833 0.01104 0.00539 -0.1076 0.9496 0.0515 -7.250 -0.3512 0.01078 0.00515 -0.1089 0.9477 0.0543 -7.000 -0.3188 0.01052 0.00491 -0.1103 0.9459 0.0575 -6.750 -0.2864 0.01028 0.00469 -0.1117 0.9440 0.0610 -6.500 -0.2538 0.01004 0.00447 -0.1130 0.9421 0.0648 -6.250 -0.2208 0.00980 0.00426 -0.1144 0.9403 0.0697 -6.000 -0.1875 0.00957 0.00406 -0.1159 0.9387 0.0758 -5.750 -0.1545 0.00934 0.00389 -0.1173 0.9371 0.0835 -5.500 -0.1222 0.00915 0.00374 -0.1185 0.9349 0.0916 -5.250 -0.0893 0.00893 0.00358 -0.1199 0.9326 0.1011 -5.000 -0.0562 0.00872 0.00343 -0.1213 0.9304 0.1122 -4.750 -0.0225 0.00849 0.00328 -0.1228 0.9284 0.1300 -4.500 0.0117 0.00824 0.00313 -0.1245 0.9265 0.1511 -4.250 0.0467 0.00796 0.00297 -0.1264 0.9246 0.1810 -4.000 0.0821 0.00768 0.00281 -0.1283 0.9224 0.2135 -3.500 0.1568 0.00683 0.00242 -0.1334 0.9123 0.3381 -3.250 0.1977 0.00624 0.00213 -0.1369 0.9047 0.4352 -3.000 0.2362 0.00577 0.00198 -0.1396 0.8923 0.5321 -2.750 0.2669 0.00573 0.00194 -0.1400 0.8769 0.5547 -2.500 0.2971 0.00574 0.00192 -0.1403 0.8634 0.5668 -2.250 0.3266 0.00579 0.00191 -0.1404 0.8408 0.5801 -2.000 0.3545 0.00595 0.00193 -0.1401 0.8002 0.5920 -1.750 0.3804 0.00629 0.00198 -0.1395 0.7352 0.6014 -1.500 0.4031 0.00695 0.00218 -0.1383 0.6269 0.6073 -1.250 0.4257 0.00772 0.00241 -0.1372 0.5021 0.6110 -1.000 0.4504 0.00835 0.00261 -0.1367 0.4049 0.6158 -0.750 0.4767 0.00879 0.00279 -0.1363 0.3360 0.6210 -0.500 0.5033 0.00919 0.00296 -0.1361 0.2793 0.6242 -0.250 0.5307 0.00951 0.00310 -0.1359 0.2367 0.6261 0.000 0.5579 0.00985 0.00325 -0.1358 0.1945 0.6280 0.250 0.5857 0.01011 0.00338 -0.1357 0.1651 0.6300 0.500 0.6135 0.01037 0.00351 -0.1356 0.1428 0.6318 0.750 0.6417 0.01059 0.00364 -0.1356 0.1258 0.6331 1.000 0.6696 0.01082 0.00377 -0.1355 0.1085 0.6339 1.250 0.6977 0.01102 0.00390 -0.1355 0.0977 0.6348 1.500 0.7258 0.01121 0.00405 -0.1354 0.0893 0.6361 1.750 0.7540 0.01138 0.00419 -0.1354 0.0822 0.6375 2.000 0.7818 0.01158 0.00435 -0.1352 0.0752 0.6389 2.250 0.8094 0.01180 0.00452 -0.1351 0.0689 0.6401 2.500 0.8372 0.01199 0.00469 -0.1350 0.0643 0.6412 2.750 0.8648 0.01220 0.00487 -0.1348 0.0606 0.6423 3.000 0.8925 0.01239 0.00505 -0.1346 0.0576 0.6434 3.250 0.9199 0.01261 0.00524 -0.1344 0.0544 0.6446 3.500 0.9473 0.01281 0.00543 -0.1342 0.0524 0.6457 3.750 0.9746 0.01302 0.00563 -0.1340 0.0504 0.6469 4.000 1.0016 0.01326 0.00583 -0.1337 0.0484 0.6480 4.250 1.0286 0.01349 0.00605 -0.1334 0.0469 0.6491 4.500 1.0555 0.01371 0.00628 -0.1330 0.0454 0.6501 4.750 1.0821 0.01396 0.00651 -0.1327 0.0438 0.6511 5.000 1.1084 0.01423 0.00676 -0.1322 0.0423 0.6521 5.250 1.1347 0.01448 0.00702 -0.1318 0.0412 0.6534 5.500 1.1610 0.01471 0.00727 -0.1314 0.0402 0.6549 5.750 1.1870 0.01497 0.00754 -0.1309 0.0390 0.6562 6.000 1.2127 0.01525 0.00783 -0.1304 0.0377 0.6575 6.250 1.2378 0.01557 0.00815 -0.1297 0.0364 0.6587 6.500 1.2634 0.01583 0.00843 -0.1292 0.0355 0.6600 6.750 1.2886 0.01611 0.00873 -0.1285 0.0342 0.6613 7.000 1.3134 0.01642 0.00904 -0.1279 0.0329 0.6626 7.250 1.3376 0.01677 0.00938 -0.1271 0.0316 0.6639 7.500 1.3620 0.01708 0.00972 -0.1263 0.0308 0.6652 7.750 1.3860 0.01741 0.01007 -0.1255 0.0298 0.6665 8.000 1.4095 0.01776 0.01043 -0.1245 0.0288 0.6677 8.250 1.4325 0.01815 0.01081 -0.1235 0.0279 0.6690 8.500 1.4551 0.01855 0.01123 -0.1225 0.0272 0.6703 8.750 1.4774 0.01893 0.01164 -0.1213 0.0266 0.6717 9.000 1.4991 0.01932 0.01207 -0.1201 0.0260 0.6735 9.250 1.5202 0.01974 0.01252 -0.1188 0.0253 0.6751 9.500 1.5407 0.02018 0.01299 -0.1173 0.0247 0.6767 9.750 1.5602 0.02066 0.01349 -0.1157 0.0241 0.6782 10.000 1.5787 0.02119 0.01405 -0.1140 0.0235 0.6799 10.250 1.5971 0.02166 0.01457 -0.1122 0.0232 0.6815 10.500 1.6124 0.02214 0.01510 -0.1098 0.0229 0.6832 10.750 1.6287 0.02267 0.01568 -0.1077 0.0226 0.6848 11.000 1.6451 0.02324 0.01629 -0.1056 0.0223 0.6864 11.250 1.6615 0.02383 0.01693 -0.1036 0.0220 0.6878 11.500 1.6772 0.02447 0.01761 -0.1016 0.0217 0.6891 11.750 1.6926 0.02514 0.01833 -0.0995 0.0214 0.6907 12.000 1.7074 0.02585 0.01910 -0.0974 0.0211 0.6928 12.250 1.7214 0.02661 0.01992 -0.0953 0.0208 0.6949 12.500 1.7344 0.02745 0.02081 -0.0930 0.0205 0.6970 12.750 1.7464 0.02837 0.02180 -0.0907 0.0202 0.6989 13.000 1.7572 0.02937 0.02286 -0.0883 0.0200 0.7008 13.250 1.7693 0.03027 0.02384 -0.0861 0.0198 0.7027 13.500 1.7810 0.03122 0.02487 -0.0839 0.0197 0.7046 13.750 1.7918 0.03225 0.02596 -0.0818 0.0196 0.7063 14.000 1.8017 0.03335 0.02714 -0.0795 0.0194 0.7079 14.250 1.8113 0.03450 0.02836 -0.0774 0.0192 0.7093 14.500 1.8198 0.03575 0.02970 -0.0753 0.0191 0.7113 14.750 1.8281 0.03705 0.03108 -0.0732 0.0188 0.7133 15.000 1.8351 0.03847 0.03260 -0.0711 0.0187 0.7154 15.250 1.8409 0.04003 0.03424 -0.0691 0.0185 0.7174 15.500 1.8459 0.04171 0.03601 -0.0671 0.0183 0.7195 15.750 1.8497 0.04355 0.03794 -0.0653 0.0182 0.7217 16.000 1.8523 0.04554 0.04002 -0.0635 0.0180 0.7238 16.250 1.8535 0.04773 0.04230 -0.0619 0.0179 0.7258 16.500 1.8535 0.05015 0.04482 -0.0604 0.0178 0.7275 17.000 1.8497 0.05580 0.05068 -0.0583 0.0175 0.7308 17.250 1.8452 0.05913 0.05412 -0.0577 0.0174 0.7326 17.500 1.8383 0.06296 0.05807 -0.0575 0.0173 0.7343 17.750 1.8294 0.06729 0.06253 -0.0578 0.0172 0.7360 18.000 1.8178 0.07226 0.06764 -0.0587 0.0171 0.7376 18.250 1.8023 0.07808 0.07361 -0.0604 0.0170 0.7391 18.500 1.7829 0.08484 0.08053 -0.0629 0.0170 0.7403 18.750 1.7594 0.09266 0.08852 -0.0664 0.0169 0.7414 19.000 1.7294 0.10198 0.09802 -0.0712 0.0169 0.7422 19.250 1.6939 0.11256 0.10881 -0.0770 0.0169 0.7428 |
Polar data table (+)
Polar graphs
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