QFLR5_v.0001 Calculated polar for: KSLaminar1 1 1 Reynolds number fixed Mach number fixed xtrf = 1.000 (top) 1.000 (bottom) Mach = 0.270 Re = 4.500 e 6 Ncrit = 9.000 alpha CL CD CDp CM Top Xtr Bot Xtr Cpmin Chinge XCp ------- -------- --------- --------- -------- ------- ------- -------- --------- --------- -2.000 0.3228 0.00579 0.00109 -0.1156 0.5729 0.1599 -0.7912 0.0000 0.6109 -1.000 0.4490 0.00532 0.00098 -0.1179 0.5641 0.2884 -0.8689 0.0000 0.5124 -0.600 0.4991 0.00517 0.00097 -0.1187 0.5565 0.3498 -0.9000 0.0000 0.4870 -0.500 0.5115 0.00512 0.00096 -0.1190 0.5542 0.3727 -0.9077 0.0000 0.4815 0.000 0.5741 0.00489 0.00097 -0.1202 0.5403 0.4853 -0.9479 0.0000 0.4573 0.500 0.6377 0.00460 0.00099 -0.1215 0.5365 0.6082 -0.9905 0.0000 0.4378 1.000 0.6998 0.00462 0.00108 -0.1224 0.5251 0.6575 -1.0351 0.0000 0.4214 1.500 0.7616 0.00472 0.00117 -0.1231 0.5105 0.6778 -1.0859 0.0000 0.4076 2.000 0.8234 0.00484 0.00126 -0.1238 0.4997 0.6857 -1.1419 0.0000 0.3957 2.500 0.8843 0.00503 0.00138 -0.1244 0.4814 0.6927 -1.2058 0.0000 0.3853 3.000 0.9445 0.00524 0.00154 -0.1248 0.4621 0.7035 -1.2772 0.0000 0.3762 3.500 1.0042 0.00549 0.00172 -0.1251 0.4389 0.7109 -1.3590 0.0000 0.3680 4.000 1.0620 0.00587 0.00197 -0.1251 0.4076 0.7150 -1.4502 0.0000 0.3606 4.500 1.1178 0.00636 0.00229 -0.1247 0.3654 0.7206 -1.5546 0.0000 0.3537 5.000 1.1709 0.00700 0.00272 -0.1239 0.3166 0.7291 -1.6734 0.0000 0.3473 5.500 1.2251 0.00753 0.00314 -0.1231 0.2829 0.7350 -1.8111 0.0000 0.3414 6.000 1.2741 0.00834 0.00372 -0.1215 0.2338 0.7394 -1.9511 0.0000 0.3356 6.500 1.3246 0.00900 0.00423 -0.1201 0.2005 0.7422 -2.1191 0.0000 0.3302 7.000 1.3700 0.00987 0.00490 -0.1179 0.1623 0.7440 -2.2967 0.0000 0.3248 7.500 1.4175 0.01055 0.00551 -0.1159 0.1397 0.7542 -2.4834 0.0000 0.3198 8.000 1.4602 0.01135 0.00624 -0.1131 0.1174 0.7628 -2.6932 0.0000 0.3147 8.500 1.4951 0.01216 0.00699 -0.1088 0.1011 0.7695 -2.9182 0.0000 0.3092 9.000 1.5313 0.01309 0.00790 -0.1050 0.0872 0.7799 -3.1533 0.0000 0.3042 9.500 1.5655 0.01419 0.00901 -0.1012 0.0751 0.7946 -3.3891 0.0000 0.2994 10.000 1.5962 0.01557 0.01040 -0.0973 0.0638 0.8139 -3.6228 0.0000 0.2948 10.500 1.6274 0.01711 0.01200 -0.0939 0.0569 0.8417 -3.8639 0.0000 0.2906 11.000 1.6587 0.01877 0.01379 -0.0908 0.0502 0.8892 -4.1115 0.0000 0.2867 11.500 1.6776 0.02098 0.01619 -0.0864 0.0427 0.9999 -4.3282 0.0000 0.2825 12.000 1.7011 0.02353 0.01876 -0.0834 0.0370 0.9999 -4.6328 0.0000 0.2790 12.500 1.7210 0.02650 0.02175 -0.0804 0.0307 0.9999 -4.9476 0.0000 0.2756 13.000 1.7419 0.02951 0.02481 -0.0777 0.0282 0.9999 -5.2775 0.0000 0.2724 13.500 1.7544 0.03318 0.02854 -0.0747 0.0239 0.9999 -5.5765 0.0000 0.2692 14.000 1.7709 0.03675 0.03218 -0.0723 0.0220 0.9999 -5.9038 0.0000 0.2663 14.500 1.7833 0.04081 0.03631 -0.0699 0.0204 0.9999 -6.2805 0.0000 0.2635 15.000 1.7901 0.04543 0.04100 -0.0676 0.0182 0.9999 -6.6467 0.0000 0.2609 15.500 1.8003 0.04974 0.04538 -0.0654 0.0156 0.9999 -7.0442 0.0000 0.2582 16.000 1.8086 0.05456 0.05031 -0.0637 0.0151 0.9999 -7.4420 0.0000 0.2559 16.500 1.8153 0.05964 0.05551 -0.0622 0.0147 0.9999 -7.8399 0.0000 0.2537 17.000 1.8240 0.06449 0.06045 -0.0609 0.0137 0.9999 -8.2639 0.0000 0.2515 17.500 1.8130 0.07143 0.06748 -0.0597 0.0111 0.9999 -8.5523 0.0000 0.2497 18.000 1.8030 0.07862 0.07478 -0.0591 0.0088 0.9999 -8.8481 0.0000 0.2482 18.500 1.7910 0.08623 0.08250 -0.0590 0.0075 0.9999 -9.1290 0.0000 0.2470 19.000 1.7755 0.09437 0.09076 -0.0594 0.0063 0.9999 -9.3783 0.0000 0.2461 19.500 1.7653 0.10179 0.09830 -0.0600 0.0049 0.9999 -9.6686 0.0000 0.2452 20.000 1.7521 0.10998 0.10663 -0.0613 0.0045 0.9999 -9.9309 0.0000 0.2448 20.500 1.7369 0.11862 0.11542 -0.0634 0.0044 0.9999 -10.1711 0.0000 0.2448 21.000 1.7194 0.12771 0.12465 -0.0661 0.0042 0.9999 -10.3791 0.0000 0.2453 21.500 1.6993 0.13725 0.13434 -0.0696 0.0039 0.9999 -10.5483 0.0000 0.2464 22.000 1.6761 0.14726 0.14450 -0.0739 0.0036 0.9999 -10.6687 0.0000 0.2480 22.500 1.6513 0.15801 0.15539 -0.0793 0.0032 0.9999 -10.7453 0.0000 0.2505 23.000 1.6199 0.17027 0.16781 -0.0862 0.0029 0.9999 -10.7120 0.0000 0.2542