XFOIL Version 6.96 Calculated polar for: NACA 65(2)-415 a=0.5 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 ------ -------- --------- --------- -------- -------- -------- -15.500 -0.4218 0.15382 0.15193 -0.0315 0.9125 0.0143 -15.250 -0.4192 0.14930 0.14735 -0.0333 0.8980 0.0144 -14.750 -0.8679 0.04371 0.04080 -0.0870 0.9150 0.0120 -14.500 -0.8257 0.04632 0.04356 -0.0859 0.8993 0.0123 -14.250 -0.8480 0.04181 0.03880 -0.0867 0.8818 0.0123 -14.000 -0.8505 0.03965 0.03650 -0.0865 0.8687 0.0125 -13.750 -0.8558 0.03733 0.03402 -0.0861 0.8570 0.0126 -13.500 -0.8627 0.03496 0.03147 -0.0851 0.8468 0.0126 -13.250 -0.8694 0.03280 0.02912 -0.0836 0.8372 0.0128 -13.000 -0.8715 0.03107 0.02723 -0.0818 0.8284 0.0130 -12.750 -0.8688 0.02984 0.02586 -0.0800 0.8207 0.0132 -12.500 -0.8681 0.02842 0.02429 -0.0777 0.8128 0.0134 -12.250 -0.8661 0.02718 0.02286 -0.0751 0.8056 0.0135 -12.000 -0.8624 0.02602 0.02155 -0.0724 0.7987 0.0138 -11.750 -0.8534 0.02509 0.02046 -0.0702 0.7924 0.0140 -11.500 -0.8382 0.02443 0.01966 -0.0689 0.7870 0.0142 -11.250 -0.8275 0.02292 0.01794 -0.0672 0.7814 0.0145 -11.000 -0.8149 0.02151 0.01638 -0.0657 0.7762 0.0149 -10.750 -0.7961 0.02081 0.01560 -0.0648 0.7714 0.0152 -10.500 -0.7750 0.02041 0.01517 -0.0642 0.7665 0.0155 -10.250 -0.7533 0.02007 0.01476 -0.0636 0.7617 0.0159 -10.000 -0.7320 0.01951 0.01410 -0.0629 0.7571 0.0163 -9.750 -0.7099 0.01891 0.01342 -0.0623 0.7526 0.0167 -9.500 -0.6868 0.01852 0.01293 -0.0619 0.7480 0.0173 -9.250 -0.6633 0.01816 0.01245 -0.0614 0.7435 0.0176 -9.000 -0.6429 0.01694 0.01110 -0.0607 0.7397 0.0182 -8.750 -0.6204 0.01623 0.01036 -0.0602 0.7357 0.0187 -8.500 -0.5961 0.01584 0.00993 -0.0599 0.7317 0.0191 -8.250 -0.5715 0.01551 0.00954 -0.0596 0.7277 0.0197 -8.000 -0.5468 0.01509 0.00906 -0.0593 0.7242 0.0202 -7.750 -0.5213 0.01475 0.00868 -0.0591 0.7206 0.0209 -7.500 -0.4954 0.01450 0.00836 -0.0590 0.7169 0.0215 -7.250 -0.4694 0.01427 0.00805 -0.0588 0.7133 0.0218 -7.000 -0.4487 0.01319 0.00691 -0.0580 0.7097 0.0228 -6.750 -0.4233 0.01281 0.00653 -0.0578 0.7065 0.0234 -6.500 -0.3973 0.01250 0.00620 -0.0577 0.7031 0.0241 -6.250 -0.3711 0.01224 0.00591 -0.0576 0.6999 0.0250 -6.000 -0.3449 0.01199 0.00560 -0.0575 0.6967 0.0258 -5.750 -0.3183 0.01176 0.00532 -0.0574 0.6938 0.0263 -5.500 -0.2941 0.01119 0.00472 -0.0570 0.6910 0.0273 -5.250 -0.2685 0.01081 0.00432 -0.0568 0.6882 0.0284 -5.000 -0.2417 0.01057 0.00407 -0.0568 0.6852 0.0295 -4.750 -0.2147 0.01038 0.00384 -0.0568 0.6823 0.0307 -4.500 -0.1876 0.01022 0.00363 -0.0568 0.6791 0.0317 -4.250 -0.1608 0.00993 0.00332 -0.0568 0.6769 0.0329 -4.000 -0.1339 0.00965 0.00303 -0.0567 0.6744 0.0351 -3.750 -0.1063 0.00947 0.00285 -0.0568 0.6719 0.0372 -3.500 -0.0784 0.00934 0.00269 -0.0570 0.6694 0.0390 -3.250 -0.0513 0.00912 0.00246 -0.0570 0.6670 0.0440 -3.000 -0.0238 0.00897 0.00231 -0.0571 0.6641 0.0518 -2.750 0.0026 0.00861 0.00214 -0.0571 0.6621 0.0969 -2.500 0.0264 0.00788 0.00191 -0.0569 0.6598 0.2335 -2.250 0.0480 0.00690 0.00167 -0.0564 0.6576 0.4401 -2.000 0.0738 0.00652 0.00160 -0.0563 0.6555 0.5389 -1.750 0.1015 0.00639 0.00157 -0.0564 0.6533 0.5805 -1.500 0.1296 0.00633 0.00156 -0.0566 0.6511 0.6088 -1.250 0.1579 0.00633 0.00157 -0.0568 0.6484 0.6325 -1.000 0.1862 0.00626 0.00158 -0.0570 0.6467 0.6582 -0.750 0.2143 0.00621 0.00162 -0.0571 0.6448 0.6879 -0.500 0.2426 0.00618 0.00166 -0.0572 0.6429 0.7106 -0.250 0.2712 0.00618 0.00168 -0.0575 0.6408 0.7249 0.000 0.3003 0.00620 0.00168 -0.0578 0.6387 0.7334 0.250 0.3290 0.00620 0.00170 -0.0581 0.6367 0.7406 0.500 0.3580 0.00625 0.00172 -0.0584 0.6346 0.7481 0.750 0.3868 0.00629 0.00177 -0.0588 0.6325 0.7550 1.000 0.4158 0.00629 0.00181 -0.0591 0.6308 0.7626 1.250 0.4447 0.00629 0.00184 -0.0595 0.6289 0.7700 1.500 0.4735 0.00630 0.00189 -0.0598 0.6270 0.7777 1.750 0.5024 0.00633 0.00193 -0.0601 0.6250 0.7851 2.000 0.5311 0.00634 0.00197 -0.0604 0.6230 0.7927 2.250 0.5599 0.00639 0.00202 -0.0607 0.6210 0.8007 2.500 0.5883 0.00645 0.00211 -0.0610 0.6187 0.8085 3.000 0.6453 0.00649 0.00225 -0.0615 0.6139 0.8241 3.250 0.6739 0.00650 0.00229 -0.0618 0.6104 0.8325 3.500 0.7017 0.00649 0.00233 -0.0619 0.6062 0.8405 4.000 0.7575 0.00654 0.00246 -0.0622 0.5975 0.8570 4.250 0.7855 0.00655 0.00251 -0.0623 0.5926 0.8656 4.500 0.8119 0.00654 0.00253 -0.0621 0.5821 0.8742 4.750 0.8383 0.00655 0.00254 -0.0620 0.5668 0.8831 5.000 0.8643 0.00661 0.00262 -0.0617 0.5548 0.8921 5.250 0.8904 0.00668 0.00271 -0.0615 0.5431 0.9010 5.500 0.9156 0.00679 0.00283 -0.0612 0.5277 0.9109 5.750 0.9382 0.00698 0.00298 -0.0603 0.4994 0.9209 6.000 0.9533 0.00755 0.00331 -0.0582 0.4404 0.9338 6.250 0.9596 0.00850 0.00391 -0.0547 0.3613 0.9524 6.500 0.9724 0.00970 0.00471 -0.0531 0.2738 0.9755 6.750 0.9903 0.01102 0.00560 -0.0530 0.1924 1.0000 7.000 0.9892 0.01187 0.00622 -0.0484 0.1483 1.0000 7.250 0.9856 0.01285 0.00699 -0.0437 0.1096 1.0000 7.500 0.9885 0.01381 0.00780 -0.0404 0.0803 1.0000 7.750 0.9920 0.01486 0.00871 -0.0374 0.0541 1.0000 8.000 1.0001 0.01579 0.00955 -0.0352 0.0395 1.0000 8.250 1.0109 0.01663 0.01035 -0.0334 0.0318 1.0000 8.500 1.0223 0.01749 0.01119 -0.0317 0.0273 1.0000 8.750 1.0359 0.01825 0.01196 -0.0304 0.0251 1.0000 9.000 1.0463 0.01923 0.01295 -0.0287 0.0228 1.0000 9.250 1.0610 0.01997 0.01372 -0.0276 0.0217 1.0000 9.500 1.0746 0.02079 0.01456 -0.0265 0.0208 1.0000 9.750 1.0873 0.02170 0.01548 -0.0252 0.0197 1.0000 10.000 1.0949 0.02295 0.01677 -0.0236 0.0186 1.0000 10.250 1.1079 0.02388 0.01774 -0.0225 0.0181 1.0000 10.500 1.1209 0.02483 0.01873 -0.0215 0.0175 1.0000 10.750 1.1333 0.02582 0.01975 -0.0204 0.0170 1.0000 11.000 1.1452 0.02686 0.02083 -0.0194 0.0164 1.0000 11.250 1.1564 0.02798 0.02198 -0.0184 0.0161 1.0000 11.500 1.1654 0.02927 0.02330 -0.0173 0.0155 1.0000 11.750 1.1731 0.03069 0.02476 -0.0161 0.0152 1.0000 12.000 1.1757 0.03258 0.02672 -0.0146 0.0147 1.0000 12.250 1.1859 0.03390 0.02809 -0.0137 0.0146 1.0000 12.500 1.1978 0.03510 0.02934 -0.0130 0.0143 1.0000 12.750 1.2064 0.03659 0.03089 -0.0122 0.0142 1.0000 13.000 1.2172 0.03795 0.03230 -0.0115 0.0139 1.0000 13.250 1.2248 0.03958 0.03399 -0.0107 0.0136 1.0000 13.500 1.2341 0.04110 0.03556 -0.0101 0.0135 1.0000 13.750 1.2432 0.04268 0.03718 -0.0095 0.0132 1.0000 14.000 1.2513 0.04437 0.03892 -0.0089 0.0129 1.0000 14.250 1.2605 0.04598 0.04059 -0.0085 0.0127 1.0000 14.500 1.2663 0.04794 0.04259 -0.0079 0.0126 1.0000 14.750 1.2730 0.04983 0.04453 -0.0075 0.0123 1.0000 15.000 1.2776 0.05197 0.04672 -0.0070 0.0121 1.0000 15.250 1.2779 0.05453 0.04936 -0.0063 0.0119 1.0000 15.500 1.2818 0.05678 0.05169 -0.0058 0.0117 1.0000 15.750 1.2890 0.05883 0.05382 -0.0057 0.0115 1.0000 16.000 1.2947 0.06102 0.05609 -0.0055 0.0115 1.0000 16.250 1.3002 0.06330 0.05845 -0.0054 0.0115 1.0000 16.500 1.3061 0.06561 0.06086 -0.0056 0.0113 1.0000 16.750 1.3102 0.06813 0.06346 -0.0057 0.0112 1.0000 17.000 1.3140 0.07072 0.06614 -0.0059 0.0111 1.0000 17.250 1.3167 0.07352 0.06904 -0.0062 0.0110 1.0000 17.500 1.3189 0.07646 0.07207 -0.0066 0.0108 1.0000 17.750 1.3207 0.07952 0.07522 -0.0073 0.0107 1.0000 18.000 1.3200 0.08292 0.07873 -0.0078 0.0106 1.0000 18.250 1.3196 0.08637 0.08229 -0.0086 0.0105 1.0000 18.500 1.3186 0.09000 0.08603 -0.0097 0.0104 1.0000 18.750 1.3163 0.09395 0.09008 -0.0110 0.0103 1.0000 19.000 1.3128 0.09811 0.09436 -0.0124 0.0102 1.0000 19.250 1.3094 0.10235 0.09871 -0.0141 0.0101 1.0000