XFOIL Version 6.96 Calculated polar for: MH 95 15.86% 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 ------ -------- --------- --------- -------- -------- -------- -17.750 -0.7652 0.10892 0.10545 -0.0540 1.0000 0.0114 -17.500 -0.7982 0.09860 0.09493 -0.0596 1.0000 0.0114 -17.250 -0.8233 0.09033 0.08648 -0.0639 1.0000 0.0113 -17.000 -0.8453 0.08300 0.07898 -0.0677 1.0000 0.0113 -16.750 -0.8622 0.07686 0.07270 -0.0706 1.0000 0.0114 -16.500 -0.8786 0.07115 0.06683 -0.0731 1.0000 0.0114 -16.250 -0.8911 0.06630 0.06185 -0.0749 1.0000 0.0114 -16.000 -0.9010 0.06211 0.05753 -0.0762 1.0000 0.0114 -15.750 -0.9104 0.05825 0.05354 -0.0771 1.0000 0.0115 -15.500 -0.9177 0.05490 0.05008 -0.0775 1.0000 0.0115 -15.250 -0.9250 0.05178 0.04684 -0.0774 1.0000 0.0115 -15.000 -0.9312 0.04901 0.04396 -0.0769 1.0000 0.0116 -14.750 -0.9364 0.04654 0.04138 -0.0761 1.0000 0.0116 -14.500 -0.9418 0.04421 0.03894 -0.0749 1.0000 0.0118 -14.250 -0.9456 0.04219 0.03682 -0.0734 1.0000 0.0118 -14.000 -0.9493 0.04029 0.03482 -0.0716 1.0000 0.0118 -13.750 -0.9523 0.03859 0.03303 -0.0695 1.0000 0.0120 -13.500 -0.9545 0.03707 0.03142 -0.0673 1.0000 0.0120 -13.250 -0.9552 0.03554 0.02981 -0.0651 0.9999 0.0121 -13.000 -0.9412 0.03394 0.02810 -0.0657 0.9987 0.0122 -12.750 -0.9269 0.03238 0.02643 -0.0660 0.9971 0.0123 -12.500 -0.9113 0.03105 0.02501 -0.0663 0.9955 0.0124 -12.250 -0.8934 0.02988 0.02372 -0.0668 0.9939 0.0126 -12.000 -0.8759 0.02878 0.02253 -0.0669 0.9922 0.0127 -11.750 -0.8638 0.02731 0.02103 -0.0663 0.9898 0.0129 -11.500 -0.8467 0.02621 0.01988 -0.0663 0.9875 0.0131 -11.250 -0.8275 0.02520 0.01881 -0.0665 0.9855 0.0132 -11.000 -0.8066 0.02424 0.01782 -0.0669 0.9838 0.0134 -10.750 -0.7838 0.02335 0.01689 -0.0675 0.9825 0.0136 -10.500 -0.7671 0.02254 0.01603 -0.0667 0.9794 0.0138 -10.250 -0.7490 0.02179 0.01524 -0.0661 0.9760 0.0140 -10.000 -0.7276 0.02101 0.01442 -0.0661 0.9735 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0.9036 0.0498 -5.000 -0.2614 0.01148 0.00473 -0.0574 0.8963 0.0707 -4.750 -0.2350 0.01097 0.00436 -0.0574 0.8914 0.1048 -4.500 -0.2186 0.01054 0.00411 -0.0552 0.8822 0.1454 -4.250 -0.1941 0.01005 0.00381 -0.0548 0.8754 0.1923 -4.000 -0.1737 0.00970 0.00359 -0.0535 0.8661 0.2305 -3.750 -0.1494 0.00924 0.00332 -0.0530 0.8577 0.2835 -3.500 -0.1316 0.00874 0.00309 -0.0512 0.8466 0.3520 -3.250 -0.1116 0.00822 0.00285 -0.0499 0.8359 0.4285 -3.000 -0.0923 0.00770 0.00263 -0.0483 0.8239 0.5107 -2.750 -0.0715 0.00737 0.00253 -0.0469 0.8107 0.5756 -2.500 -0.0462 0.00726 0.00245 -0.0462 0.7971 0.6084 -2.250 -0.0202 0.00721 0.00239 -0.0457 0.7822 0.6295 -2.000 0.0058 0.00720 0.00234 -0.0451 0.7655 0.6464 -1.750 0.0314 0.00723 0.00230 -0.0445 0.7479 0.6607 -1.500 0.0566 0.00726 0.00228 -0.0438 0.7297 0.6729 -1.250 0.0816 0.00732 0.00226 -0.0430 0.7109 0.6832 -1.000 0.1062 0.00739 0.00226 -0.0422 0.6917 0.6937 -0.750 0.1308 0.00747 0.00226 -0.0414 0.6738 0.7026 -0.500 0.1552 0.00756 0.00228 -0.0405 0.6549 0.7119 -0.250 0.1795 0.00765 0.00230 -0.0397 0.6368 0.7198 0.000 0.2035 0.00775 0.00233 -0.0388 0.6176 0.7271 0.250 0.2276 0.00787 0.00235 -0.0380 0.5985 0.7339 0.500 0.2511 0.00798 0.00240 -0.0369 0.5782 0.7394 0.750 0.2746 0.00811 0.00245 -0.0360 0.5583 0.7455 1.250 0.3209 0.00840 0.00258 -0.0339 0.5169 0.7573 1.500 0.3440 0.00856 0.00266 -0.0329 0.4958 0.7635 1.750 0.3670 0.00873 0.00272 -0.0319 0.4734 0.7692 2.000 0.3893 0.00890 0.00282 -0.0308 0.4512 0.7738 2.250 0.4109 0.00911 0.00293 -0.0295 0.4258 0.7787 2.500 0.4320 0.00936 0.00304 -0.0282 0.3964 0.7838 3.000 0.4755 0.00982 0.00328 -0.0259 0.3467 0.7920 3.250 0.4980 0.01001 0.00341 -0.0249 0.3294 0.7959 3.500 0.5202 0.01021 0.00353 -0.0238 0.3124 0.8000 3.750 0.5423 0.01040 0.00365 -0.0227 0.2964 0.8042 4.000 0.5642 0.01060 0.00378 -0.0216 0.2818 0.8078 4.250 0.5857 0.01079 0.00393 -0.0204 0.2689 0.8113 4.500 0.6072 0.01098 0.00409 -0.0193 0.2564 0.8153 4.750 0.6292 0.01118 0.00425 -0.0182 0.2445 0.8193 5.000 0.6509 0.01141 0.00442 -0.0171 0.2322 0.8233 5.250 0.6722 0.01165 0.00462 -0.0160 0.2206 0.8270 5.500 0.6936 0.01186 0.00482 -0.0148 0.2103 0.8309 5.750 0.7148 0.01210 0.00503 -0.0137 0.2008 0.8350 6.000 0.7357 0.01237 0.00525 -0.0125 0.1901 0.8391 6.250 0.7571 0.01262 0.00548 -0.0115 0.1793 0.8434 6.500 0.7771 0.01289 0.00573 -0.0101 0.1696 0.8473 6.750 0.7965 0.01319 0.00599 -0.0087 0.1595 0.8518 7.000 0.8170 0.01345 0.00625 -0.0075 0.1509 0.8564 7.250 0.8367 0.01378 0.00654 -0.0063 0.1425 0.8610 7.500 0.8559 0.01407 0.00683 -0.0048 0.1348 0.8653 7.750 0.8743 0.01439 0.00714 -0.0033 0.1281 0.8705 8.000 0.8931 0.01472 0.00747 -0.0019 0.1215 0.8760 8.250 0.9115 0.01507 0.00781 -0.0005 0.1165 0.8810 8.500 0.9296 0.01537 0.00814 0.0010 0.1119 0.8862 8.750 0.9469 0.01574 0.00852 0.0026 0.1079 0.8925 9.000 0.9640 0.01611 0.00890 0.0042 0.1045 0.8988 9.250 0.9813 0.01642 0.00927 0.0058 0.1019 0.9059 9.750 1.0132 0.01720 0.01011 0.0093 0.0964 0.9217 10.000 1.0280 0.01764 0.01058 0.0111 0.0937 0.9317 10.500 1.0678 0.01845 0.01153 0.0127 0.0900 0.9581 10.750 1.0957 0.01900 0.01212 0.0115 0.0878 0.9741 11.000 1.1160 0.01957 0.01270 0.0118 0.0859 1.0000 11.250 1.1311 0.02020 0.01334 0.0131 0.0843 1.0000 11.500 1.1461 0.02084 0.01401 0.0144 0.0829 1.0000 11.750 1.1625 0.02141 0.01463 0.0154 0.0818 1.0000 12.000 1.1778 0.02204 0.01531 0.0166 0.0804 1.0000 12.250 1.1923 0.02273 0.01604 0.0178 0.0792 1.0000 12.500 1.2060 0.02348 0.01682 0.0190 0.0779 1.0000 12.750 1.2188 0.02429 0.01767 0.0202 0.0769 1.0000 13.000 1.2301 0.02521 0.01862 0.0215 0.0755 1.0000 13.250 1.2399 0.02626 0.01970 0.0229 0.0744 1.0000 13.500 1.2509 0.02725 0.02075 0.0241 0.0735 1.0000 13.750 1.2635 0.02817 0.02173 0.0250 0.0726 1.0000 14.000 1.2749 0.02919 0.02283 0.0260 0.0718 1.0000 14.250 1.2857 0.03028 0.02399 0.0269 0.0708 1.0000 14.500 1.2958 0.03146 0.02523 0.0278 0.0699 1.0000 14.750 1.3049 0.03275 0.02656 0.0286 0.0688 1.0000 15.000 1.3131 0.03415 0.02801 0.0294 0.0678 1.0000 15.250 1.3197 0.03573 0.02964 0.0301 0.0668 1.0000 15.500 1.3245 0.03752 0.03148 0.0308 0.0659 1.0000 15.750 1.3295 0.03934 0.03337 0.0313 0.0651 1.0000 16.000 1.3382 0.04090 0.03503 0.0316 0.0642 1.0000 16.250 1.3446 0.04272 0.03693 0.0318 0.0636 1.0000 16.500 1.3509 0.04460 0.03889 0.0319 0.0627 1.0000 16.750 1.3560 0.04665 0.04103 0.0319 0.0618 1.0000 17.000 1.3599 0.04888 0.04334 0.0318 0.0609 1.0000 17.250 1.3626 0.05130 0.04583 0.0316 0.0601 1.0000 17.500 1.3642 0.05393 0.04852 0.0312 0.0594 1.0000 17.750 1.3637 0.05685 0.05152 0.0306 0.0586 1.0000 18.000 1.3612 0.06007 0.05480 0.0298 0.0580 1.0000 18.250 1.3612 0.06309 0.05792 0.0290 0.0573 1.0000 18.500 1.3620 0.06608 0.06102 0.0281 0.0567 1.0000 18.750 1.3622 0.06923 0.06428 0.0270 0.0560 1.0000 19.000 1.3608 0.07263 0.06779 0.0258 0.0551 1.0000 19.250 1.3580 0.07627 0.07153 0.0244 0.0545 1.0000