S809 VENTED AILERON MODEL, 18 IN CHORD --------- Run Conditions: vel=108.8 ft/s Re=1.012x10^6 AOA=-6.01 Flap deflection=5.00 Totals: Cl=-0.2912 Cdp=0.0244 Cm(c/4)=-0.0289 Cs=0.0062 Ch=0.0157 Main component: Cl=-0.3044 Cdp=0.0259 Cm=0.0523 Flap component: Cl=0.0132 Cdp=-0.0015 Cm=-0.0082 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.1304 0.5871, 0.07930, -0.2291 0.5501, 0.08690, -0.3061 0.5112, 0.09370, -0.4660 0.4731, 0.09830, -0.5383 0.4349, 0.10070, -0.5240 0.3960, 0.10120, -0.4728 0.3566, 0.10020, -0.4032 0.3172, 0.09790, -0.3360 0.2778, 0.09440, -0.2839 0.2393, 0.08960, -0.2327 0.2056, 0.08360, -0.1572 0.1633, 0.07610, -0.0663 0.1261, 0.06710, 0.0658 0.0900, 0.05640, 0.1890 0.0571, 0.04390, 0.4015 0.0283, 0.02940, 0.6954 0.0142, 0.01970, 0.9062 0.0081, 0.01410, 0.9856 0.0026, 0.00780, 0.8065 0.0000, 0.00000, 0.0708 0.0037, -0.00840, -0.7859 0.0112, -0.01420, -1.0827 0.0191, -0.01930, -0.6492 0.0397, -0.03030, -0.6108 0.0706, -0.04420, -0.6240 0.1037, -0.05710, -0.6414 0.1384, -0.06890, -0.7211 0.1741, -0.07950, -0.7708 0.2102, -0.08660, -0.8526 0.2472, -0.09640, -0.9280 0.2844, -0.10270, -0.9541 0.3225, -0.10690, -0.9546 0.3608, -0.10890, -0.9390 0.3991, -0.10830, -0.8554 0.4373, -0.10510, -0.6993 0.4757, -0.09890, -0.4705 0.5137, -0.09070, -0.2704 0.5514, -0.08120, -0.1713 0.5917, -0.06870, -0.1349 0.5917, -0.02380, -0.1401 0.5917, 0.02120, -0.1415 16 Flap element taps 1.0000, 0.00130, 0.0867 0.9365, 0.01390, 0.0229 0.8333, 0.03280, -0.0938 0.7436, 0.04930, -0.2686 0.7049, 0.05670, -0.6688 0.6667, 0.05450, -0.0288 0.6302, 0.03770, -0.1386 0.6083, 0.01980, -0.1287 0.6000, 0.00000, -0.1385 0.6076, -0.01900, -0.1419 0.6285, -0.03060, -0.1388 0.6667, -0.04090, -0.1362 0.7046, -0.04120, -0.1480 0.7429, -0.03210, -0.1574 0.8333, -0.01400, -0.1413 0.9311, -0.00120, -0.0461 Wake drag found for this condition, Cdw=0.0277 --------- Run Conditions: vel=108.7 ft/s Re=1.011x10^6 AOA=0.00 Flap deflection=5.00 Totals: Cl=0.2145 Cdp=0.0135 Cm(c/4)=-0.0599 Cs=-0.0135 Ch=0.0098 Main component: Cl=0.0975 Cdp=0.0224 Cm=-0.0207 Flap component: Cl=0.1170 Cdp=-0.0089 Cm=-0.0928 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.1557 0.5871, 0.07930, -0.2761 0.5501, 0.08690, -0.3977 0.5112, 0.09370, -0.5952 0.4731, 0.09830, -0.7165 0.4349, 0.10070, -0.7418 0.3960, 0.10120, -0.7312 0.3566, 0.10020, -0.6846 0.3172, 0.09790, -0.6536 0.2778, 0.09440, -0.6385 0.2393, 0.08960, -0.6270 0.2056, 0.08360, -0.6017 0.1633, 0.07610, -0.5498 0.1261, 0.06710, -0.4741 0.0900, 0.05640, -0.4378 0.0571, 0.04390, -0.3138 0.0283, 0.02940, -0.0887 0.0142, 0.01970, 0.1122 0.0081, 0.01410, 0.2467 0.0026, 0.00780, 0.5295 0.0000, 0.00000, 0.9943 0.0037, -0.00840, 0.7959 0.0112, -0.01420, 0.4469 0.0191, -0.01930, 0.4363 0.0397, -0.03030, 0.2389 0.0706, -0.04420, 0.0552 0.1037, -0.05710, -0.0619 0.1384, -0.06890, -0.2021 0.1741, -0.07950, -0.3115 0.2102, -0.08660, -0.4447 0.2472, -0.09640, -0.5655 0.2844, -0.10270, -0.6458 0.3225, -0.10690, -0.7006 0.3608, -0.10890, -0.7552 0.3991, -0.10830, -0.7496 0.4373, -0.10510, -0.6878 0.4757, -0.09890, -0.5480 0.5137, -0.09070, -0.4094 0.5514, -0.08120, -0.2281 0.5917, -0.06870, -0.0949 0.5917, -0.02380, -0.0943 0.5917, 0.02120, -0.1575 16 Flap element taps 1.0000, 0.00130, 0.0798 0.9365, 0.01390, 0.0282 0.8333, 0.03280, -0.0743 0.7436, 0.04930, -0.2670 0.7049, 0.05670, -0.6038 0.6667, 0.05450, -0.2561 0.6302, 0.03770, -0.1415 0.6083, 0.01980, -0.1410 0.6000, 0.00000, -0.1644 0.6076, -0.01900, -0.1254 0.6285, -0.03060, -0.1189 0.6667, -0.04090, -0.1181 0.7046, -0.04120, 0.0389 0.7429, -0.03210, 0.2106 0.8333, -0.01400, 0.2865 0.9311, -0.00120, 0.2682 Wake drag found for this condition, Cdw=0.0187 --------- Run Conditions: vel=107.7 ft/s Re=0.999x10^6 AOA=3.03 Flap deflection=5.00 Totals: Cl=0.4488 Cdp=0.0192 Cm(c/4)=-0.0581 Cs=0.0045 Ch=0.0081 Main component: Cl=0.3150 Cdp=0.0200 Cm=-0.0641 Flap component: Cl=0.1338 Cdp=-0.0007 Cm=-0.1064 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.1659 0.5871, 0.07930, -0.2820 0.5501, 0.08690, -0.4129 0.5112, 0.09370, -0.6235 0.4731, 0.09830, -0.7712 0.4349, 0.10070, -0.8217 0.3960, 0.10120, -0.8392 0.3566, 0.10020, -0.8094 0.3172, 0.09790, -0.7992 0.2778, 0.09440, -0.8063 0.2393, 0.08960, -0.8232 0.2056, 0.08360, -0.8304 0.1633, 0.07610, -0.8044 0.1261, 0.06710, -0.7727 0.0900, 0.05640, -0.7953 0.0571, 0.04390, -0.7613 0.0283, 0.02940, -0.6411 0.0142, 0.01970, -0.5498 0.0081, 0.01410, -0.5303 0.0026, 0.00780, -0.1092 0.0000, 0.00000, 0.4665 0.0037, -0.00840, 1.0088 0.0112, -0.01420, 0.8487 0.0191, -0.01930, 0.7748 0.0397, -0.03030, 0.5576 0.0706, -0.04420, 0.3360 0.1037, -0.05710, 0.1957 0.1384, -0.06890, 0.0439 0.1741, -0.07950, -0.0875 0.2102, -0.08660, -0.2357 0.2472, -0.09640, -0.3633 0.2844, -0.10270, -0.4621 0.3225, -0.10690, -0.5245 0.3608, -0.10890, -0.6036 0.3991, -0.10830, -0.6167 0.4373, -0.10510, -0.5840 0.4757, -0.09890, -0.4716 0.5137, -0.09070, -0.3606 0.5514, -0.08120, -0.2000 0.5917, -0.06870, -0.0811 0.5917, -0.02380, -0.0764 0.5917, 0.02120, -0.1678 16 Flap element taps 1.0000, 0.00130, -0.0328 0.9365, 0.01390, -0.0762 0.8333, 0.03280, -0.1092 0.7436, 0.04930, -0.2146 0.7049, 0.05670, -0.4684 0.6667, 0.05450, -0.2552 0.6302, 0.03770, -0.1444 0.6083, 0.01980, -0.1422 0.6000, 0.00000, -0.1791 0.6076, -0.01900, -0.1253 0.6285, -0.03060, -0.1217 0.6667, -0.04090, -0.1000 0.7046, -0.04120, 0.2333 0.7429, -0.03210, 0.3196 0.8333, -0.01400, 0.2919 0.9311, -0.00120, 0.2412 Wake drag found for this condition, Cdw=0.0222 --------- Run Conditions: vel=107.2 ft/s Re=0.995x10^6 AOA=6.03 Flap deflection=5.00 Totals: Cl=0.6648 Cdp=0.0290 Cm(c/4)=-0.0551 Cs=0.0410 Ch=0.0077 Main component: Cl=0.5151 Cdp=0.0181 Cm=-0.1014 Flap component: Cl=0.1498 Cdp=0.0110 Cm=-0.1197 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.1853 0.5871, 0.07930, -0.2667 0.5501, 0.08690, -0.3956 0.5112, 0.09370, -0.6071 0.4731, 0.09830, -0.7845 0.4349, 0.10070, -0.8674 0.3960, 0.10120, -0.9180 0.3566, 0.10020, -0.9099 0.3172, 0.09790, -0.9261 0.2778, 0.09440, -0.9590 0.2393, 0.08960, -1.0080 0.2056, 0.08360, -1.0485 0.1633, 0.07610, -1.0595 0.1261, 0.06710, -1.0760 0.0900, 0.05640, -1.1731 0.0571, 0.04390, -1.2400 0.0283, 0.02940, -1.2783 0.0142, 0.01970, -1.3823 0.0081, 0.01410, -1.4362 0.0026, 0.00780, -1.0480 0.0000, 0.00000, -0.7814 0.0037, -0.00840, 0.8920 0.0112, -0.01420, 1.0128 0.0191, -0.01930, 0.9631 0.0397, -0.03030, 0.7876 0.0706, -0.04420, 0.5675 0.1037, -0.05710, 0.4131 0.1384, -0.06890, 0.2598 0.1741, -0.07950, 0.1182 0.2102, -0.08660, -0.0424 0.2472, -0.09640, -0.1792 0.2844, -0.10270, -0.2933 0.3225, -0.10690, -0.3737 0.3608, -0.10890, -0.4667 0.3991, -0.10830, -0.5014 0.4373, -0.10510, -0.4830 0.4757, -0.09890, -0.3887 0.5137, -0.09070, -0.3047 0.5514, -0.08120, -0.1537 0.5917, -0.06870, -0.0741 0.5917, -0.02380, -0.0540 0.5917, 0.02120, -0.1797 16 Flap element taps 1.0000, 0.00130, -0.1314 0.9365, 0.01390, -0.1680 0.8333, 0.03280, -0.1709 0.7436, 0.04930, -0.1979 0.7049, 0.05670, -0.3112 0.6667, 0.05450, -0.2337 0.6302, 0.03770, -0.1487 0.6083, 0.01980, -0.1443 0.6000, 0.00000, -0.2014 0.6076, -0.01900, -0.1227 0.6285, -0.03060, -0.1398 0.6667, -0.04090, -0.0132 0.7046, -0.04120, 0.4840 0.7429, -0.03210, 0.3397 0.8333, -0.01400, 0.2863 0.9311, -0.00120, 0.2174 Wake drag found for this condition, Cdw=0.0283 --------- Run Conditions: vel=107.4 ft/s Re=0.995x10^6 AOA=9.04 Flap deflection=5.00 Totals: Cl=0.8807 Cdp=0.0444 Cm(c/4)=-0.0533 Cs=0.0945 Ch=0.0181 Main component: Cl=0.7091 Cdp=0.0216 Cm=-0.1360 Flap component: Cl=0.1716 Cdp=0.0228 Cm=-0.1365 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.2729 0.5871, 0.07930, -0.3135 0.5501, 0.08690, -0.3947 0.5112, 0.09370, -0.5672 0.4731, 0.09830, -0.7676 0.4349, 0.10070, -0.8880 0.3960, 0.10120, -0.9740 0.3566, 0.10020, -0.9993 0.3172, 0.09790, -1.0446 0.2778, 0.09440, -1.1053 0.2393, 0.08960, -1.1845 0.2056, 0.08360, -1.2642 0.1633, 0.07610, -1.3176 0.1261, 0.06710, -1.3877 0.0900, 0.05640, -1.5656 0.0571, 0.04390, -1.7589 0.0283, 0.02940, -1.9946 0.0142, 0.01970, -2.3444 0.0081, 0.01410, -2.5861 0.0026, 0.00780, -2.3096 0.0000, 0.00000, -2.7160 0.0037, -0.00840, 0.4232 0.0112, -0.01420, 0.9588 0.0191, -0.01930, 1.0195 0.0397, -0.03030, 0.9430 0.0706, -0.04420, 0.7516 0.1037, -0.05710, 0.6015 0.1384, -0.06890, 0.4518 0.1741, -0.07950, 0.3128 0.2102, -0.08660, 0.1448 0.2472, -0.09640, 0.0045 0.2844, -0.10270, -0.1217 0.3225, -0.10690, -0.2114 0.3608, -0.10890, -0.3195 0.3991, -0.10830, -0.3690 0.4373, -0.10510, -0.3749 0.4757, -0.09890, -0.3155 0.5137, -0.09070, -0.2598 0.5514, -0.08120, -0.1703 0.5917, -0.06870, -0.0872 0.5917, -0.02380, 0.0154 0.5917, 0.02120, -0.2525 16 Flap element taps 1.0000, 0.00130, -0.1791 0.9365, 0.01390, -0.2105 0.8333, 0.03280, -0.2008 0.7436, 0.04930, -0.2083 0.7049, 0.05670, -0.2794 0.6667, 0.05450, -0.2665 0.6302, 0.03770, -0.1935 0.6083, 0.01980, -0.1862 0.6000, 0.00000, -0.3091 0.6076, -0.01900, -0.1586 0.6285, -0.03060, -0.2087 0.6667, -0.04090, 0.3981 0.7046, -0.04120, 0.4954 0.7429, -0.03210, 0.3394 0.8333, -0.01400, 0.2943 0.9311, -0.00120, 0.2135 --------- Run Conditions: vel=107.9 ft/s Re=1.000x10^6 AOA=12.05 Flap deflection=5.00 Totals: Cl=1.0602 Cdp=0.0714 Cm(c/4)=-0.0558 Cs=0.1515 Ch=0.0297 Main component: Cl=0.8623 Cdp=0.0348 Cm=-0.1614 Flap component: Cl=0.1979 Cdp=0.0366 Cm=-0.1573 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.4004 0.5871, 0.07930, -0.4228 0.5501, 0.08690, -0.4456 0.5112, 0.09370, -0.5059 0.4731, 0.09830, -0.6482 0.4349, 0.10070, -0.7989 0.3960, 0.10120, -0.9322 0.3566, 0.10020, -1.0048 0.3172, 0.09790, -1.0895 0.2778, 0.09440, -1.1871 0.2393, 0.08960, -1.2985 0.2056, 0.08360, -1.4164 0.1633, 0.07610, -1.5216 0.1261, 0.06710, -1.6518 0.0900, 0.05640, -1.9071 0.0571, 0.04390, -2.2325 0.0283, 0.02940, -2.6892 0.0142, 0.01970, -3.3152 0.0081, 0.01410, -3.8010 0.0026, 0.00780, -3.6789 0.0000, 0.00000, -5.0386 0.0037, -0.00840, -0.3090 0.0112, -0.01420, 0.7365 0.0191, -0.01930, 0.9624 0.0397, -0.03030, 1.0114 0.0706, -0.04420, 0.8785 0.1037, -0.05710, 0.7462 0.1384, -0.06890, 0.6058 0.1741, -0.07950, 0.4695 0.2102, -0.08660, 0.3071 0.2472, -0.09640, 0.1638 0.2844, -0.10270, 0.0327 0.3225, -0.10690, -0.0661 0.3608, -0.10890, -0.1828 0.3991, -0.10830, -0.2466 0.4373, -0.10510, -0.2721 0.4757, -0.09890, -0.2306 0.5137, -0.09070, -0.1862 0.5514, -0.08120, -0.1533 0.5917, -0.06870, -0.0783 0.5917, -0.02380, -0.0085 0.5917, 0.02120, -0.3605 16 Flap element taps 1.0000, 0.00130, -0.2242 0.9365, 0.01390, -0.2594 0.8333, 0.03280, -0.2468 0.7436, 0.04930, -0.2470 0.7049, 0.05670, -0.2894 0.6667, 0.05450, -0.3385 0.6302, 0.03770, -0.2561 0.6083, 0.01980, -0.2472 0.6000, 0.00000, -0.4900 0.6076, -0.01900, -0.2212 0.6285, -0.03060, -0.2672 0.6667, -0.04090, 0.7927 0.7046, -0.04120, 0.4419 0.7429, -0.03210, 0.3496 0.8333, -0.01400, 0.3017 0.9311, -0.00120, 0.2068 --------- Run Conditions: vel=106.6 ft/s Re=0.987x10^6 AOA=15.02 Flap deflection=5.00 Totals: Cl=1.0140 Cdp=0.1489 Cm(c/4)=-0.0847 Cs=0.1190 Ch=0.0410 Main component: Cl=0.7624 Cdp=0.0815 Cm=-0.1359 Flap component: Cl=0.2516 Cdp=0.0673 Cm=-0.2033 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.5831 0.5871, 0.07930, -0.5735 0.5501, 0.08690, -0.5736 0.5112, 0.09370, -0.5794 0.4731, 0.09830, -0.5886 0.4349, 0.10070, -0.6044 0.3960, 0.10120, -0.6441 0.3566, 0.10020, -0.6715 0.3172, 0.09790, -0.7379 0.2778, 0.09440, -0.8314 0.2393, 0.08960, -0.9605 0.2056, 0.08360, -1.1110 0.1633, 0.07610, -1.2696 0.1261, 0.06710, -1.4511 0.0900, 0.05640, -1.7396 0.0571, 0.04390, -2.1269 0.0283, 0.02940, -2.6787 0.0142, 0.01970, -3.3898 0.0081, 0.01410, -3.9824 0.0026, 0.00780, -3.9452 0.0000, 0.00000, -5.6345 0.0037, -0.00840, -0.5561 0.0112, -0.01420, 0.6412 0.0191, -0.01930, 0.9266 0.0397, -0.03030, 1.0242 0.0706, -0.04420, 0.9156 0.1037, -0.05710, 0.7943 0.1384, -0.06890, 0.6547 0.1741, -0.07950, 0.5180 0.2102, -0.08660, 0.3548 0.2472, -0.09640, 0.2069 0.2844, -0.10270, 0.0685 0.3225, -0.10690, -0.0416 0.3608, -0.10890, -0.1684 0.3991, -0.10830, -0.2448 0.4373, -0.10510, -0.2812 0.4757, -0.09890, -0.2531 0.5137, -0.09070, -0.2164 0.5514, -0.08120, -0.1656 0.5917, -0.06870, -0.1585 0.5917, -0.02380, -0.0476 0.5917, 0.02120, -0.5348 16 Flap element taps 1.0000, 0.00130, -0.4211 0.9365, 0.01390, -0.4576 0.8333, 0.03280, -0.4669 0.7436, 0.04930, -0.4812 0.7049, 0.05670, -0.5420 0.6667, 0.05450, -0.6104 0.6302, 0.03770, -0.3895 0.6083, 0.01980, -0.3703 0.6000, 0.00000, -0.7049 0.6076, -0.01900, -0.3532 0.6285, -0.03060, -0.3920 0.6667, -0.04090, 0.9093 0.7046, -0.04120, 0.3816 0.7429, -0.03210, 0.3097 0.8333, -0.01400, 0.2457 0.9311, -0.00120, 0.1216 --------- Run Conditions: vel=106.6 ft/s Re=0.986x10^6 AOA=18.00 Flap deflection=5.00 Totals: Cl=0.8906 Cdp=0.2494 Cm(c/4)=-0.1148 Cs=0.0380 Ch=0.0430 Main component: Cl=0.6271 Cdp=0.1677 Cm=-0.1305 Flap component: Cl=0.2635 Cdp=0.0817 Cm=-0.2153 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.7359 0.5871, 0.07930, -0.6792 0.5501, 0.08690, -0.6897 0.5112, 0.09370, -0.7093 0.4731, 0.09830, -0.7356 0.4349, 0.10070, -0.7413 0.3960, 0.10120, -0.7576 0.3566, 0.10020, -0.7497 0.3172, 0.09790, -0.7673 0.2778, 0.09440, -0.7779 0.2393, 0.08960, -0.7954 0.2056, 0.08360, -0.8233 0.1633, 0.07610, -0.8594 0.1261, 0.06710, -0.9134 0.0900, 0.05640, -1.0254 0.0571, 0.04390, -1.3319 0.0283, 0.02940, -1.9010 0.0142, 0.01970, -2.5930 0.0081, 0.01410, -3.1748 0.0026, 0.00780, -3.2673 0.0000, 0.00000, -4.8090 0.0037, -0.00840, -0.4013 0.0112, -0.01420, 0.6704 0.0191, -0.01930, 0.9278 0.0397, -0.03030, 1.0184 0.0706, -0.04420, 0.9157 0.1037, -0.05710, 0.7983 0.1384, -0.06890, 0.6615 0.1741, -0.07950, 0.5279 0.2102, -0.08660, 0.3651 0.2472, -0.09640, 0.2145 0.2844, -0.10270, 0.0738 0.3225, -0.10690, -0.0400 0.3608, -0.10890, -0.1720 0.3991, -0.10830, -0.2591 0.4373, -0.10510, -0.3028 0.4757, -0.09890, -0.2823 0.5137, -0.09070, -0.2543 0.5514, -0.08120, -0.1955 0.5917, -0.06870, -0.2555 0.5917, -0.02380, -0.1232 0.5917, 0.02120, -0.6614 16 Flap element taps 1.0000, 0.00130, -0.4985 0.9365, 0.01390, -0.5526 0.8333, 0.03280, -0.5465 0.7436, 0.04930, -0.5382 0.7049, 0.05670, -0.5773 0.6667, 0.05450, -0.7522 0.6302, 0.03770, -0.4767 0.6083, 0.01980, -0.4530 0.6000, 0.00000, -0.8920 0.6076, -0.01900, -0.4963 0.6285, -0.03060, -0.4662 0.6667, -0.04090, 0.9500 0.7046, -0.04120, 0.3322 0.7429, -0.03210, 0.2739 0.8333, -0.01400, 0.2065 0.9311, -0.00120, 0.0734 --------- Run Conditions: vel=106.6 ft/s Re=0.985x10^6 AOA=20.01 Flap deflection=5.00 Totals: Cl=0.8941 Cdp=0.3342 Cm(c/4)=-0.1366 Cs=-0.0080 Ch=0.0452 Main component: Cl=0.6160 Cdp=0.2413 Cm=-0.1463 Flap component: Cl=0.2782 Cdp=0.0929 Cm=-0.2290 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.8553 0.5871, 0.07930, -0.7953 0.5501, 0.08690, -0.7744 0.5112, 0.09370, -0.7776 0.4731, 0.09830, -0.8125 0.4349, 0.10070, -0.8394 0.3960, 0.10120, -0.8679 0.3566, 0.10020, -0.8528 0.3172, 0.09790, -0.8667 0.2778, 0.09440, -0.8762 0.2393, 0.08960, -0.8939 0.2056, 0.08360, -0.9079 0.1633, 0.07610, -0.9246 0.1261, 0.06710, -0.9477 0.0900, 0.05640, -0.9766 0.0571, 0.04390, -1.0366 0.0283, 0.02940, -1.2969 0.0142, 0.01970, -1.7509 0.0081, 0.01410, -2.2522 0.0026, 0.00780, -2.5067 0.0000, 0.00000, -4.0357 0.0037, -0.00840, -0.2980 0.0112, -0.01420, 0.6838 0.0191, -0.01930, 0.9272 0.0397, -0.03030, 1.0209 0.0706, -0.04420, 0.9280 0.1037, -0.05710, 0.8198 0.1384, -0.06890, 0.6880 0.1741, -0.07950, 0.5583 0.2102, -0.08660, 0.4002 0.2472, -0.09640, 0.2500 0.2844, -0.10270, 0.1098 0.3225, -0.10690, -0.0079 0.3608, -0.10890, -0.1425 0.3991, -0.10830, -0.2340 0.4373, -0.10510, -0.2824 0.4757, -0.09890, -0.2708 0.5137, -0.09070, -0.2548 0.5514, -0.08120, -0.1941 0.5917, -0.06870, -0.3106 0.5917, -0.02380, -0.1778 0.5917, 0.02120, -0.7737 16 Flap element taps 1.0000, 0.00130, -0.5416 0.9365, 0.01390, -0.6049 0.8333, 0.03280, -0.6075 0.7436, 0.04930, -0.5887 0.7049, 0.05670, -0.6365 0.6667, 0.05450, -0.8557 0.6302, 0.03770, -0.5280 0.6083, 0.01980, -0.5003 0.6000, 0.00000, -1.1020 0.6076, -0.01900, -0.6318 0.6285, -0.03060, -0.4944 0.6667, -0.04090, 0.9790 0.7046, -0.04120, 0.3043 0.7429, -0.03210, 0.2686 0.8333, -0.01400, 0.1986 0.9311, -0.00120, 0.0601 --------- Run Conditions: vel=107.5 ft/s Re=0.993x10^6 AOA=23.99 Flap deflection=5.00 Totals: Cl=0.9302 Cdp=0.4634 Cm(c/4)=-0.1543 Cs=-0.0451 Ch=0.0499 Main component: Cl=0.6422 Cdp=0.3438 Cm=-0.1706 Flap component: Cl=0.2880 Cdp=0.1195 Cm=-0.2432 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.9387 0.5871, 0.07930, -0.9138 0.5501, 0.08690, -0.9001 0.5112, 0.09370, -0.8922 0.4731, 0.09830, -0.9005 0.4349, 0.10070, -0.8921 0.3960, 0.10120, -0.9148 0.3566, 0.10020, -0.9116 0.3172, 0.09790, -0.9259 0.2778, 0.09440, -0.9446 0.2393, 0.08960, -0.9626 0.2056, 0.08360, -0.9904 0.1633, 0.07610, -1.0271 0.1261, 0.06710, -1.0719 0.0900, 0.05640, -1.1234 0.0571, 0.04390, -1.1582 0.0283, 0.02940, -1.2308 0.0142, 0.01970, -1.3191 0.0081, 0.01410, -1.3971 0.0026, 0.00780, -1.3271 0.0000, 0.00000, -2.8801 0.0037, -0.00840, -0.2567 0.0112, -0.01420, 0.6343 0.0191, -0.01930, 0.8897 0.0397, -0.03030, 1.0172 0.0706, -0.04420, 0.9580 0.1037, -0.05710, 0.8699 0.1384, -0.06890, 0.7498 0.1741, -0.07950, 0.6301 0.2102, -0.08660, 0.4802 0.2472, -0.09640, 0.3349 0.2844, -0.10270, 0.1954 0.3225, -0.10690, 0.0732 0.3608, -0.10890, -0.0647 0.3991, -0.10830, -0.1651 0.4373, -0.10510, -0.2254 0.4757, -0.09890, -0.2261 0.5137, -0.09070, -0.2223 0.5514, -0.08120, -0.1694 0.5917, -0.06870, -0.3547 0.5917, -0.02380, -0.2754 0.5917, 0.02120, -0.8409 16 Flap element taps 1.0000, 0.00130, -0.6109 0.9365, 0.01390, -0.6593 0.8333, 0.03280, -0.6598 0.7436, 0.04930, -0.6650 0.7049, 0.05670, -0.7706 0.6667, 0.05450, -0.9845 0.6302, 0.03770, -0.5433 0.6083, 0.01980, -0.5182 0.6000, 0.00000, -1.2138 0.6076, -0.01900, -0.7436 0.6285, -0.03060, -0.4971 0.6667, -0.04090, 0.9746 0.7046, -0.04120, 0.2839 0.7429, -0.03210, 0.2630 0.8333, -0.01400, 0.1835 0.9311, -0.00120, 0.0347 --------- Run Conditions: vel=106.6 ft/s Re=0.982x10^6 AOA=26.95 Flap deflection=5.00 Totals: Cl=0.9004 Cdp=0.5288 Cm(c/4)=-0.1669 Cs=-0.0633 Ch=0.0508 Main component: Cl=0.6010 Cdp=0.3667 Cm=-0.1615 Flap component: Cl=0.2994 Cdp=0.1621 Cm=-0.2659 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.8496 0.5871, 0.07930, -0.8067 0.5501, 0.08690, -0.7929 0.5112, 0.09370, -0.7811 0.4731, 0.09830, -0.7941 0.4349, 0.10070, -0.7963 0.3960, 0.10120, -0.8096 0.3566, 0.10020, -0.8236 0.3172, 0.09790, -0.8519 0.2778, 0.09440, -0.8801 0.2393, 0.08960, -0.9454 0.2056, 0.08360, -0.9757 0.1633, 0.07610, -1.0109 0.1261, 0.06710, -1.0375 0.0900, 0.05640, -1.0708 0.0571, 0.04390, -1.1111 0.0283, 0.02940, -1.1347 0.0142, 0.01970, -1.1822 0.0081, 0.01410, -1.2182 0.0026, 0.00780, -1.0642 0.0000, 0.00000, -2.0310 0.0037, -0.00840, -0.1822 0.0112, -0.01420, 0.6266 0.0191, -0.01930, 0.8794 0.0397, -0.03030, 1.0185 0.0706, -0.04420, 0.9763 0.1037, -0.05710, 0.9015 0.1384, -0.06890, 0.7859 0.1741, -0.07950, 0.6714 0.2102, -0.08660, 0.5276 0.2472, -0.09640, 0.3821 0.2844, -0.10270, 0.2428 0.3225, -0.10690, 0.1163 0.3608, -0.10890, -0.0236 0.3991, -0.10830, -0.1303 0.4373, -0.10510, -0.1972 0.4757, -0.09890, -0.2035 0.5137, -0.09070, -0.2054 0.5514, -0.08120, -0.1514 0.5917, -0.06870, -0.3041 0.5917, -0.02380, -0.1716 0.5917, 0.02120, -0.7592 16 Flap element taps 1.0000, 0.00130, -0.7322 0.9365, 0.01390, -0.7629 0.8333, 0.03280, -0.7779 0.7436, 0.04930, -0.8287 0.7049, 0.05670, -0.9572 0.6667, 0.05450, -0.9345 0.6302, 0.03770, -0.5134 0.6083, 0.01980, -0.4785 0.6000, 0.00000, -1.0746 0.6076, -0.01900, -0.6294 0.6285, -0.03060, -0.4966 0.6667, -0.04090, 0.9861 0.7046, -0.04120, 0.2844 0.7429, -0.03210, 0.2515 0.8333, -0.01400, 0.1622 0.9311, -0.00120, -0.0059