XFOIL Version 6.96 Calculated polar for: NACA 0010-65 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 ------ -------- --------- --------- -------- -------- -------- -17.250 -1.2134 0.06115 0.05851 -0.0552 1.0000 0.0047 -17.000 -1.2490 0.05223 0.04934 -0.0601 1.0000 0.0046 -16.750 -1.2699 0.04700 0.04393 -0.0612 1.0000 0.0047 -16.500 -1.2844 0.04312 0.03989 -0.0609 1.0000 0.0047 -16.250 -1.2943 0.04007 0.03669 -0.0597 1.0000 0.0047 -16.000 -1.3011 0.03754 0.03401 -0.0580 1.0000 0.0048 -15.750 -1.3050 0.03541 0.03175 -0.0559 1.0000 0.0049 -15.500 -1.3069 0.03355 0.02976 -0.0536 1.0000 0.0050 -15.250 -1.3068 0.03194 0.02801 -0.0511 1.0000 0.0050 -15.000 -1.3053 0.03050 0.02645 -0.0484 1.0000 0.0051 -14.750 -1.3027 0.02924 0.02506 -0.0455 1.0000 0.0052 -14.500 -1.2997 0.02810 0.02381 -0.0424 1.0000 0.0053 -14.250 -1.2967 0.02710 0.02270 -0.0390 1.0000 0.0054 -14.000 -1.2941 0.02621 0.02171 -0.0353 1.0000 0.0055 -13.750 -1.2922 0.02545 0.02085 -0.0312 1.0000 0.0056 -13.500 -1.2922 0.02481 0.02012 -0.0265 1.0000 0.0057 -13.250 -1.2936 0.02427 0.01949 -0.0213 1.0000 0.0058 -13.000 -1.2816 0.02323 0.01834 -0.0192 0.9993 0.0061 -12.750 -1.2614 0.02223 0.01725 -0.0187 0.9982 0.0064 -12.500 -1.2400 0.02137 0.01629 -0.0183 0.9971 0.0067 -12.250 -1.2179 0.02060 0.01544 -0.0181 0.9961 0.0071 -12.000 -1.1948 0.01988 0.01463 -0.0179 0.9953 0.0074 -11.750 -1.1706 0.01921 0.01386 -0.0179 0.9946 0.0077 -11.500 -1.1475 0.01861 0.01317 -0.0176 0.9935 0.0080 -11.250 -1.1254 0.01794 0.01243 -0.0171 0.9920 0.0085 -11.000 -1.1022 0.01732 0.01174 -0.0167 0.9907 0.0091 -10.750 -1.0778 0.01676 0.01114 -0.0166 0.9896 0.0098 -10.500 -1.0522 0.01625 0.01057 -0.0167 0.9885 0.0105 -10.250 -1.0259 0.01576 0.01002 -0.0169 0.9876 0.0112 -10.000 -0.9990 0.01530 0.00955 -0.0173 0.9869 0.0126 -9.750 -0.9716 0.01490 0.00914 -0.0177 0.9862 0.0139 -9.500 -0.9437 0.01452 0.00870 -0.0182 0.9857 0.0149 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0.0324 -4.500 -0.4161 0.00939 0.00322 -0.0171 0.9523 0.0332 -4.250 -0.3889 0.00921 0.00302 -0.0171 0.9505 0.0341 -4.000 -0.3615 0.00905 0.00284 -0.0171 0.9488 0.0350 -3.750 -0.3372 0.00892 0.00271 -0.0165 0.9457 0.0358 -3.500 -0.3119 0.00876 0.00257 -0.0160 0.9428 0.0390 -3.250 -0.2860 0.00859 0.00243 -0.0157 0.9401 0.0441 -3.000 -0.2600 0.00837 0.00229 -0.0154 0.9377 0.0587 -2.750 -0.2331 0.00818 0.00216 -0.0153 0.9356 0.0738 -2.500 -0.2071 0.00803 0.00206 -0.0150 0.9331 0.0862 -2.250 -0.1825 0.00786 0.00198 -0.0145 0.9297 0.1034 -2.000 -0.1580 0.00763 0.00188 -0.0139 0.9265 0.1374 -1.750 -0.1328 0.00740 0.00179 -0.0134 0.9236 0.1735 -1.500 -0.1076 0.00712 0.00168 -0.0130 0.9210 0.2245 -1.250 -0.0846 0.00677 0.00159 -0.0122 0.9177 0.2960 -1.000 -0.0664 0.00624 0.00146 -0.0103 0.9108 0.4125 -0.750 -0.0593 0.00514 0.00119 -0.0060 0.9007 0.6464 -0.500 -0.0447 0.00465 0.00108 -0.0030 0.8877 0.7556 -0.250 -0.0237 0.00445 0.00103 -0.0012 0.8690 0.8095 0.000 0.0000 0.00440 0.00101 0.0000 0.8425 0.8429 0.250 0.0238 0.00445 0.00103 0.0012 0.8096 0.8691 0.500 0.0447 0.00465 0.00108 0.0030 0.7548 0.8874 0.750 0.0596 0.00514 0.00119 0.0060 0.6481 0.9006 1.000 0.0663 0.00624 0.00146 0.0103 0.4114 0.9108 1.250 0.0847 0.00677 0.00159 0.0122 0.2959 0.9178 1.500 0.1076 0.00711 0.00168 0.0130 0.2251 0.9210 1.750 0.1329 0.00740 0.00179 0.0134 0.1741 0.9236 2.000 0.1581 0.00763 0.00188 0.0139 0.1378 0.9264 2.250 0.1826 0.00786 0.00198 0.0144 0.1033 0.9297 2.500 0.2072 0.00803 0.00206 0.0150 0.0863 0.9331 2.750 0.2332 0.00818 0.00216 0.0153 0.0741 0.9356 3.000 0.2601 0.00837 0.00229 0.0154 0.0587 0.9377 3.250 0.2861 0.00859 0.00243 0.0157 0.0442 0.9401 3.500 0.3119 0.00876 0.00257 0.0160 0.0390 0.9428 3.750 0.3373 0.00892 0.00271 0.0164 0.0358 0.9457 4.000 0.3616 0.00905 0.00284 0.0171 0.0350 0.9488 4.250 0.3890 0.00921 0.00302 0.0171 0.0341 0.9505 4.500 0.4161 0.00939 0.00322 0.0171 0.0332 0.9523 4.750 0.4427 0.00959 0.00342 0.0173 0.0324 0.9543 5.000 0.4687 0.00979 0.00362 0.0175 0.0314 0.9566 5.250 0.4936 0.01000 0.00384 0.0180 0.0301 0.9592 5.500 0.5161 0.01023 0.00408 0.0190 0.0291 0.9624 5.750 0.5430 0.01054 0.00442 0.0191 0.0281 0.9637 6.000 0.5692 0.01090 0.00482 0.0192 0.0272 0.9652 6.250 0.5966 0.01111 0.00506 0.0191 0.0270 0.9667 6.500 0.6236 0.01133 0.00530 0.0190 0.0266 0.9684 6.750 0.6497 0.01155 0.00553 0.0192 0.0260 0.9704 7.000 0.6737 0.01176 0.00577 0.0198 0.0253 0.9730 7.250 0.6988 0.01199 0.00603 0.0202 0.0245 0.9750 7.500 0.7271 0.01225 0.00632 0.0197 0.0236 0.9759 7.750 0.7556 0.01249 0.00657 0.0193 0.0226 0.9768 8.000 0.7835 0.01279 0.00686 0.0189 0.0215 0.9778 8.250 0.8101 0.01325 0.00735 0.0188 0.0203 0.9790 8.500 0.8379 0.01345 0.00760 0.0185 0.0198 0.9802 8.750 0.8650 0.01368 0.00786 0.0183 0.0190 0.9816 9.000 0.8907 0.01392 0.00812 0.0184 0.0178 0.9833 9.250 0.9152 0.01418 0.00837 0.0188 0.0165 0.9852 9.500 0.9439 0.01452 0.00870 0.0181 0.0149 0.9857 9.750 0.9718 0.01490 0.00914 0.0176 0.0140 0.9863 10.000 0.9992 0.01530 0.00955 0.0172 0.0126 0.9869 10.250 1.0260 0.01576 0.01002 0.0169 0.0112 0.9876 10.500 1.0524 0.01625 0.01057 0.0167 0.0105 0.9885 10.750 1.0780 0.01676 0.01114 0.0166 0.0098 0.9896 11.000 1.1025 0.01732 0.01174 0.0167 0.0091 0.9908 11.250 1.1257 0.01794 0.01243 0.0170 0.0085 0.9921 11.500 1.1479 0.01860 0.01317 0.0175 0.0080 0.9935 11.750 1.1711 0.01921 0.01387 0.0178 0.0077 0.9946 12.000 1.1952 0.01988 0.01463 0.0178 0.0074 0.9953 12.250 1.2183 0.02060 0.01543 0.0180 0.0071 0.9962 12.500 1.2404 0.02137 0.01629 0.0183 0.0067 0.9971 12.750 1.2617 0.02223 0.01725 0.0186 0.0064 0.9982 13.000 1.2819 0.02323 0.01834 0.0191 0.0061 0.9993 13.250 1.2938 0.02426 0.01948 0.0212 0.0058 1.0000 13.500 1.2924 0.02481 0.02011 0.0264 0.0057 1.0000 13.750 1.2925 0.02544 0.02084 0.0311 0.0056 1.0000 14.000 1.2944 0.02621 0.02171 0.0352 0.0055 1.0000 14.250 1.2973 0.02709 0.02269 0.0389 0.0054 1.0000 14.500 1.3003 0.02810 0.02381 0.0423 0.0053 1.0000 14.750 1.3035 0.02924 0.02507 0.0454 0.0052 1.0000 15.000 1.3062 0.03051 0.02645 0.0482 0.0051 1.0000 15.250 1.3077 0.03195 0.02802 0.0509 0.0050 1.0000 15.500 1.3081 0.03356 0.02977 0.0534 0.0049 1.0000 15.750 1.3062 0.03542 0.03176 0.0557 0.0049 1.0000 16.000 1.3026 0.03754 0.03402 0.0577 0.0048 1.0000 16.250 1.2959 0.04007 0.03669 0.0594 0.0047 1.0000 16.500 1.2860 0.04313 0.03990 0.0606 0.0047 1.0000 16.750 1.2716 0.04700 0.04394 0.0609 0.0046 1.0000 17.000 1.2509 0.05223 0.04935 0.0598 0.0046 1.0000 17.250 1.2152 0.06121 0.05857 0.0548 0.0047 1.0000