XFOIL Version 6.96 Calculated polar for: WORTMANN FX 75-193 1 1 Reynolds number fixed Mach number fixed xtrf = 1.000 (top) 1.000 (bottom) Mach = 0.000 Re = 0.200 e 6 Ncrit = 5.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------ -------- --------- --------- -------- -------- -------- -14.750 -0.2453 0.07984 0.07445 -0.1516 0.8182 0.0132 -14.500 -0.2831 0.06945 0.06384 -0.1580 0.8177 0.0131 -14.250 -0.3117 0.06217 0.05634 -0.1618 0.8172 0.0129 -14.000 -0.3273 0.05750 0.05150 -0.1639 0.8165 0.0129 -13.750 -0.3409 0.05351 0.04731 -0.1651 0.8157 0.0130 -13.500 -0.3542 0.04982 0.04341 -0.1656 0.8149 0.0129 -13.250 -0.3604 0.04718 0.04061 -0.1656 0.8141 0.0130 -13.000 -0.3657 0.04469 0.03792 -0.1652 0.8131 0.0132 -12.750 -0.3682 0.04247 0.03551 -0.1645 0.8122 0.0133 -12.500 -0.3669 0.04059 0.03346 -0.1636 0.8110 0.0133 -12.250 -0.3628 0.03897 0.03169 -0.1627 0.8097 0.0133 -12.000 -0.3569 0.03742 0.02997 -0.1616 0.8084 0.0134 -11.750 -0.3486 0.03610 0.02852 -0.1607 0.8074 0.0135 -11.500 -0.3388 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-1.250 0.2411 0.02272 0.01613 -0.0959 0.7229 0.6807 -1.000 0.2274 0.02343 0.01689 -0.0891 0.7134 0.6838 -0.750 0.2533 0.02329 0.01667 -0.0891 0.7113 0.6867 -0.500 0.2842 0.02304 0.01634 -0.0902 0.7099 0.6898 -0.250 0.3182 0.02271 0.01591 -0.0921 0.7089 0.6934 0.000 0.3285 0.02285 0.01604 -0.0893 0.7047 0.6949 0.250 0.3812 0.02223 0.01535 -0.0935 0.7072 0.6960 0.750 0.3850 0.02282 0.01596 -0.0853 0.6940 0.7001 1.000 0.4168 0.02250 0.01561 -0.0861 0.6932 0.7019 1.250 0.4494 0.02216 0.01523 -0.0872 0.6924 0.7039 1.750 0.4617 0.02334 0.01635 -0.0821 0.6783 0.7100 2.000 0.4914 0.02304 0.01605 -0.0825 0.6774 0.7111 2.250 0.5221 0.02270 0.01571 -0.0830 0.6765 0.7123 3.250 0.5939 0.02352 0.01657 -0.0783 0.6587 0.7190 3.750 0.6251 0.02421 0.01728 -0.0757 0.6470 0.7232 4.000 0.6577 0.02385 0.01692 -0.0766 0.6457 0.7250 4.250 0.6915 0.02346 0.01653 -0.0778 0.6446 0.7265 4.750 0.7186 0.02438 0.01751 -0.0747 0.6317 0.7291 5.000 0.7505 0.02397 0.01713 -0.0753 0.6298 0.7302 5.250 0.7859 0.02341 0.01660 -0.0764 0.6283 0.7314 5.750 0.8176 0.02412 0.01741 -0.0737 0.6152 0.7338 6.000 0.8517 0.02367 0.01699 -0.0748 0.6128 0.7349 6.250 0.8898 0.02308 0.01643 -0.0763 0.6111 0.7358 6.750 0.9210 0.02390 0.01736 -0.0737 0.5969 0.7382 7.000 0.9616 0.02318 0.01666 -0.0756 0.5937 0.7394 7.250 0.9660 0.02412 0.01767 -0.0729 0.5840 0.7409 7.500 0.9930 0.02404 0.01764 -0.0731 0.5785 0.7421 7.750 1.0327 0.02342 0.01704 -0.0748 0.5747 0.7429 8.000 1.0312 0.02461 0.01830 -0.0715 0.5630 0.7438 8.250 1.0581 0.02443 0.01812 -0.0715 0.5525 0.7445 8.500 1.0780 0.02455 0.01825 -0.0706 0.5400 0.7454 8.750 1.0892 0.02501 0.01870 -0.0686 0.5230 0.7463 9.000 1.1018 0.02543 0.01909 -0.0668 0.5044 0.7472 9.250 1.1107 0.02602 0.01960 -0.0646 0.4796 0.7479 9.500 1.1159 0.02686 0.02032 -0.0620 0.4521 0.7485 9.750 1.1218 0.02775 0.02108 -0.0596 0.4270 0.7492 10.000 1.1239 0.02892 0.02216 -0.0570 0.3986 0.7500 10.250 1.1212 0.03040 0.02348 -0.0539 0.3666 0.7509 10.500 1.1173 0.03211 0.02501 -0.0509 0.3339 0.7516 10.750 1.1124 0.03401 0.02674 -0.0481 0.3008 0.7522 11.000 1.1076 0.03606 0.02862 -0.0455 0.2674 0.7526 11.250 1.0997 0.03846 0.03081 -0.0429 0.2290 0.7530 11.500 1.0912 0.04107 0.03319 -0.0404 0.1893 0.7535 11.750 1.0846 0.04369 0.03559 -0.0384 0.1514 0.7542 12.000 1.0783 0.04640 0.03808 -0.0366 0.1144 0.7548 12.250 1.0762 0.04888 0.04041 -0.0352 0.0864 0.7553 12.500 1.0751 0.05137 0.04277 -0.0340 0.0655 0.7556 12.750 1.0781 0.05358 0.04492 -0.0332 0.0499 0.7559 13.000 1.0816 0.05582 0.04713 -0.0325 0.0411 0.7562 13.250 1.0874 0.05789 0.04924 -0.0320 0.0340 0.7565 13.500 1.0931 0.06004 0.05142 -0.0315 0.0280 0.7568 13.750 1.0985 0.06225 0.05366 -0.0312 0.0240 0.7571 14.250 1.1088 0.06686 0.05839 -0.0307 0.0199 0.7578 14.500 1.1124 0.06942 0.06100 -0.0305 0.0187 0.7581 14.750 1.1181 0.07180 0.06348 -0.0305 0.0179 0.7584 15.000 1.1225 0.07436 0.06615 -0.0305 0.0170 0.7587 15.250 1.1268 0.07699 0.06887 -0.0306 0.0163 0.7590 15.500 1.1298 0.07981 0.07178 -0.0308 0.0159 0.7593 15.750 1.1331 0.08266 0.07472 -0.0311 0.0154 0.7596 16.000 1.1367 0.08551 0.07768 -0.0315 0.0151 0.7599 16.250 1.1402 0.08842 0.08069 -0.0319 0.0147 0.7603 16.500 1.1433 0.09139 0.08378 -0.0324 0.0145 0.7608 16.750 1.1465 0.09438 0.08687 -0.0331 0.0141 0.7613 17.000 1.1496 0.09743 0.09001 -0.0338 0.0139 0.7617