XFOIL Version 6.96 Calculated polar for: MB253515 15.0% smoothed 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 ------ -------- --------- --------- -------- -------- -------- -15.750 -0.8631 0.06565 0.06331 -0.0636 1.0000 0.0090 -15.500 -0.8847 0.05850 0.05599 -0.0681 1.0000 0.0089 -15.250 -0.9052 0.05215 0.04946 -0.0718 1.0000 0.0089 -15.000 -0.9168 0.04756 0.04472 -0.0740 1.0000 0.0089 -14.750 -0.9421 0.04184 0.03878 -0.0759 1.0000 0.0090 -14.500 -0.9528 0.03826 0.03505 -0.0764 1.0000 0.0091 -14.250 -0.9540 0.03596 0.03265 -0.0763 1.0000 0.0093 -14.000 -0.9541 0.03393 0.03053 -0.0757 1.0000 0.0094 -13.750 -0.9506 0.03239 0.02892 -0.0748 1.0000 0.0095 -13.500 -0.9511 0.03060 0.02703 -0.0734 1.0000 0.0096 -13.250 -0.9454 0.02949 0.02585 -0.0719 1.0000 0.0098 -13.000 -0.9379 0.02867 0.02499 -0.0703 1.0000 0.0100 -12.750 -0.9317 0.02783 0.02410 -0.0682 1.0000 0.0102 -12.500 -0.9339 0.02641 0.02255 -0.0650 1.0000 0.0103 -12.250 -0.9310 0.02567 0.02173 -0.0618 1.0000 0.0106 -12.000 -0.9340 0.02482 0.02078 -0.0574 1.0000 0.0107 -11.750 -0.9118 0.02378 0.01962 -0.0578 0.9973 0.0111 -11.500 -0.8877 0.02272 0.01843 -0.0585 0.9875 0.0113 -11.250 -0.8651 0.02116 0.01668 -0.0591 0.9770 0.0117 -11.000 -0.8327 0.02006 0.01552 -0.0614 0.9691 0.0123 -10.750 -0.7912 0.01977 0.01523 -0.0650 0.9605 0.0128 -10.500 -0.7475 0.01944 0.01485 -0.0691 0.9502 0.0133 -10.250 -0.7070 0.01876 0.01403 -0.0726 0.9341 0.0141 -10.000 -0.6776 0.01813 0.01323 -0.0737 0.9121 0.0145 -9.750 -0.6570 0.01781 0.01276 -0.0726 0.8915 0.0148 -9.500 -0.6436 0.01672 0.01152 -0.0706 0.8741 0.0156 -9.250 -0.6253 0.01639 0.01112 -0.0690 0.8595 0.0160 -9.000 -0.6050 0.01631 0.01096 -0.0678 0.8466 0.0165 -8.750 -0.5853 0.01599 0.01055 -0.0665 0.8350 0.0170 -8.500 -0.5639 0.01583 0.01033 -0.0655 0.8246 0.0177 -8.250 -0.5423 0.01567 0.01006 -0.0644 0.8149 0.0184 -8.000 -0.5206 0.01540 0.00970 -0.0634 0.8055 0.0188 -7.750 -0.5033 0.01434 0.00856 -0.0618 0.7968 0.0197 -7.500 -0.4823 0.01401 0.00817 -0.0608 0.7887 0.0204 -7.250 -0.4594 0.01377 0.00791 -0.0600 0.7809 0.0211 -7.000 -0.4368 0.01353 0.00760 -0.0591 0.7732 0.0219 -6.750 -0.4134 0.01327 0.00731 -0.0584 0.7660 0.0228 -6.500 -0.3901 0.01303 0.00700 -0.0577 0.7591 0.0235 -6.250 -0.3649 0.01295 0.00687 -0.0572 0.7526 0.0240 -6.000 -0.3494 0.01196 0.00579 -0.0552 0.7457 0.0252 -5.750 -0.3279 0.01157 0.00536 -0.0541 0.7396 0.0262 -5.500 -0.3043 0.01132 0.00509 -0.0534 0.7334 0.0273 -5.250 -0.2813 0.01106 0.00477 -0.0526 0.7274 0.0281 -5.000 -0.2574 0.01078 0.00447 -0.0519 0.7216 0.0290 -4.750 -0.2332 0.01057 0.00421 -0.0513 0.7157 0.0298 -4.500 -0.2085 0.01042 0.00400 -0.0507 0.7104 0.0305 -4.250 -0.1855 0.01006 0.00359 -0.0499 0.7047 0.0314 -4.000 -0.1625 0.00975 0.00321 -0.0490 0.6992 0.0329 -3.750 -0.1378 0.00954 0.00296 -0.0484 0.6941 0.0343 -3.500 -0.1125 0.00937 0.00277 -0.0480 0.6883 0.0358 -3.000 -0.0616 0.00911 0.00242 -0.0471 0.6744 0.0387 -2.750 -0.0367 0.00898 0.00224 -0.0465 0.6671 0.0421 -2.500 -0.0113 0.00880 0.00209 -0.0461 0.6611 0.0522 -2.250 -0.0001 0.00763 0.00173 -0.0433 0.6556 0.2760 -2.000 0.0175 0.00703 0.00157 -0.0416 0.6506 0.4053 -1.750 0.0384 0.00662 0.00148 -0.0404 0.6453 0.4967 -1.500 0.0603 0.00636 0.00142 -0.0393 0.6401 0.5670 -1.250 0.0832 0.00620 0.00140 -0.0383 0.6353 0.6191 -1.000 0.1077 0.00607 0.00139 -0.0377 0.6302 0.6590 -0.750 0.1329 0.00602 0.00138 -0.0371 0.6248 0.6835 -0.500 0.1585 0.00599 0.00138 -0.0367 0.6196 0.7070 -0.250 0.1841 0.00594 0.00138 -0.0362 0.6141 0.7290 0.000 0.2097 0.00593 0.00139 -0.0357 0.6087 0.7486 0.250 0.2358 0.00592 0.00141 -0.0354 0.6035 0.7637 0.500 0.2620 0.00591 0.00142 -0.0351 0.5974 0.7798 0.750 0.2875 0.00592 0.00144 -0.0346 0.5917 0.7950 1.000 0.3144 0.00592 0.00147 -0.0344 0.5862 0.8060 1.250 0.3407 0.00594 0.00149 -0.0342 0.5799 0.8170 1.500 0.3669 0.00596 0.00152 -0.0339 0.5737 0.8282 1.750 0.3933 0.00597 0.00155 -0.0336 0.5669 0.8389 2.000 0.4191 0.00601 0.00159 -0.0333 0.5605 0.8503 2.250 0.4455 0.00603 0.00163 -0.0330 0.5535 0.8616 2.500 0.4712 0.00608 0.00169 -0.0326 0.5459 0.8730 2.750 0.4977 0.00610 0.00175 -0.0324 0.5377 0.8847 3.000 0.5235 0.00616 0.00181 -0.0320 0.5299 0.8973 3.250 0.5499 0.00621 0.00189 -0.0318 0.5208 0.9099 3.500 0.5772 0.00628 0.00197 -0.0318 0.5110 0.9215 3.750 0.6060 0.00639 0.00207 -0.0321 0.5001 0.9317 4.000 0.6352 0.00651 0.00219 -0.0326 0.4886 0.9418 4.250 0.6677 0.00665 0.00232 -0.0338 0.4754 0.9499 4.500 0.6995 0.00683 0.00246 -0.0349 0.4602 0.9573 4.750 0.7341 0.00704 0.00263 -0.0367 0.4445 0.9621 5.000 0.7628 0.00727 0.00280 -0.0371 0.4281 0.9696 5.250 0.7986 0.00755 0.00300 -0.0392 0.4054 0.9718 5.500 0.8312 0.00792 0.00325 -0.0407 0.3784 0.9749 5.750 0.8621 0.00824 0.00349 -0.0418 0.3587 0.9790 6.000 0.8914 0.00856 0.00374 -0.0426 0.3409 0.9835 6.500 0.9587 0.00917 0.00422 -0.0460 0.3077 0.9882 6.750 0.9904 0.00949 0.00448 -0.0474 0.2885 0.9915 7.000 1.0203 0.00994 0.00481 -0.0485 0.2603 0.9946 7.250 1.0473 0.01093 0.00541 -0.0495 0.1944 0.9982 7.500 1.0309 0.01274 0.00658 -0.0424 0.0828 1.0000 7.750 1.0149 0.01357 0.00721 -0.0342 0.0429 1.0000 8.000 1.0105 0.01408 0.00765 -0.0283 0.0288 1.0000 8.250 1.0150 0.01457 0.00811 -0.0242 0.0224 1.0000 8.500 1.0253 0.01498 0.00854 -0.0214 0.0201 1.0000 8.750 1.0342 0.01554 0.00910 -0.0185 0.0176 1.0000 9.000 1.0444 0.01612 0.00973 -0.0159 0.0163 1.0000 9.250 1.0573 0.01664 0.01028 -0.0139 0.0153 1.0000 9.500 1.0692 0.01726 0.01093 -0.0119 0.0145 1.0000 9.750 1.0779 0.01810 0.01180 -0.0097 0.0134 1.0000 10.000 1.0855 0.01907 0.01284 -0.0074 0.0127 1.0000 10.250 1.0970 0.01990 0.01372 -0.0058 0.0125 1.0000 10.500 1.1066 0.02088 0.01477 -0.0041 0.0121 1.0000 10.750 1.1188 0.02175 0.01568 -0.0029 0.0116 1.0000 11.000 1.1268 0.02296 0.01694 -0.0013 0.0113 1.0000 11.250 1.1361 0.02412 0.01814 -0.0001 0.0108 1.0000 11.500 1.1427 0.02553 0.01959 0.0013 0.0102 1.0000 11.750 1.1415 0.02759 0.02175 0.0030 0.0099 1.0000 12.000 1.1416 0.02966 0.02391 0.0044 0.0096 1.0000 12.250 1.1486 0.03123 0.02554 0.0053 0.0095 1.0000 12.500 1.1570 0.03270 0.02707 0.0060 0.0093 1.0000 12.750 1.1612 0.03460 0.02905 0.0069 0.0091 1.0000 13.000 1.1637 0.03669 0.03120 0.0076 0.0090 1.0000 13.250 1.1676 0.03871 0.03330 0.0083 0.0087 1.0000 13.500 1.1711 0.04085 0.03549 0.0088 0.0085 1.0000 13.750 1.1732 0.04316 0.03788 0.0092 0.0084 1.0000 14.000 1.1771 0.04536 0.04014 0.0095 0.0081 1.0000 14.250 1.1758 0.04812 0.04299 0.0098 0.0082 1.0000 14.500 1.1808 0.05034 0.04524 0.0098 0.0078 1.0000 14.750 1.1791 0.05326 0.04823 0.0099 0.0078 1.0000 15.000 1.1805 0.05592 0.05095 0.0099 0.0076 1.0000 15.250 1.1772 0.05909 0.05420 0.0099 0.0075 1.0000 15.500 1.1701 0.06261 0.05778 0.0101 0.0073 1.0000 15.750 1.1637 0.06576 0.06102 0.0110 0.0072 1.0000 16.000 1.1667 0.06840 0.06374 0.0107 0.0072 1.0000 16.250 1.1694 0.07112 0.06653 0.0104 0.0071 1.0000 16.500 1.1734 0.07401 0.06951 0.0094 0.0070 1.0000 16.750 1.1755 0.07698 0.07257 0.0087 0.0068 1.0000 17.000 1.1765 0.08012 0.07579 0.0079 0.0066 1.0000 17.250 1.1751 0.08311 0.07887 0.0080 0.0067 1.0000 17.500 1.1754 0.08641 0.08226 0.0071 0.0066 1.0000 17.750 1.1759 0.08979 0.08571 0.0060 0.0064 1.0000 18.000 1.1747 0.09326 0.08927 0.0050 0.0063 1.0000 18.250 1.1725 0.09676 0.09286 0.0043 0.0063 1.0000 18.500 1.1702 0.10047 0.09667 0.0032 0.0062 1.0000 18.750 1.1685 0.10445 0.10071 0.0015 0.0059 1.0000 19.000 1.1645 0.10833 0.10470 0.0004 0.0059 1.0000 19.250 1.1618 0.11221 0.10867 -0.0010 0.0059 1.0000