XFOIL Version 6.96 Calculated polar for: SC(2)-0714 Supercritical airfoil (coordinates fr 1 1 Reynolds number fixed Mach number fixed xtrf = 1.000 (top) 1.000 (bottom) Mach = 0.000 Re = 0.500 e 6 Ncrit = 5.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------ -------- --------- --------- -------- -------- -------- -19.750 -1.0210 0.10796 0.10407 -0.0505 1.0000 0.0237 -19.500 -1.0451 0.09970 0.09566 -0.0550 1.0000 0.0239 -19.250 -1.0647 0.09246 0.08828 -0.0589 1.0000 0.0240 -19.000 -1.0805 0.08602 0.08170 -0.0624 1.0000 0.0241 -18.750 -1.0933 0.08028 0.07584 -0.0654 1.0000 0.0243 -18.500 -1.1035 0.07509 0.07051 -0.0680 1.0000 0.0244 -18.250 -1.1113 0.07044 0.06575 -0.0703 1.0000 0.0246 -18.000 -1.1172 0.06623 0.06142 -0.0722 1.0000 0.0248 -17.750 -1.1212 0.06245 0.05753 -0.0737 1.0000 0.0250 -17.500 -1.1236 0.05902 0.05399 -0.0750 1.0000 0.0252 -17.250 -1.1249 0.05589 0.05076 -0.0759 1.0000 0.0254 -17.000 -1.1250 0.05308 0.04784 -0.0766 1.0000 0.0256 -16.750 -1.1238 0.05054 0.04519 -0.0770 1.0000 0.0259 -16.500 -1.1220 0.04823 0.04278 -0.0770 1.0000 0.0261 -16.250 -1.1219 0.04591 0.04040 -0.0769 1.0000 0.0263 -16.000 -1.1214 0.04377 0.03821 -0.0765 1.0000 0.0266 -15.750 -1.1195 0.04191 0.03630 -0.0759 1.0000 0.0269 -15.500 -1.1173 0.04023 0.03457 -0.0750 1.0000 0.0271 -15.250 -1.1149 0.03873 0.03303 -0.0738 1.0000 0.0274 -15.000 -1.1128 0.03737 0.03162 -0.0723 1.0000 0.0277 -14.750 -1.1111 0.03611 0.03031 -0.0705 1.0000 0.0280 -14.500 -1.1095 0.03496 0.02911 -0.0685 1.0000 0.0283 -14.250 -1.1088 0.03385 0.02795 -0.0662 1.0000 0.0287 -14.000 -1.1071 0.03281 0.02687 -0.0639 0.9999 0.0290 -13.750 -1.0891 0.03158 0.02556 -0.0648 0.9986 0.0295 -13.500 -1.0707 0.03045 0.02435 -0.0656 0.9970 0.0300 -13.250 -1.0511 0.02940 0.02323 -0.0664 0.9954 0.0304 -13.000 -1.0318 0.02822 0.02200 -0.0675 0.9938 0.0310 -12.750 -1.0122 0.02718 0.02095 -0.0683 0.9921 0.0316 -12.500 -0.9949 0.02631 0.02004 -0.0684 0.9892 0.0323 -12.250 -0.9749 0.02550 0.01920 -0.0688 0.9866 0.0330 -12.000 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0.0575 -7.250 -0.3942 0.01392 0.00733 -0.0981 0.9559 0.0609 -7.000 -0.3594 0.01355 0.00698 -0.1002 0.9551 0.0649 -6.750 -0.3241 0.01318 0.00665 -0.1024 0.9544 0.0706 -6.500 -0.2886 0.01283 0.00634 -0.1045 0.9537 0.0769 -6.000 -0.2283 0.01228 0.00588 -0.1065 0.9485 0.0930 -5.750 -0.1952 0.01198 0.00564 -0.1081 0.9466 0.1027 -5.500 -0.1613 0.01170 0.00540 -0.1098 0.9450 0.1130 -5.250 -0.1265 0.01139 0.00517 -0.1117 0.9436 0.1266 -5.000 -0.0903 0.01102 0.00492 -0.1140 0.9424 0.1499 -4.750 -0.0530 0.01060 0.00466 -0.1167 0.9414 0.1846 -4.500 -0.0141 0.01011 0.00438 -0.1198 0.9405 0.2327 -4.250 0.0289 0.00942 0.00402 -0.1241 0.9399 0.3130 -4.000 0.0747 0.00863 0.00363 -0.1292 0.9395 0.4176 -3.750 0.1173 0.00808 0.00354 -0.1331 0.9389 0.5266 -3.500 0.1491 0.00806 0.00360 -0.1339 0.9365 0.5658 -3.250 0.1779 0.00807 0.00365 -0.1339 0.9324 0.5798 -3.000 0.2088 0.00805 0.00365 -0.1344 0.9286 0.5888 -2.750 0.2418 0.00797 0.00355 -0.1352 0.9247 0.5982 -2.500 0.2716 0.00797 0.00359 -0.1353 0.9193 0.6079 -2.250 0.3010 0.00798 0.00359 -0.1352 0.9118 0.6184 -2.000 0.3311 0.00798 0.00359 -0.1352 0.9026 0.6264 -1.750 0.3615 0.00790 0.00344 -0.1353 0.8854 0.6320 -1.500 0.3906 0.00783 0.00331 -0.1351 0.8619 0.6341 -1.250 0.4195 0.00784 0.00324 -0.1349 0.8338 0.6362 -1.000 0.4478 0.00794 0.00322 -0.1346 0.8027 0.6388 -0.750 0.4742 0.00816 0.00321 -0.1338 0.7459 0.6410 -0.500 0.4955 0.00874 0.00332 -0.1322 0.6485 0.6430 -0.250 0.5159 0.00946 0.00354 -0.1306 0.5457 0.6451 0.000 0.5375 0.01019 0.00379 -0.1295 0.4429 0.6470 0.250 0.5614 0.01079 0.00400 -0.1288 0.3607 0.6485 0.500 0.5862 0.01134 0.00419 -0.1283 0.2888 0.6499 1.000 0.6374 0.01213 0.00459 -0.1274 0.1977 0.6525 1.250 0.6633 0.01251 0.00480 -0.1270 0.1623 0.6538 1.500 0.6897 0.01283 0.00500 -0.1267 0.1382 0.6549 1.750 0.7165 0.01312 0.00520 -0.1264 0.1204 0.6562 2.000 0.7434 0.01340 0.00539 -0.1262 0.1067 0.6575 2.250 0.7704 0.01365 0.00559 -0.1260 0.0958 0.6588 2.500 0.7974 0.01391 0.00580 -0.1257 0.0861 0.6604 2.750 0.8243 0.01418 0.00602 -0.1254 0.0782 0.6622 3.000 0.8510 0.01446 0.00625 -0.1252 0.0719 0.6641 3.250 0.8780 0.01472 0.00648 -0.1249 0.0678 0.6658 3.500 0.9047 0.01501 0.00672 -0.1246 0.0640 0.6673 3.750 0.9310 0.01528 0.00699 -0.1242 0.0614 0.6685 4.000 0.9572 0.01553 0.00727 -0.1238 0.0592 0.6697 4.250 0.9829 0.01583 0.00756 -0.1233 0.0568 0.6708 4.500 1.0081 0.01618 0.00790 -0.1227 0.0545 0.6720 4.750 1.0337 0.01648 0.00822 -0.1222 0.0529 0.6734 5.000 1.0592 0.01677 0.00855 -0.1216 0.0513 0.6749 5.250 1.0844 0.01710 0.00889 -0.1210 0.0497 0.6764 5.500 1.1092 0.01746 0.00924 -0.1204 0.0480 0.6779 5.750 1.1334 0.01787 0.00965 -0.1196 0.0464 0.6794 6.000 1.1584 0.01817 0.00999 -0.1190 0.0450 0.6808 6.250 1.1830 0.01851 0.01035 -0.1183 0.0435 0.6823 6.500 1.2072 0.01887 0.01073 -0.1176 0.0422 0.6838 6.750 1.2308 0.01928 0.01113 -0.1168 0.0410 0.6851 7.000 1.2536 0.01972 0.01159 -0.1157 0.0399 0.6864 7.250 1.2765 0.02011 0.01204 -0.1147 0.0389 0.6876 7.500 1.2991 0.02051 0.01249 -0.1137 0.0378 0.6889 7.750 1.3213 0.02092 0.01293 -0.1126 0.0367 0.6903 8.000 1.3428 0.02137 0.01340 -0.1114 0.0357 0.6917 8.250 1.3629 0.02192 0.01396 -0.1100 0.0348 0.6932 8.500 1.3831 0.02241 0.01451 -0.1086 0.0341 0.6948 8.750 1.4025 0.02291 0.01507 -0.1070 0.0334 0.6964 9.000 1.4207 0.02343 0.01565 -0.1052 0.0328 0.6981 9.250 1.4367 0.02396 0.01623 -0.1031 0.0321 0.6998 9.500 1.4536 0.02453 0.01684 -0.1011 0.0315 0.7015 9.750 1.4706 0.02515 0.01749 -0.0993 0.0309 0.7032 10.000 1.4867 0.02584 0.01822 -0.0973 0.0303 0.7047 10.250 1.5011 0.02665 0.01909 -0.0952 0.0297 0.7063 10.500 1.5173 0.02733 0.01987 -0.0933 0.0293 0.7079 10.750 1.5328 0.02806 0.02069 -0.0914 0.0288 0.7096 11.000 1.5475 0.02885 0.02156 -0.0894 0.0284 0.7113 11.250 1.5615 0.02969 0.02247 -0.0874 0.0279 0.7131 11.500 1.5749 0.03057 0.02344 -0.0853 0.0275 0.7149 11.750 1.5878 0.03150 0.02443 -0.0833 0.0271 0.7167 12.000 1.5999 0.03249 0.02549 -0.0812 0.0268 0.7185 12.250 1.6109 0.03356 0.02662 -0.0791 0.0264 0.7201 12.500 1.6207 0.03473 0.02787 -0.0770 0.0261 0.7217 12.750 1.6287 0.03604 0.02927 -0.0747 0.0258 0.7232 13.000 1.6344 0.03757 0.03088 -0.0723 0.0255 0.7249 13.250 1.6411 0.03906 0.03248 -0.0701 0.0253 0.7267 13.500 1.6480 0.04057 0.03411 -0.0681 0.0251 0.7287 13.750 1.6538 0.04221 0.03587 -0.0661 0.0249 0.7307 14.000 1.6585 0.04399 0.03778 -0.0643 0.0247 0.7326 14.250 1.6622 0.04593 0.03984 -0.0625 0.0245 0.7345 14.500 1.6645 0.04805 0.04207 -0.0609 0.0243 0.7363 14.750 1.6656 0.05036 0.04451 -0.0594 0.0240 0.7378 15.000 1.6656 0.05286 0.04714 -0.0581 0.0239 0.7393 15.250 1.6642 0.05561 0.05003 -0.0570 0.0237 0.7408 15.500 1.6614 0.05867 0.05323 -0.0563 0.0235 0.7425 15.750 1.6577 0.06200 0.05670 -0.0559 0.0233 0.7442 16.000 1.6528 0.06570 0.06053 -0.0559 0.0232 0.7460 16.250 1.6463 0.06983 0.06480 -0.0564 0.0230 0.7477 16.500 1.6383 0.07441 0.06953 -0.0575 0.0229 0.7494 16.750 1.6277 0.07962 0.07489 -0.0591 0.0228 0.7509 17.000 1.6154 0.08538 0.08080 -0.0614 0.0226 0.7522 17.250 1.5998 0.09200 0.08758 -0.0644 0.0225 0.7534 17.500 1.5818 0.09931 0.09506 -0.0681 0.0224 0.7545 17.750 1.5605 0.10741 0.10333 -0.0725 0.0224 0.7554 18.000 1.5357 0.11642 0.11252 -0.0778 0.0223 0.7561 18.250 1.5085 0.12615 0.12244 -0.0837 0.0223 0.7567 18.500 1.4793 0.13653 0.13299 -0.0904 0.0222 0.7573 18.750 1.4478 0.14771 0.14436 -0.0980 0.0221 0.7577 19.000 1.4141 0.15991 0.15674 -0.1067 0.0220 0.7581