XFOIL Version 6.96 Calculated polar for: Joukovsky f=0% t=18% 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 -1.3347 0.09531 0.09115 -0.0036 1.0000 0.0385 -19.500 -1.3445 0.09020 0.08596 -0.0062 1.0000 0.0391 -19.250 -1.3541 0.08518 0.08088 -0.0088 1.0000 0.0398 -19.000 -1.3629 0.08040 0.07600 -0.0111 1.0000 0.0403 -18.750 -1.3709 0.07578 0.07131 -0.0133 1.0000 0.0410 -18.500 -1.3769 0.07159 0.06704 -0.0152 1.0000 0.0416 -18.250 -1.3824 0.06753 0.06290 -0.0169 1.0000 0.0421 -18.000 -1.3909 0.06318 0.05847 -0.0187 1.0000 0.0427 -17.750 -1.3977 0.05916 0.05438 -0.0203 1.0000 0.0434 -17.500 -1.4029 0.05542 0.05058 -0.0217 1.0000 0.0441 -17.250 -1.4063 0.05200 0.04709 -0.0228 1.0000 0.0448 -17.000 -1.4086 0.04882 0.04384 -0.0238 1.0000 0.0456 -16.750 -1.4091 0.04591 0.04086 -0.0246 1.0000 0.0463 -16.500 -1.4113 0.04296 0.03785 -0.0252 1.0000 0.0471 -16.250 -1.4130 0.04014 0.03498 -0.0257 1.0000 0.0480 -16.000 -1.4123 0.03763 0.03242 -0.0261 1.0000 0.0488 -15.750 -1.4102 0.03533 0.03007 -0.0262 1.0000 0.0498 -15.500 -1.4060 0.03328 0.02797 -0.0262 1.0000 0.0508 -15.250 -1.4010 0.03137 0.02600 -0.0261 1.0000 0.0517 -15.000 -1.3972 0.02942 0.02401 -0.0259 1.0000 0.0527 -14.750 -1.3920 0.02765 0.02221 -0.0255 1.0000 0.0540 -14.500 -1.3847 0.02613 0.02065 -0.0251 1.0000 0.0551 -14.250 -1.3761 0.02477 0.01925 -0.0245 1.0000 0.0565 -14.000 -1.3682 0.02343 0.01788 -0.0237 1.0000 0.0578 -13.750 -1.3601 0.02217 0.01659 -0.0228 1.0000 0.0592 -13.500 -1.3505 0.02109 0.01549 -0.0218 1.0000 0.0608 -13.250 -1.3394 0.02017 0.01454 -0.0207 1.0000 0.0621 -13.000 -1.3294 0.01928 0.01362 -0.0193 1.0000 0.0636 -12.750 -1.3199 0.01844 0.01277 -0.0177 1.0000 0.0656 -12.500 -1.3087 0.01777 0.01208 -0.0160 1.0000 0.0673 -12.250 -1.2965 0.01722 0.01151 -0.0141 1.0000 0.0688 -12.000 -1.2857 0.01666 0.01095 -0.0118 1.0000 0.0708 -11.750 -1.2688 0.01619 0.01047 -0.0104 1.0000 0.0730 -11.500 -1.2426 0.01583 0.01004 -0.0106 0.9239 0.0754 -11.250 -1.2281 0.01548 0.00960 -0.0085 0.8860 0.0780 -11.000 -1.2093 0.01515 0.00919 -0.0071 0.8618 0.0807 -10.750 -1.1882 0.01485 0.00882 -0.0060 0.8416 0.0832 -10.500 -1.1671 0.01448 0.00842 -0.0050 0.8241 0.0866 -10.250 -1.1441 0.01418 0.00807 -0.0043 0.8088 0.0896 -10.000 -1.1210 0.01386 0.00771 -0.0036 0.7938 0.0929 -9.750 -1.0971 0.01355 0.00738 -0.0030 0.7793 0.0966 -9.500 -1.0725 0.01327 0.00706 -0.0025 0.7667 0.1003 -9.000 -1.0222 0.01273 0.00647 -0.0016 0.7412 0.1082 -8.750 -0.9970 0.01243 0.00616 -0.0012 0.7291 0.1131 -8.500 -0.9707 0.01220 0.00590 -0.0009 0.7173 0.1171 -8.250 -0.9448 0.01193 0.00563 -0.0006 0.7062 0.1223 -8.000 -0.9180 0.01171 0.00539 -0.0003 0.6948 0.1272 -7.750 -0.8915 0.01146 0.00513 -0.0001 0.6837 0.1329 -7.500 -0.8643 0.01126 0.00491 0.0001 0.6728 0.1381 -7.250 -0.8373 0.01103 0.00468 0.0003 0.6620 0.1439 -7.000 -0.8097 0.01084 0.00448 0.0005 0.6515 0.1498 -6.750 -0.7823 0.01064 0.00427 0.0006 0.6408 0.1559 -6.500 -0.7545 0.01045 0.00409 0.0007 0.6308 0.1624 -6.250 -0.7267 0.01027 0.00390 0.0009 0.6200 0.1691 -6.000 -0.6985 0.01010 0.00373 0.0009 0.6107 0.1760 -5.750 -0.6705 0.00993 0.00356 0.0010 0.5998 0.1830 -5.500 -0.6420 0.00978 0.00341 0.0010 0.5907 0.1904 -5.250 -0.6137 0.00962 0.00325 0.0011 0.5800 0.1976 -5.000 -0.5851 0.00949 0.00312 0.0011 0.5706 0.2053 -4.750 -0.5565 0.00934 0.00298 0.0011 0.5607 0.2132 -4.500 -0.5277 0.00924 0.00286 0.0011 0.5508 0.2210 -4.250 -0.4989 0.00910 0.00274 0.0011 0.5412 0.2294 -4.000 -0.4699 0.00901 0.00263 0.0011 0.5311 0.2374 -3.750 -0.4410 0.00889 0.00252 0.0011 0.5218 0.2457 -3.500 -0.4118 0.00881 0.00244 0.0010 0.5116 0.2541 -3.250 -0.3827 0.00870 0.00234 0.0010 0.5027 0.2629 -3.000 -0.3535 0.00863 0.00227 0.0009 0.4925 0.2715 -2.750 -0.3243 0.00854 0.00219 0.0009 0.4838 0.2802 -2.500 -0.2949 0.00849 0.00213 0.0008 0.4737 0.2891 -2.250 -0.2656 0.00842 0.00206 0.0007 0.4648 0.2979 -2.000 -0.2361 0.00836 0.00201 0.0007 0.4549 0.3070 -1.750 -0.2068 0.00832 0.00196 0.0006 0.4455 0.3158 -1.500 -0.1772 0.00827 0.00192 0.0005 0.4362 0.3251 -1.250 -0.1478 0.00825 0.00189 0.0004 0.4263 0.3339 -1.000 -0.1182 0.00820 0.00186 0.0004 0.4177 0.3434 -0.500 -0.0591 0.00816 0.00182 0.0002 0.3991 0.3619 -0.250 -0.0296 0.00817 0.00182 0.0001 0.3888 0.3704 0.000 0.0000 0.00815 0.00181 0.0000 0.3804 0.3804 0.250 0.0296 0.00817 0.00182 -0.0001 0.3704 0.3889 0.500 0.0591 0.00816 0.00182 -0.0002 0.3618 0.3991 1.000 0.1182 0.00820 0.00186 -0.0003 0.3434 0.4177 1.250 0.1478 0.00825 0.00189 -0.0004 0.3339 0.4263 1.500 0.1772 0.00827 0.00192 -0.0005 0.3251 0.4363 1.750 0.2067 0.00832 0.00196 -0.0006 0.3160 0.4456 2.000 0.2361 0.00836 0.00201 -0.0007 0.3070 0.4548 2.250 0.2655 0.00842 0.00206 -0.0007 0.2979 0.4648 2.500 0.2949 0.00849 0.00213 -0.0008 0.2891 0.4736 2.750 0.3242 0.00854 0.00219 -0.0009 0.2802 0.4839 3.000 0.3534 0.00863 0.00227 -0.0009 0.2714 0.4925 3.250 0.3827 0.00870 0.00234 -0.0010 0.2629 0.5028 3.500 0.4118 0.00881 0.00244 -0.0010 0.2541 0.5117 3.750 0.4409 0.00889 0.00252 -0.0011 0.2457 0.5218 4.000 0.4699 0.00901 0.00263 -0.0011 0.2373 0.5310 4.250 0.4989 0.00910 0.00274 -0.0011 0.2294 0.5411 4.500 0.5276 0.00924 0.00286 -0.0011 0.2210 0.5508 4.750 0.5565 0.00935 0.00298 -0.0011 0.2131 0.5605 5.000 0.5850 0.00949 0.00312 -0.0011 0.2052 0.5706 5.250 0.6137 0.00962 0.00325 -0.0011 0.1977 0.5799 5.500 0.6420 0.00978 0.00341 -0.0010 0.1903 0.5907 5.750 0.6704 0.00993 0.00356 -0.0010 0.1830 0.5998 6.000 0.6985 0.01010 0.00373 -0.0009 0.1760 0.6108 6.250 0.7266 0.01027 0.00390 -0.0008 0.1690 0.6201 6.500 0.7544 0.01045 0.00409 -0.0007 0.1624 0.6309 6.750 0.7823 0.01064 0.00427 -0.0006 0.1560 0.6408 7.000 0.8097 0.01084 0.00448 -0.0005 0.1499 0.6515 7.250 0.8373 0.01103 0.00468 -0.0003 0.1439 0.6620 7.500 0.8643 0.01126 0.00491 -0.0001 0.1382 0.6730 7.750 0.8915 0.01146 0.00513 0.0001 0.1328 0.6837 8.000 0.9179 0.01171 0.00539 0.0003 0.1272 0.6946 8.250 0.9447 0.01193 0.00563 0.0006 0.1223 0.7062 8.500 0.9706 0.01220 0.00590 0.0009 0.1172 0.7173 8.750 0.9969 0.01243 0.00616 0.0012 0.1129 0.7292 9.500 1.0724 0.01328 0.00707 0.0025 0.1001 0.7665 9.750 1.0971 0.01355 0.00738 0.0030 0.0968 0.7792 10.000 1.1209 0.01386 0.00771 0.0036 0.0928 0.7937 10.250 1.1441 0.01418 0.00807 0.0043 0.0896 0.8085 10.500 1.1670 0.01448 0.00842 0.0051 0.0865 0.8241 10.750 1.1882 0.01485 0.00882 0.0060 0.0832 0.8414 11.000 1.2092 0.01515 0.00919 0.0071 0.0807 0.8617 11.250 1.2281 0.01547 0.00959 0.0085 0.0781 0.8860 11.500 1.2425 0.01583 0.01004 0.0106 0.0755 0.9245 11.750 1.2689 0.01618 0.01047 0.0104 0.0731 1.0000 12.000 1.2858 0.01666 0.01095 0.0118 0.0708 1.0000 12.250 1.2969 0.01722 0.01151 0.0140 0.0688 1.0000 12.500 1.3090 0.01776 0.01208 0.0159 0.0673 1.0000 12.750 1.3198 0.01845 0.01278 0.0177 0.0653 1.0000 13.000 1.3299 0.01926 0.01360 0.0193 0.0637 1.0000 13.250 1.3400 0.02016 0.01452 0.0206 0.0621 1.0000 13.500 1.3511 0.02107 0.01547 0.0217 0.0608 1.0000 13.750 1.3609 0.02214 0.01656 0.0227 0.0592 1.0000 14.000 1.3688 0.02341 0.01785 0.0237 0.0577 1.0000 14.250 1.3770 0.02473 0.01921 0.0244 0.0564 1.0000 14.500 1.3859 0.02607 0.02059 0.0250 0.0553 1.0000 14.750 1.3930 0.02761 0.02216 0.0255 0.0540 1.0000 15.000 1.3980 0.02939 0.02397 0.0258 0.0527 1.0000 15.250 1.4019 0.03134 0.02596 0.0261 0.0516 1.0000 15.500 1.4074 0.03320 0.02788 0.0262 0.0508 1.0000 15.750 1.4115 0.03526 0.02999 0.0261 0.0498 1.0000 16.000 1.4139 0.03753 0.03231 0.0260 0.0488 1.0000 16.250 1.4143 0.04007 0.03490 0.0257 0.0478 1.0000 16.500 1.4119 0.04296 0.03784 0.0251 0.0468 1.0000 16.750 1.4110 0.04578 0.04072 0.0245 0.0462 1.0000 17.000 1.4103 0.04870 0.04371 0.0237 0.0455 1.0000 17.250 1.4081 0.05188 0.04696 0.0228 0.0448 1.0000 17.500 1.4044 0.05532 0.05048 0.0216 0.0440 1.0000 17.750 1.3998 0.05899 0.05421 0.0203 0.0434 1.0000 18.000 1.3929 0.06301 0.05830 0.0187 0.0427 1.0000 18.250 1.3846 0.06734 0.06271 0.0169 0.0421 1.0000 18.500 1.3793 0.07138 0.06681 0.0151 0.0415 1.0000 18.750 1.3733 0.07558 0.07110 0.0132 0.0409 1.0000 19.000 1.3652 0.08019 0.07580 0.0110 0.0401 1.0000 19.250 1.3560 0.08504 0.08072 0.0087 0.0396 1.0000