S809 UNVENTED AILERON, CLEAN, CHORD = 18 IN --------- Run Conditions: vel=106.3 ft/s Re=1.002x10^6 AOA=-6.00 Flap deflection=-5.00 Totals: Cl=-0.6991 Cdp=0.0398 Cm(c/4)=0.0346 Cs=0.0334 Ch=0.0747 Main component: Cl=-0.6151 Cdp=0.0327 Cm=0.1427 Flap component: Cl=-0.0839 Cdp=0.0071 Cm=0.0668 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.2644 0.6175, -0.04610, -0.2242 0.5841, -0.02440, -0.1754 0.5775, 0.01750, -0.1761 0.5777, 0.04660, -0.1815 0.6274, 0.07170, 0.1978 0.5694, 0.08320, -0.1929 0.5112, 0.09370, -0.2260 0.4731, 0.09830, -0.2870 0.4349, 0.10070, -0.3069 0.3960, 0.10120, -0.2736 0.3566, 0.10020, -0.1997 0.3172, 0.09790, -0.1387 0.2778, 0.09440, -0.0943 0.2393, 0.08960, -0.0363 0.2056, 0.08360, 0.0119 0.1633, 0.07610, 0.1366 0.1261, 0.06710, 0.2478 0.0900, 0.05640, 0.4166 0.0571, 0.04390, 0.6178 0.0283, 0.02940, 0.8731 0.0142, 0.01970, 1.0119 0.0081, 0.01410, 0.9793 0.0026, 0.00780, 0.6557 0.0000, 0.00000, -0.8324 0.0037, -0.00840, -1.8600 0.0112, -0.01420, -1.5196 0.0191, -0.01930, -1.3042 0.0397, -0.03030, -1.0295 0.0706, -0.04420, -0.9443 0.1037, -0.05710, -0.9819 0.1384, -0.06890, -1.0069 0.1741, -0.07950, -1.0542 0.2102, -0.08660, -1.1425 0.2472, -0.09640, -1.2258 0.2844, -0.10270, -1.2571 0.3225, -0.10690, -1.2500 0.3608, -0.10890, -1.2558 0.3991, -0.10830, -1.1665 0.4373, -0.10510, -1.0550 0.4757, -0.09890, -0.8165 0.5137, -0.09070, -0.6260 0.5694, -0.07640, -0.3545 15 Flap element taps 1.0000, 0.00130, -0.0806 0.9365, 0.01390, 0.0172 0.8333, 0.03280, 0.0433 0.7436, 0.04930, 0.0689 0.7049, 0.05670, 0.1219 0.6662, 0.06410, 0.0131 0.6522, 0.01390, -0.1797 0.5969, -0.00020, -0.1847 0.6000, -0.03020, -0.2386 0.6324, -0.04540, -0.2409 0.6667, -0.04880, -0.2448 0.7046, -0.04110, -0.2307 0.7429, -0.03210, -0.2309 0.8333, -0.01400, -0.2270 0.9311, -0.00120, -0.1605 Wake drag found for this condition, Cdw=0.0517 --------- Run Conditions: vel=106.3 ft/s Re=1.004x10^6 AOA=0.02 Flap deflection=-5.00 Totals: Cl=-0.2705 Cdp=0.0104 Cm(c/4)=0.0270 Cs=-0.0105 Ch=0.0010 Main component: Cl=-0.2525 Cdp=0.0343 Cm=0.0841 Flap component: Cl=-0.0180 Cdp=-0.0239 Cm=0.0106 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.3012 0.6175, -0.04610, -0.2253 0.5841, -0.02440, -0.1844 0.5775, 0.01750, -0.1826 0.5777, 0.04660, -0.1894 0.6274, 0.07170, 0.1327 0.5694, 0.08320, -0.0705 0.5112, 0.09370, -0.4089 0.4731, 0.09830, -0.4352 0.4349, 0.10070, -0.5007 0.3960, 0.10120, -0.5319 0.3566, 0.10020, -0.4511 0.3172, 0.09790, -0.4209 0.2778, 0.09440, -0.4046 0.2393, 0.08960, -0.3861 0.2056, 0.08360, -0.4021 0.1633, 0.07610, -0.2817 0.1261, 0.06710, -0.2315 0.0900, 0.05640, -0.0973 0.0571, 0.04390, 0.0486 0.0283, 0.02940, 0.2951 0.0142, 0.01970, 0.5533 0.0081, 0.01410, 0.6783 0.0026, 0.00780, 0.9369 0.0000, 0.00000, 0.9617 0.0037, -0.00840, 0.3379 0.0112, -0.01420, 0.1140 0.0191, -0.01930, 0.0407 0.0397, -0.03030, -0.0613 0.0706, -0.04420, -0.2331 0.1037, -0.05710, -0.3819 0.1384, -0.06890, -0.4569 0.1741, -0.07950, -0.5807 0.2102, -0.08660, -0.7512 0.2472, -0.09640, -0.8647 0.2844, -0.10270, -0.9666 0.3225, -0.10690, -1.0008 0.3608, -0.10890, -1.0832 0.3991, -0.10830, -1.0509 0.4373, -0.10510, -1.0105 0.4757, -0.09890, -0.9361 0.5137, -0.09070, -0.9020 0.5694, -0.07640, -0.4084 15 Flap element taps 1.0000, 0.00130, 0.1940 0.9365, 0.01390, 0.1313 0.8333, 0.03280, 0.0722 0.7436, 0.04930, 0.0556 0.7049, 0.05670, 0.0857 0.6662, 0.06410, -0.0175 0.6522, 0.01390, -0.1929 0.5969, -0.00020, -0.1899 0.6000, -0.03020, -0.2426 0.6324, -0.04540, -0.2481 0.6667, -0.04880, -0.2733 0.7046, -0.04110, -0.1554 0.7429, -0.03210, -0.0462 0.8333, -0.01400, 0.1026 0.9311, -0.00120, 0.2154 Wake drag found for this condition, Cdw=0.0115 --------- Run Conditions: vel=106.8 ft/s Re=1.009x10^6 AOA=3.03 Flap deflection=-5.00 Totals: Cl=0.0668 Cdp=0.0033 Cm(c/4)=0.0192 Cs=0.0003 Ch=-0.0192 Main component: Cl=0.0587 Cdp=0.0282 Cm=0.0114 Flap component: Cl=0.0081 Cdp=-0.0249 Cm=-0.0089 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.2329 0.6175, -0.04610, -0.1791 0.5841, -0.02440, -0.1498 0.5775, 0.01750, -0.1504 0.5777, 0.04660, -0.1590 0.6274, 0.07170, 0.0712 0.5694, 0.08320, -0.0910 0.5112, 0.09370, -0.5649 0.4731, 0.09830, -0.5792 0.4349, 0.10070, -0.6532 0.3960, 0.10120, -0.7276 0.3566, 0.10020, -0.6366 0.3172, 0.09790, -0.6253 0.2778, 0.09440, -0.6281 0.2393, 0.08960, -0.6364 0.2056, 0.08360, -0.6986 0.1633, 0.07610, -0.5833 0.1261, 0.06710, -0.5845 0.0900, 0.05640, -0.4906 0.0571, 0.04390, -0.4249 0.0283, 0.02940, -0.2753 0.0142, 0.01970, -0.0769 0.0081, 0.01410, 0.0179 0.0026, 0.00780, 0.3557 0.0000, 0.00000, 0.9044 0.0037, -0.00840, 0.9344 0.0112, -0.01420, 0.7100 0.0191, -0.01930, 0.5816 0.0397, -0.03030, 0.3919 0.0706, -0.04420, 0.1505 0.1037, -0.05710, -0.0311 0.1384, -0.06890, -0.1087 0.1741, -0.07950, -0.2566 0.2102, -0.08660, -0.4631 0.2472, -0.09640, -0.5770 0.2844, -0.10270, -0.7069 0.3225, -0.10690, -0.7376 0.3608, -0.10890, -0.8508 0.3991, -0.10830, -0.8334 0.4373, -0.10510, -0.8326 0.4757, -0.09890, -0.7449 0.5137, -0.09070, -0.7266 0.5694, -0.07640, -0.3063 15 Flap element taps 1.0000, 0.00130, 0.1996 0.9365, 0.01390, 0.1199 0.8333, 0.03280, 0.0387 0.7436, 0.04930, 0.0091 0.7049, 0.05670, 0.0338 0.6662, 0.06410, -0.1037 0.6522, 0.01390, -0.1713 0.5969, -0.00020, -0.1549 0.6000, -0.03020, -0.1935 0.6324, -0.04540, -0.2106 0.6667, -0.04880, -0.2253 0.7046, -0.04110, -0.0993 0.7429, -0.03210, -0.0029 0.8333, -0.01400, 0.1361 0.9311, -0.00120, 0.2526 Wake drag found for this condition, Cdw=0.0100 --------- Run Conditions: vel=107.1 ft/s Re=1.011x10^6 AOA=6.02 Flap deflection=-5.00 Totals: Cl=0.4210 Cdp=0.0027 Cm(c/4)=0.0074 Cs=0.0414 Ch=-0.0396 Main component: Cl=0.3849 Cdp=0.0260 Cm=-0.0676 Flap component: Cl=0.0361 Cdp=-0.0232 Cm=-0.0298 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.1582 0.6175, -0.04610, -0.1309 0.5841, -0.02440, -0.1172 0.5775, 0.01750, -0.1196 0.5777, 0.04660, -0.1283 0.6274, 0.07170, 0.0020 0.5694, 0.08320, -0.2284 0.5112, 0.09370, -0.7088 0.4731, 0.09830, -0.7626 0.4349, 0.10070, -0.8298 0.3960, 0.10120, -0.9298 0.3566, 0.10020, -0.8373 0.3172, 0.09790, -0.8436 0.2778, 0.09440, -0.8665 0.2393, 0.08960, -0.9010 0.2056, 0.08360, -1.0131 0.1633, 0.07610, -0.9147 0.1261, 0.06710, -0.9747 0.0900, 0.05640, -0.9406 0.0571, 0.04390, -0.9915 0.0283, 0.02940, -1.0111 0.0142, 0.01970, -0.9829 0.0081, 0.01410, -1.0436 0.0026, 0.00780, -0.6747 0.0000, 0.00000, -0.1090 0.0037, -0.00840, 0.9878 0.0112, -0.01420, 0.9913 0.0191, -0.01930, 0.9110 0.0397, -0.03030, 0.7296 0.0706, -0.04420, 0.4704 0.1037, -0.05710, 0.2779 0.1384, -0.06890, 0.2044 0.1741, -0.07950, 0.0431 0.2102, -0.08660, -0.1903 0.2472, -0.09640, -0.2990 0.2844, -0.10270, -0.4511 0.3225, -0.10690, -0.4825 0.3608, -0.10890, -0.6203 0.3991, -0.10830, -0.6161 0.4373, -0.10510, -0.6516 0.4757, -0.09890, -0.5643 0.5137, -0.09070, -0.5336 0.5694, -0.07640, -0.1810 15 Flap element taps 1.0000, 0.00130, 0.2059 0.9365, 0.01390, 0.1137 0.8333, 0.03280, 0.0096 0.7436, 0.04930, -0.0370 0.7049, 0.05670, -0.0224 0.6662, 0.06410, -0.1868 0.6522, 0.01390, -0.1419 0.5969, -0.00020, -0.1162 0.6000, -0.03020, -0.1417 0.6324, -0.04540, -0.1660 0.6667, -0.04880, -0.1520 0.7046, -0.04110, -0.0291 0.7429, -0.03210, 0.0532 0.8333, -0.01400, 0.1769 0.9311, -0.00120, 0.2883 Wake drag found for this condition, Cdw=0.0089 --------- Run Conditions: vel=106.0 ft/s Re=1.004x10^6 AOA=9.01 Flap deflection=-5.00 Totals: Cl=0.6928 Cdp=0.0099 Cm(c/4)=0.0067 Cs=0.0987 Ch=-0.0532 Main component: Cl=0.6314 Cdp=0.0306 Cm=-0.1171 Flap component: Cl=0.0614 Cdp=-0.0207 Cm=-0.0476 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.1019 0.6175, -0.04610, -0.1312 0.5841, -0.02440, -0.1352 0.5775, 0.01750, -0.1383 0.5777, 0.04660, -0.1487 0.6274, 0.07170, -0.1631 0.5694, 0.08320, -0.3068 0.5112, 0.09370, -0.6319 0.4731, 0.09830, -0.8107 0.4349, 0.10070, -0.9244 0.3960, 0.10120, -1.0561 0.3566, 0.10020, -0.9683 0.3172, 0.09790, -0.9902 0.2778, 0.09440, -1.0351 0.2393, 0.08960, -1.1101 0.2056, 0.08360, -1.2723 0.1633, 0.07610, -1.1887 0.1261, 0.06710, -1.3211 0.0900, 0.05640, -1.3907 0.0571, 0.04390, -1.5701 0.0283, 0.02940, -1.8134 0.0142, 0.01970, -2.0261 0.0081, 0.01410, -2.3490 0.0026, 0.00780, -2.1375 0.0000, 0.00000, -1.9271 0.0037, -0.00840, 0.6095 0.0112, -0.01420, 0.9898 0.0191, -0.01930, 1.0194 0.0397, -0.03030, 0.9308 0.0706, -0.04420, 0.6961 0.1037, -0.05710, 0.5106 0.1384, -0.06890, 0.4531 0.1741, -0.07950, 0.2852 0.2102, -0.08660, 0.0325 0.2472, -0.09640, -0.0699 0.2844, -0.10270, -0.2353 0.3225, -0.10690, -0.2664 0.3608, -0.10890, -0.4236 0.3991, -0.10830, -0.4299 0.4373, -0.10510, -0.4989 0.4757, -0.09890, -0.4289 0.5137, -0.09070, -0.3924 0.5694, -0.07640, -0.2658 15 Flap element taps 1.0000, 0.00130, 0.1704 0.9365, 0.01390, 0.1062 0.8333, 0.03280, -0.0101 0.7436, 0.04930, -0.0814 0.7049, 0.05670, -0.1073 0.6662, 0.06410, -0.1833 0.6522, 0.01390, -0.1656 0.5969, -0.00020, -0.1305 0.6000, -0.03020, -0.1380 0.6324, -0.04540, -0.1699 0.6667, -0.04880, -0.0092 0.7046, -0.04110, 0.0365 0.7429, -0.03210, 0.1003 0.8333, -0.01400, 0.2027 0.9311, -0.00120, 0.3041 Wake drag found for this condition, Cdw=0.0121 --------- Run Conditions: vel=106.0 ft/s Re=1.005x10^6 AOA=12.03 Flap deflection=-5.00 Totals: Cl=0.8872 Cdp=0.0307 Cm(c/4)=-0.0073 Cs=0.1549 Ch=-0.0996 Main component: Cl=0.7758 Cdp=0.0382 Cm=-0.1380 Flap component: Cl=0.1115 Cdp=-0.0075 Cm=-0.0878 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.0890 0.6175, -0.04610, -0.1780 0.5841, -0.02440, -0.1858 0.5775, 0.01750, -0.1891 0.5777, 0.04660, -0.2000 0.6274, 0.07170, -0.2675 0.5694, 0.08320, -0.2668 0.5112, 0.09370, -0.4734 0.4731, 0.09830, -0.6706 0.4349, 0.10070, -0.8384 0.3960, 0.10120, -1.0346 0.3566, 0.10020, -0.9779 0.3172, 0.09790, -1.0358 0.2778, 0.09440, -1.1097 0.2393, 0.08960, -1.2200 0.2056, 0.08360, -1.4357 0.1633, 0.07610, -1.3893 0.1261, 0.06710, -1.5775 0.0900, 0.05640, -1.6888 0.0571, 0.04390, -1.9909 0.0283, 0.02940, -2.4114 0.0142, 0.01970, -3.0381 0.0081, 0.01410, -3.6676 0.0026, 0.00780, -3.6513 0.0000, 0.00000, -3.9161 0.0037, -0.00840, 0.0071 0.0112, -0.01420, 0.8324 0.0191, -0.01930, 0.9979 0.0397, -0.03030, 1.0218 0.0706, -0.04420, 0.8326 0.1037, -0.05710, 0.6632 0.1384, -0.06890, 0.6237 0.1741, -0.07950, 0.4604 0.2102, -0.08660, 0.1900 0.2472, -0.09640, 0.0925 0.2844, -0.10270, -0.0877 0.3225, -0.10690, -0.1163 0.3608, -0.10890, -0.2909 0.3991, -0.10830, -0.3081 0.4373, -0.10510, -0.4064 0.4757, -0.09890, -0.3539 0.5137, -0.09070, -0.3381 0.5694, -0.07640, -0.2064 15 Flap element taps 1.0000, 0.00130, 0.0030 0.9365, 0.01390, -0.0885 0.8333, 0.03280, -0.1808 0.7436, 0.04930, -0.2248 0.7049, 0.05670, -0.2455 0.6662, 0.06410, -0.2773 0.6522, 0.01390, -0.2206 0.5969, -0.00020, -0.1806 0.6000, -0.03020, -0.1869 0.6324, -0.04540, -0.2225 0.6667, -0.04880, 0.1360 0.7046, -0.04110, 0.0497 0.7429, -0.03210, 0.1005 0.8333, -0.01400, 0.1821 0.9311, -0.00120, 0.2596 Wake drag found for this condition, Cdw=0.0236 --------- Run Conditions: vel=105.7 ft/s Re=1.003x10^6 AOA=15.00 Flap deflection=-5.00 Totals: Cl=0.9460 Cdp=0.0630 Cm(c/4)=-0.0176 Cs=0.1839 Ch=-0.1435 Main component: Cl=0.7963 Cdp=0.0507 Cm=-0.1292 Flap component: Cl=0.1497 Cdp=0.0123 Cm=-0.1209 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.1446 0.6175, -0.04610, -0.2292 0.5841, -0.02440, -0.2403 0.5775, 0.01750, -0.2444 0.5777, 0.04660, -0.2559 0.6274, 0.07170, -0.3564 0.5694, 0.08320, -0.3141 0.5112, 0.09370, -0.3682 0.4731, 0.09830, -0.4150 0.4349, 0.10070, -0.5429 0.3960, 0.10120, -0.7997 0.3566, 0.10020, -0.7742 0.3172, 0.09790, -0.8846 0.2778, 0.09440, -0.9957 0.2393, 0.08960, -1.1452 0.2056, 0.08360, -1.4139 0.1633, 0.07610, -1.3996 0.1261, 0.06710, -1.6491 0.0900, 0.05640, -1.8187 0.0571, 0.04390, -2.2290 0.0283, 0.02940, -2.8320 0.0142, 0.01970, -3.4738 0.0081, 0.01410, -4.7065 0.0026, 0.00780, -4.8766 0.0000, 0.00000, -5.5391 0.0037, -0.00840, -0.5697 0.0112, -0.01420, 0.6287 0.0191, -0.01930, 0.9209 0.0397, -0.03030, 1.0473 0.0706, -0.04420, 0.9022 0.1037, -0.05710, 0.7528 0.1384, -0.06890, 0.7321 0.1741, -0.07950, 0.5701 0.2102, -0.08660, 0.2853 0.2472, -0.09640, 0.1959 0.2844, -0.10270, 0.0037 0.3225, -0.10690, -0.0235 0.3608, -0.10890, -0.2150 0.3991, -0.10830, -0.2401 0.4373, -0.10510, -0.3616 0.4757, -0.09890, -0.3275 0.5137, -0.09070, -0.3343 0.5694, -0.07640, -0.1836 15 Flap element taps 1.0000, 0.00130, -0.2322 0.9365, 0.01390, -0.3494 0.8333, 0.03280, -0.3746 0.7436, 0.04930, -0.3677 0.7049, 0.05670, -0.3715 0.6662, 0.06410, -0.3872 0.6522, 0.01390, -0.2779 0.5969, -0.00020, -0.2360 0.6000, -0.03020, -0.2427 0.6324, -0.04540, -0.2820 0.6667, -0.04880, 0.1504 0.7046, -0.04110, 0.0232 0.7429, -0.03210, 0.0608 0.8333, -0.01400, 0.1158 0.9311, -0.00120, 0.1625 --------- Run Conditions: vel=105.7 ft/s Re=1.003x10^6 AOA=17.99 Flap deflection=-5.00 Totals: Cl=0.8657 Cdp=0.1204 Cm(c/4)=-0.0384 Cs=0.1528 Ch=-0.1713 Main component: Cl=0.6864 Cdp=0.0897 Cm=-0.1071 Flap component: Cl=0.1793 Cdp=0.0307 Cm=-0.1464 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.2046 0.6175, -0.04610, -0.3120 0.5841, -0.02440, -0.3242 0.5775, 0.01750, -0.3283 0.5777, 0.04660, -0.3394 0.6274, 0.07170, -0.5202 0.5694, 0.08320, -0.4591 0.5112, 0.09370, -0.4972 0.4731, 0.09830, -0.4809 0.4349, 0.10070, -0.4939 0.3960, 0.10120, -0.6384 0.3566, 0.10020, -0.4808 0.3172, 0.09790, -0.4906 0.2778, 0.09440, -0.5238 0.2393, 0.08960, -0.6566 0.2056, 0.08360, -0.9957 0.1633, 0.07610, -1.0462 0.1261, 0.06710, -1.3818 0.0900, 0.05640, -1.6047 0.0571, 0.04390, -2.0841 0.0283, 0.02940, -2.7739 0.0142, 0.01970, -3.4809 0.0081, 0.01410, -4.8123 0.0026, 0.00780, -5.2010 0.0000, 0.00000, -6.0142 0.0037, -0.00840, -0.7910 0.0112, -0.01420, 0.5372 0.0191, -0.01930, 0.8776 0.0397, -0.03030, 1.0523 0.0706, -0.04420, 0.9265 0.1037, -0.05710, 0.7858 0.1384, -0.06890, 0.7833 0.1741, -0.07950, 0.6193 0.2102, -0.08660, 0.3183 0.2472, -0.09640, 0.2330 0.2844, -0.10270, 0.0287 0.3225, -0.10690, 0.0032 0.3608, -0.10890, -0.2046 0.3991, -0.10830, -0.2346 0.4373, -0.10510, -0.3784 0.4757, -0.09890, -0.3522 0.5137, -0.09070, -0.3766 0.5694, -0.07640, -0.2183 15 Flap element taps 1.0000, 0.00130, -0.4547 0.9365, 0.01390, -0.5235 0.8333, 0.03280, -0.5536 0.7436, 0.04930, -0.5508 0.7049, 0.05670, -0.5468 0.6662, 0.06410, -0.5544 0.6522, 0.01390, -0.3669 0.5969, -0.00020, -0.3206 0.6000, -0.03020, -0.3283 0.6324, -0.04540, -0.3682 0.6667, -0.04880, 0.1489 0.7046, -0.04110, -0.0361 0.7429, -0.03210, -0.0040 0.8333, -0.01400, 0.0346 0.9311, -0.00120, 0.0564 --------- Run Conditions: vel=105.3 ft/s Re=0.999x10^6 AOA=19.98 Flap deflection=-5.00 Totals: Cl=0.5121 Cdp=0.2572 Cm(c/4)=-0.0716 Cs=-0.0668 Ch=-0.1641 Main component: Cl=0.3410 Cdp=0.2261 Cm=-0.0741 Flap component: Cl=0.1710 Cdp=0.0311 Cm=-0.1398 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.3639 0.6175, -0.04610, -0.4735 0.5841, -0.02440, -0.4887 0.5775, 0.01750, -0.4924 0.5777, 0.04660, -0.5056 0.6274, 0.07170, -0.6298 0.5694, 0.08320, -0.5845 0.5112, 0.09370, -0.6392 0.4731, 0.09830, -0.6396 0.4349, 0.10070, -0.6553 0.3960, 0.10120, -0.8178 0.3566, 0.10020, -0.6357 0.3172, 0.09790, -0.6363 0.2778, 0.09440, -0.6122 0.2393, 0.08960, -0.6294 0.2056, 0.08360, -0.7826 0.1633, 0.07610, -0.5842 0.1261, 0.06710, -0.6834 0.0900, 0.05640, -0.5922 0.0571, 0.04390, -0.6380 0.0283, 0.02940, -0.6515 0.0142, 0.01970, -0.6540 0.0081, 0.01410, -0.8008 0.0026, 0.00780, -0.6102 0.0000, 0.00000, -0.8810 0.0037, -0.00840, 0.6277 0.0112, -0.01420, 0.9687 0.0191, -0.01930, 1.0232 0.0397, -0.03030, 1.0006 0.0706, -0.04420, 0.7989 0.1037, -0.05710, 0.6306 0.1384, -0.06890, 0.6339 0.1741, -0.07950, 0.4569 0.2102, -0.08660, 0.1369 0.2472, -0.09640, 0.0492 0.2844, -0.10270, -0.1653 0.3225, -0.10690, -0.1857 0.3608, -0.10890, -0.4069 0.3991, -0.10830, -0.4327 0.4373, -0.10510, -0.5823 0.4757, -0.09890, -0.5479 0.5137, -0.09070, -0.5656 0.5694, -0.07640, -0.3899 15 Flap element taps 1.0000, 0.00130, -0.5630 0.9365, 0.01390, -0.6236 0.8333, 0.03280, -0.6687 0.7436, 0.04930, -0.6547 0.7049, 0.05670, -0.6539 0.6662, 0.06410, -0.6617 0.6522, 0.01390, -0.5334 0.5969, -0.00020, -0.4832 0.6000, -0.03020, -0.4930 0.6324, -0.04540, -0.5363 0.6667, -0.04880, -0.0319 0.7046, -0.04110, -0.1766 0.7429, -0.03210, -0.1412 0.8333, -0.01400, -0.0942 0.9311, -0.00120, -0.0611 --------- Run Conditions: vel=106.2 ft/s Re=1.007x10^6 AOA=23.97 Flap deflection=-5.00 Totals: Cl=0.6156 Cdp=0.3477 Cm(c/4)=-0.0949 Cs=-0.0676 Ch=-0.1854 Main component: Cl=0.4189 Cdp=0.2929 Cm=-0.1077 Flap component: Cl=0.1967 Cdp=0.0548 Cm=-0.1632 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.3377 0.6175, -0.04610, -0.4816 0.5841, -0.02440, -0.4978 0.5775, 0.01750, -0.5019 0.5777, 0.04660, -0.5119 0.6274, 0.07170, -0.7212 0.5694, 0.08320, -0.6710 0.5112, 0.09370, -0.7303 0.4731, 0.09830, -0.7272 0.4349, 0.10070, -0.7409 0.3960, 0.10120, -0.9149 0.3566, 0.10020, -0.7214 0.3172, 0.09790, -0.7182 0.2778, 0.09440, -0.6904 0.2393, 0.08960, -0.7027 0.2056, 0.08360, -0.8639 0.1633, 0.07610, -0.6493 0.1261, 0.06710, -0.7565 0.0900, 0.05640, -0.6570 0.0571, 0.04390, -0.7033 0.0283, 0.02940, -0.7055 0.0142, 0.01970, -0.7095 0.0081, 0.01410, -0.8642 0.0026, 0.00780, -0.6580 0.0000, 0.00000, -0.9038 0.0037, -0.00840, 0.4332 0.0112, -0.01420, 0.8866 0.0191, -0.01930, 0.9986 0.0397, -0.03030, 1.0379 0.0706, -0.04420, 0.8737 0.1037, -0.05710, 0.7266 0.1384, -0.06890, 0.7567 0.1741, -0.07950, 0.5897 0.2102, -0.08660, 0.2611 0.2472, -0.09640, 0.1863 0.2844, -0.10270, -0.0353 0.3225, -0.10690, -0.0485 0.3608, -0.10890, -0.2818 0.3991, -0.10830, -0.3122 0.4373, -0.10510, -0.4828 0.4757, -0.09890, -0.4648 0.5137, -0.09070, -0.5033 0.5694, -0.07640, -0.3362 15 Flap element taps 1.0000, 0.00130, -0.6498 0.9365, 0.01390, -0.7026 0.8333, 0.03280, -0.7533 0.7436, 0.04930, -0.7457 0.7049, 0.05670, -0.7481 0.6662, 0.06410, -0.7600 0.6522, 0.01390, -0.5464 0.5969, -0.00020, -0.4945 0.6000, -0.03020, -0.5033 0.6324, -0.04540, -0.5492 0.6667, -0.04880, 0.1724 0.7046, -0.04110, -0.1695 0.7429, -0.03210, -0.1401 0.8333, -0.01400, -0.1106 0.9311, -0.00120, -0.0891 --------- Run Conditions: vel=106.0 ft/s Re=1.008x10^6 AOA=27.01 Flap deflection=-5.00 Totals: Cl=0.7342 Cdp=0.4460 Cm(c/4)=-0.1218 Cs=-0.0639 Ch=-0.2166 Main component: Cl=0.5107 Cdp=0.3628 Cm=-0.1452 Flap component: Cl=0.2235 Cdp=0.0832 Cm=-0.1908 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.2979 0.6175, -0.04610, -0.4603 0.5841, -0.02440, -0.4779 0.5775, 0.01750, -0.4829 0.5777, 0.04660, -0.4959 0.6274, 0.07170, -0.8383 0.5694, 0.08320, -0.7820 0.5112, 0.09370, -0.8453 0.4731, 0.09830, -0.8392 0.4349, 0.10070, -0.8551 0.3960, 0.10120, -1.0382 0.3566, 0.10020, -0.8334 0.3172, 0.09790, -0.8276 0.2778, 0.09440, -0.7981 0.2393, 0.08960, -0.8153 0.2056, 0.08360, -0.9856 0.1633, 0.07610, -0.7596 0.1261, 0.06710, -0.8750 0.0900, 0.05640, -0.7668 0.0571, 0.04390, -0.8155 0.0283, 0.02940, -0.8136 0.0142, 0.01970, -0.8168 0.0081, 0.01410, -0.9789 0.0026, 0.00780, -0.7614 0.0000, 0.00000, -0.8182 0.0037, -0.00840, 0.2214 0.0112, -0.01420, 0.7867 0.0191, -0.01930, 0.9557 0.0397, -0.03030, 1.0553 0.0706, -0.04420, 0.9310 0.1037, -0.05710, 0.8059 0.1384, -0.06890, 0.8608 0.1741, -0.07950, 0.7019 0.2102, -0.08660, 0.3685 0.2472, -0.09640, 0.3079 0.2844, -0.10270, 0.0812 0.3225, -0.10690, 0.0767 0.3608, -0.10890, -0.1658 0.3991, -0.10830, -0.1977 0.4373, -0.10510, -0.3866 0.4757, -0.09890, -0.3838 0.5137, -0.09070, -0.4379 0.5694, -0.07640, -0.2815 15 Flap element taps 1.0000, 0.00130, -0.7608 0.9365, 0.01390, -0.8156 0.8333, 0.03280, -0.8585 0.7436, 0.04930, -0.8539 0.7049, 0.05670, -0.8575 0.6662, 0.06410, -0.8712 0.6522, 0.01390, -0.5313 0.5969, -0.00020, -0.4774 0.6000, -0.03020, -0.4852 0.6324, -0.04540, -0.5339 0.6667, -0.04880, 0.2645 0.7046, -0.04110, -0.1549 0.7429, -0.03210, -0.1307 0.8333, -0.01400, -0.1204 0.9311, -0.00120, -0.1156