XFOIL Version 6.96 Calculated polar for: E. Bambino 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 ------ -------- --------- --------- -------- -------- -------- -6.750 -0.6154 0.09768 0.09633 0.0317 1.0000 0.0030 -6.500 -0.6141 0.09363 0.09230 0.0288 1.0000 0.0031 -6.250 -0.6129 0.08928 0.08796 0.0245 1.0000 0.0031 -6.000 -0.6057 0.08470 0.08337 0.0202 1.0000 0.0032 -5.750 -0.5964 0.08014 0.07878 0.0163 1.0000 0.0033 -5.500 -0.5871 0.07590 0.07440 0.0136 0.9271 0.0033 -5.250 -0.5804 0.07232 0.07042 0.0126 0.8100 0.0034 -5.000 -0.5661 0.06836 0.06592 0.0100 0.6707 0.0036 -4.750 -0.5494 0.06410 0.06142 0.0077 0.6225 0.0038 -4.500 -0.5308 0.05990 0.05698 0.0057 0.5792 0.0041 -2.000 -0.2898 0.02410 0.01779 0.0044 0.0593 0.0073 -1.750 -0.2635 0.02267 0.01619 0.0045 0.0585 0.0083 -1.500 -0.2357 0.02080 0.01408 0.0050 0.0569 0.0090 -1.250 -0.2076 0.01918 0.01224 0.0055 0.0553 0.0099 -1.000 -0.1790 0.01790 0.01079 0.0059 0.0527 0.0112 0.500 -0.0094 0.01124 0.00325 0.0085 0.0460 0.0085 0.750 0.0190 0.01093 0.00283 0.0086 0.0459 0.0085 1.000 0.0474 0.01081 0.00262 0.0086 0.0459 0.0118 1.250 0.0758 0.01087 0.00264 0.0085 0.0461 0.0138 1.500 0.1043 0.01101 0.00270 0.0085 0.0462 0.0156 1.750 0.1325 0.01111 0.00294 0.0083 0.0465 0.0591 2.000 0.1561 0.00934 0.00310 0.0079 0.0467 0.7301 2.250 0.1799 0.00930 0.00348 0.0089 0.0471 0.8566 3.000 0.2554 0.00977 0.00419 0.0112 0.0467 0.9816 3.250 0.2919 0.00962 0.00400 0.0092 0.0441 0.9933 3.750 0.3608 0.00977 0.00406 0.0058 0.0406 1.0000 4.000 0.3850 0.01041 0.00465 0.0061 0.0375 1.0000 4.250 0.4122 0.00903 0.00312 0.0064 0.0363 1.0000 4.750 0.4661 0.00874 0.00255 0.0064 0.0161 1.0000 5.000 0.4934 0.00901 0.00287 0.0064 0.0132 1.0000 5.250 0.5207 0.00925 0.00316 0.0063 0.0122 1.0000 5.500 0.5481 0.00951 0.00345 0.0062 0.0123 1.0000 5.750 0.5751 0.01001 0.00405 0.0061 0.0108 1.0000 6.000 0.6023 0.01043 0.00455 0.0060 0.0082 1.0000 6.250 0.6299 0.01070 0.00484 0.0059 0.0075 1.0000 6.500 0.6572 0.01110 0.00523 0.0058 0.0079 1.0000 7.500 0.7625 0.01397 0.00816 0.0059 0.0074 1.0000 8.000 0.8064 0.02019 0.01423 0.0066 0.0041 1.0000 11.000 0.9961 0.05118 0.04813 0.0132 0.0040 1.0000 11.250 0.9906 0.05417 0.05137 0.0139 0.0039 1.0000 11.500 0.9780 0.05722 0.05461 0.0148 0.0039 1.0000 11.750 0.9616 0.06099 0.05853 0.0139 0.0039 1.0000 12.000 0.9462 0.06617 0.06385 0.0101 0.0039 1.0000 12.250 0.9318 0.07246 0.07027 0.0048 0.0040 1.0000 12.500 0.9181 0.07960 0.07752 -0.0013 0.0040 1.0000 12.750 0.9053 0.08765 0.08567 -0.0081 0.0040 1.0000