S809 VENTED AILERON MODEL, 18 IN CHORD --------- Run Conditions: vel=114.4 ft/s Re=1.004x10^6 AOA=-6.02 Flap deflection=-20.00 Totals: Cl=-0.7828 Cdp=0.0855 Cm(c/4)=0.1292 Cs=-0.0029 Ch=-0.0124 Main component: Cl=-0.5005 Cdp=0.0936 Cm=0.1030 Flap component: Cl=-0.2822 Cdp=-0.0082 Cm=0.2230 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.7959 0.5871, 0.07930, -0.2466 0.5501, 0.08690, -0.2046 0.5112, 0.09370, -0.3050 0.4731, 0.09830, -0.3468 0.4349, 0.10070, -0.3181 0.3960, 0.10120, -0.2616 0.3566, 0.10020, -0.2062 0.3172, 0.09790, -0.1465 0.2778, 0.09440, -0.0899 0.2393, 0.08960, -0.0351 0.2056, 0.08360, 0.0422 0.1633, 0.07610, 0.1376 0.1261, 0.06710, 0.2648 0.0900, 0.05640, 0.3957 0.0571, 0.04390, 0.6056 0.0283, 0.02940, 0.8707 0.0142, 0.01970, 0.9985 0.0081, 0.01410, 0.9926 0.0026, 0.00780, 0.6561 0.0000, 0.00000, -0.9244 0.0037, -0.00840, -1.7209 0.0112, -0.01420, -1.7769 0.0191, -0.01930, -1.1570 0.0397, -0.03030, -0.9867 0.0706, -0.04420, -0.9211 0.1037, -0.05710, -0.8975 0.1384, -0.06890, -0.9480 0.1741, -0.07950, -0.9822 0.2102, -0.08660, -1.0414 0.2472, -0.09640, -1.1007 0.2844, -0.10270, -1.0954 0.3225, -0.10690, -1.0755 0.3608, -0.10890, -1.0142 0.3991, -0.10830, -0.8688 0.4373, -0.10510, -0.6419 0.4757, -0.09890, -0.3808 0.5137, -0.09070, -0.2804 0.5514, -0.08120, -0.2744 0.5917, -0.06870, -0.2891 0.5917, -0.02380, -0.6694 0.5917, 0.02120, -0.7974 16 Flap element taps 1.0000, 0.00130, -0.3235 0.9365, 0.01390, 0.1139 0.8333, 0.03280, 0.4506 0.7436, 0.04930, 0.8540 0.7049, 0.05670, 0.9313 0.6667, 0.05450, -0.8380 0.6302, 0.03770, -1.1856 0.6083, 0.01980, -1.2175 0.6000, 0.00000, -1.6257 0.6076, -0.01900, -1.7916 0.6285, -0.03060, -1.1228 0.6667, -0.04090, -0.7143 0.7046, -0.04120, -0.4264 0.7429, -0.03210, -0.3714 0.8333, -0.01400, -0.3610 0.9311, -0.00120, -0.3654 --------- Run Conditions: vel=114.5 ft/s Re=1.002x10^6 AOA=0.00 Flap deflection=-20.00 Totals: Cl=-0.3938 Cdp=0.0599 Cm(c/4)=0.1444 Cs=-0.0599 Ch=-0.0412 Main component: Cl=-0.1098 Cdp=0.0488 Cm=0.0205 Flap component: Cl=-0.2840 Cdp=0.0111 Cm=0.2223 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.4424 0.5871, 0.07930, -0.2555 0.5501, 0.08690, -0.2801 0.5112, 0.09370, -0.4167 0.4731, 0.09830, -0.5000 0.4349, 0.10070, -0.5038 0.3960, 0.10120, -0.4783 0.3566, 0.10020, -0.4452 0.3172, 0.09790, -0.4075 0.2778, 0.09440, -0.3852 0.2393, 0.08960, -0.3638 0.2056, 0.08360, -0.3267 0.1633, 0.07610, -0.2648 0.1261, 0.06710, -0.1770 0.0900, 0.05640, -0.1119 0.0571, 0.04390, 0.0481 0.0283, 0.02940, 0.3170 0.0142, 0.01970, 0.5420 0.0081, 0.01410, 0.7163 0.0026, 0.00780, 0.8456 0.0000, 0.00000, 0.9369 0.0037, -0.00840, 0.3349 0.0112, -0.01420, -0.0842 0.0191, -0.01930, 0.0593 0.0397, -0.03030, -0.0816 0.0706, -0.04420, -0.2161 0.1037, -0.05710, -0.3041 0.1384, -0.06890, -0.4322 0.1741, -0.07950, -0.5270 0.2102, -0.08660, -0.6390 0.2472, -0.09640, -0.7467 0.2844, -0.10270, -0.7957 0.3225, -0.10690, -0.8293 0.3608, -0.10890, -0.8349 0.3991, -0.10830, -0.7663 0.4373, -0.10510, -0.6162 0.4757, -0.09890, -0.3559 0.5137, -0.09070, -0.1261 0.5514, -0.08120, -0.0706 0.5917, -0.06870, -0.0605 0.5917, -0.02380, -0.3550 0.5917, 0.02120, -0.4459 16 Flap element taps 1.0000, 0.00130, -0.2731 0.9365, 0.01390, 0.1042 0.8333, 0.03280, 0.4195 0.7436, 0.04930, 0.8693 0.7049, 0.05670, 0.6265 0.6667, 0.05450, -0.6676 0.6302, 0.03770, -0.6460 0.6083, 0.01980, -0.5955 0.6000, 0.00000, -0.8077 0.6076, -0.01900, -1.4371 0.6285, -0.03060, -1.1624 0.6667, -0.04090, -0.8368 0.7046, -0.04120, -0.4825 0.7429, -0.03210, -0.4013 0.8333, -0.01400, -0.3670 0.9311, -0.00120, -0.3429 --------- Run Conditions: vel=115.0 ft/s Re=1.005x10^6 AOA=3.03 Flap deflection=-20.00 Totals: Cl=-0.1456 Cdp=0.0338 Cm(c/4)=0.1098 Cs=-0.0415 Ch=-0.0350 Main component: Cl=0.0469 Cdp=-0.0069 Cm=-0.0023 Flap component: Cl=-0.1925 Cdp=0.0407 Cm=0.1480 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, 0.0383 0.5871, 0.07930, -0.0492 0.5501, 0.08690, -0.1703 0.5112, 0.09370, -0.3520 0.4731, 0.09830, -0.4859 0.4349, 0.10070, -0.5296 0.3960, 0.10120, -0.5345 0.3566, 0.10020, -0.5298 0.3172, 0.09790, -0.5159 0.2778, 0.09440, -0.5181 0.2393, 0.08960, -0.5213 0.2056, 0.08360, -0.5079 0.1633, 0.07610, -0.4750 0.1261, 0.06710, -0.4223 0.0900, 0.05640, -0.4073 0.0571, 0.04390, -0.3061 0.0283, 0.02940, -0.1001 0.0142, 0.01970, 0.0796 0.0081, 0.01410, 0.2088 0.0026, 0.00780, 0.4778 0.0000, 0.00000, 0.9710 0.0037, -0.00840, 0.8300 0.0112, -0.01420, 0.4925 0.0191, -0.01930, 0.4731 0.0397, -0.03030, 0.2695 0.0706, -0.04420, 0.0759 0.1037, -0.05710, -0.0486 0.1384, -0.06890, -0.2036 0.1741, -0.07950, -0.3240 0.2102, -0.08660, -0.4546 0.2472, -0.09640, -0.5836 0.2844, -0.10270, -0.6588 0.3225, -0.10690, -0.7228 0.3608, -0.10890, -0.7598 0.3991, -0.10830, -0.7360 0.4373, -0.10510, -0.6384 0.4757, -0.09890, -0.4293 0.5137, -0.09070, -0.1853 0.5514, -0.08120, -0.0179 0.5917, -0.06870, 0.0284 0.5917, -0.02380, 0.0296 0.5917, 0.02120, 0.0424 16 Flap element taps 1.0000, 0.00130, -0.2612 0.9365, 0.01390, 0.1336 0.8333, 0.03280, 0.3352 0.7436, 0.04930, 0.0146 0.7049, 0.05670, 0.0219 0.6667, 0.05450, 0.0236 0.6302, 0.03770, 0.0283 0.6083, 0.01980, 0.0200 0.6000, 0.00000, -0.0298 0.6076, -0.01900, -0.6775 0.6285, -0.03060, -0.9215 0.6667, -0.04090, -0.6605 0.7046, -0.04120, -0.3130 0.7429, -0.03210, -0.2900 0.8333, -0.01400, -0.3042 0.9311, -0.00120, -0.3212 --------- Run Conditions: vel=115.0 ft/s Re=1.006x10^6 AOA=6.04 Flap deflection=-20.00 Totals: Cl=-0.0716 Cdp=0.0274 Cm(c/4)=0.1234 Cs=-0.0348 Ch=-0.0731 Main component: Cl=0.1283 Cdp=-0.0086 Cm=-0.0054 Flap component: Cl=-0.1999 Cdp=0.0360 Cm=0.1460 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, 0.0706 0.5871, 0.07930, 0.0126 0.5501, 0.08690, -0.1054 0.5112, 0.09370, -0.2892 0.4731, 0.09830, -0.4440 0.4349, 0.10070, -0.5127 0.3960, 0.10120, -0.5357 0.3566, 0.10020, -0.5588 0.3172, 0.09790, -0.5665 0.2778, 0.09440, -0.5897 0.2393, 0.08960, -0.6132 0.2056, 0.08360, -0.6186 0.1633, 0.07610, -0.6206 0.1261, 0.06710, -0.5947 0.0900, 0.05640, -0.6303 0.0571, 0.04390, -0.5942 0.0283, 0.02940, -0.4650 0.0142, 0.01970, -0.3594 0.0081, 0.01410, -0.3131 0.0026, 0.00780, 0.0448 0.0000, 0.00000, 0.6299 0.0037, -0.00840, 0.9858 0.0112, -0.01420, 0.7752 0.0191, -0.01930, 0.7072 0.0397, -0.03030, 0.4837 0.0706, -0.04420, 0.2628 0.1037, -0.05710, 0.1152 0.1384, -0.06890, -0.0646 0.1741, -0.07950, -0.2037 0.2102, -0.08660, -0.3463 0.2472, -0.09640, -0.4930 0.2844, -0.10270, -0.5888 0.3225, -0.10690, -0.6838 0.3608, -0.10890, -0.7470 0.3991, -0.10830, -0.7602 0.4373, -0.10510, -0.6969 0.4757, -0.09890, -0.5280 0.5137, -0.09070, -0.3188 0.5514, -0.08120, -0.0813 0.5917, -0.06870, 0.0441 0.5917, -0.02380, 0.0464 0.5917, 0.02120, 0.0550 16 Flap element taps 1.0000, 0.00130, -0.1568 0.9365, 0.01390, 0.1182 0.8333, 0.03280, 0.0985 0.7436, 0.04930, 0.0655 0.7049, 0.05670, 0.0723 0.6667, 0.05450, 0.0577 0.6302, 0.03770, 0.0472 0.6083, 0.01980, 0.0192 0.6000, 0.00000, 0.2375 0.6076, -0.01900, -0.6919 0.6285, -0.03060, -1.1631 0.6667, -0.04090, -1.0623 0.7046, -0.04120, -0.5080 0.7429, -0.03210, -0.2950 0.8333, -0.01400, -0.2933 0.9311, -0.00120, -0.2575 --------- Run Conditions: vel=115.3 ft/s Re=1.007x10^6 AOA=9.03 Flap deflection=-20.00 Totals: Cl=-0.0946 Cdp=0.0165 Cm(c/4)=0.1582 Cs=-0.0312 Ch=-0.1586 Main component: Cl=0.1635 Cdp=-0.0104 Cm=0.0038 Flap component: Cl=-0.2580 Cdp=0.0270 Cm=0.1771 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, 0.0715 0.5871, 0.07930, 0.0572 0.5501, 0.08690, -0.0006 0.5112, 0.09370, -0.1373 0.4731, 0.09830, -0.3164 0.4349, 0.10070, -0.4181 0.3960, 0.10120, -0.4656 0.3566, 0.10020, -0.5251 0.3172, 0.09790, -0.5561 0.2778, 0.09440, -0.6039 0.2393, 0.08960, -0.6496 0.2056, 0.08360, -0.6717 0.1633, 0.07610, -0.7127 0.1261, 0.06710, -0.7159 0.0900, 0.05640, -0.7998 0.0571, 0.04390, -0.8225 0.0283, 0.02940, -0.7842 0.0142, 0.01970, -0.7761 0.0081, 0.01410, -0.7910 0.0026, 0.00780, -0.4045 0.0000, 0.00000, 0.0805 0.0037, -0.00840, 0.9972 0.0112, -0.01420, 0.9303 0.0191, -0.01930, 0.8518 0.0397, -0.03030, 0.6331 0.0706, -0.04420, 0.4038 0.1037, -0.05710, 0.2428 0.1384, -0.06890, 0.0427 0.1741, -0.07950, -0.1137 0.2102, -0.08660, -0.2645 0.2472, -0.09640, -0.4334 0.2844, -0.10270, -0.5432 0.3225, -0.10690, -0.6663 0.3608, -0.10890, -0.7472 0.3991, -0.10830, -0.7924 0.4373, -0.10510, -0.7533 0.4757, -0.09890, -0.6083 0.5137, -0.09070, -0.4236 0.5514, -0.08120, -0.1533 0.5917, -0.06870, 0.0430 0.5917, -0.02380, 0.0430 0.5917, 0.02120, 0.0512 16 Flap element taps 1.0000, 0.00130, 0.1270 0.9365, 0.01390, 0.1295 0.8333, 0.03280, 0.0751 0.7436, 0.04930, 0.0682 0.7049, 0.05670, 0.0749 0.6667, 0.05450, 0.0496 0.6302, 0.03770, 0.0381 0.6083, 0.01980, 0.0032 0.6000, 0.00000, 0.3768 0.6076, -0.01900, -1.0383 0.6285, -0.03060, -1.5623 0.6667, -0.04090, -1.7012 0.7046, -0.04120, -1.5272 0.7429, -0.03210, -0.5260 0.8333, -0.01400, -0.1746 0.9311, -0.00120, 0.0457 --------- Run Conditions: vel=115.3 ft/s Re=1.006x10^6 AOA=12.02 Flap deflection=-20.00 Totals: Cl=0.0975 Cdp=0.0270 Cm(c/4)=0.1585 Cs=-0.0061 Ch=-0.1336 Main component: Cl=0.3255 Cdp=0.0117 Cm=-0.0231 Flap component: Cl=-0.2280 Cdp=0.0154 Cm=0.1563 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.0396 0.5871, 0.07930, -0.0448 0.5501, 0.08690, -0.0635 0.5112, 0.09370, -0.1228 0.4731, 0.09830, -0.2648 0.4349, 0.10070, -0.3963 0.3960, 0.10120, -0.4716 0.3566, 0.10020, -0.5702 0.3172, 0.09790, -0.6319 0.2778, 0.09440, -0.7077 0.2393, 0.08960, -0.7821 0.2056, 0.08360, -0.8311 0.1633, 0.07610, -0.9199 0.1261, 0.06710, -0.9670 0.0900, 0.05640, -1.1262 0.0571, 0.04390, -1.2521 0.0283, 0.02940, -1.3776 0.0142, 0.01970, -1.5738 0.0081, 0.01410, -1.6452 0.0026, 0.00780, -1.3852 0.0000, 0.00000, -1.3184 0.0037, -0.00840, 0.7724 0.0112, -0.01420, 1.0069 0.0191, -0.01930, 0.9875 0.0397, -0.03030, 0.8296 0.0706, -0.04420, 0.6170 0.1037, -0.05710, 0.4519 0.1384, -0.06890, 0.2463 0.1741, -0.07950, 0.0842 0.2102, -0.08660, -0.0647 0.2472, -0.09640, -0.2484 0.2844, -0.10270, -0.3714 0.3225, -0.10690, -0.5201 0.3608, -0.10890, -0.6189 0.3991, -0.10830, -0.7001 0.4373, -0.10510, -0.6829 0.4757, -0.09890, -0.5725 0.5137, -0.09070, -0.4405 0.5514, -0.08120, -0.2015 0.5917, -0.06870, -0.0483 0.5917, -0.02380, -0.0536 0.5917, 0.02120, -0.0530 16 Flap element taps 1.0000, 0.00130, 0.1292 0.9365, 0.01390, 0.1257 0.8333, 0.03280, 0.1197 0.7436, 0.04930, 0.0699 0.7049, 0.05670, -0.0990 0.6667, 0.05450, -0.1623 0.6302, 0.03770, -0.1537 0.6083, 0.01980, -0.2929 0.6000, 0.00000, 0.9990 0.6076, -0.01900, -1.0030 0.6285, -0.03060, -1.4085 0.6667, -0.04090, -1.5158 0.7046, -0.04120, -1.3357 0.7429, -0.03210, -0.8570 0.8333, -0.01400, -0.1116 0.9311, -0.00120, 0.1188 --------- Run Conditions: vel=114.8 ft/s Re=1.003x10^6 AOA=15.03 Flap deflection=-20.00 Totals: Cl=0.7791 Cdp=0.0826 Cm(c/4)=0.0552 Cs=0.1222 Ch=0.0448 Main component: Cl=0.7621 Cdp=0.0831 Cm=-0.1323 Flap component: Cl=0.0170 Cdp=-0.0005 Cm=-0.0060 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.3611 0.5871, 0.07930, -0.3803 0.5501, 0.08690, -0.3838 0.5112, 0.09370, -0.3946 0.4731, 0.09830, -0.4585 0.4349, 0.10070, -0.5639 0.3960, 0.10120, -0.6686 0.3566, 0.10020, -0.8037 0.3172, 0.09790, -0.9054 0.2778, 0.09440, -1.0229 0.2393, 0.08960, -1.1407 0.2056, 0.08360, -1.2411 0.1633, 0.07610, -1.3938 0.1261, 0.06710, -1.5250 0.0900, 0.05640, -1.8076 0.0571, 0.04390, -2.1432 0.0283, 0.02940, -2.6185 0.0142, 0.01970, -3.2652 0.0081, 0.01410, -3.7446 0.0026, 0.00780, -3.7174 0.0000, 0.00000, -5.1548 0.0037, -0.00840, -0.3629 0.0112, -0.01420, 0.7122 0.0191, -0.01930, 0.9510 0.0397, -0.03030, 1.0050 0.0706, -0.04420, 0.8847 0.1037, -0.05710, 0.7549 0.1384, -0.06890, 0.5822 0.1741, -0.07950, 0.4427 0.2102, -0.08660, 0.3083 0.2472, -0.09640, 0.1446 0.2844, -0.10270, 0.0323 0.3225, -0.10690, -0.1008 0.3608, -0.10890, -0.1950 0.3991, -0.10830, -0.2725 0.4373, -0.10510, -0.2657 0.4757, -0.09890, -0.1983 0.5137, -0.09070, -0.1465 0.5514, -0.08120, -0.0817 0.5917, -0.06870, -0.3779 0.5917, -0.02380, -0.3873 0.5917, 0.02120, -0.3725 16 Flap element taps 1.0000, 0.00130, -0.2864 0.9365, 0.01390, -0.1178 0.8333, 0.03280, -0.1111 0.7436, 0.04930, -0.2362 0.7049, 0.05670, -0.5749 0.6667, 0.05450, -0.6258 0.6302, 0.03770, -0.6199 0.6083, 0.01980, -0.7856 0.6000, 0.00000, 0.9540 0.6076, -0.01900, -0.0575 0.6285, -0.03060, -0.3990 0.6667, -0.04090, -0.2573 0.7046, -0.04120, -0.2669 0.7429, -0.03210, -0.2446 0.8333, -0.01400, -0.2527 0.9311, -0.00120, -0.2509 --------- Run Conditions: vel=114.3 ft/s Re=0.996x10^6 AOA=18.01 Flap deflection=-20.00 Totals: Cl=0.6244 Cdp=0.1466 Cm(c/4)=0.0354 Cs=0.0537 Ch=0.0476 Main component: Cl=0.5841 Cdp=0.1409 Cm=-0.0997 Flap component: Cl=0.0403 Cdp=0.0057 Cm=-0.0247 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.5435 0.5871, 0.07930, -0.5407 0.5501, 0.08690, -0.5553 0.5112, 0.09370, -0.5548 0.4731, 0.09830, -0.5565 0.4349, 0.10070, -0.5529 0.3960, 0.10120, -0.5410 0.3566, 0.10020, -0.5538 0.3172, 0.09790, -0.5686 0.2778, 0.09440, -0.5956 0.2393, 0.08960, -0.6408 0.2056, 0.08360, -0.7195 0.1633, 0.07610, -0.8838 0.1261, 0.06710, -1.0711 0.0900, 0.05640, -1.3726 0.0571, 0.04390, -1.7709 0.0283, 0.02940, -2.3048 0.0142, 0.01970, -2.9727 0.0081, 0.01410, -3.4839 0.0026, 0.00780, -3.5137 0.0000, 0.00000, -4.9719 0.0037, -0.00840, -0.3654 0.0112, -0.01420, 0.7048 0.0191, -0.01930, 0.9481 0.0397, -0.03030, 1.0109 0.0706, -0.04420, 0.8938 0.1037, -0.05710, 0.7653 0.1384, -0.06890, 0.6010 0.1741, -0.07950, 0.4561 0.2102, -0.08660, 0.3062 0.2472, -0.09640, 0.1407 0.2844, -0.10270, 0.0129 0.3225, -0.10690, -0.1241 0.3608, -0.10890, -0.2368 0.3991, -0.10830, -0.3261 0.4373, -0.10510, -0.3360 0.4757, -0.09890, -0.2757 0.5137, -0.09070, -0.2137 0.5514, -0.08120, -0.2144 0.5917, -0.06870, -0.5338 0.5917, -0.02380, -0.5474 0.5917, 0.02120, -0.5424 16 Flap element taps 1.0000, 0.00130, -0.3896 0.9365, 0.01390, -0.2862 0.8333, 0.03280, -0.3804 0.7436, 0.04930, -0.5412 0.7049, 0.05670, -0.8449 0.6667, 0.05450, -0.8323 0.6302, 0.03770, -0.8095 0.6083, 0.01980, -0.9861 0.6000, 0.00000, 0.9524 0.6076, -0.01900, -0.1731 0.6285, -0.03060, -0.5800 0.6667, -0.04090, -0.4489 0.7046, -0.04120, -0.4516 0.7429, -0.03210, -0.4356 0.8333, -0.01400, -0.4327 0.9311, -0.00120, -0.3998 --------- Run Conditions: vel=114.7 ft/s Re=1.000x10^6 AOA=20.02 Flap deflection=-20.00 Totals: Cl=0.3216 Cdp=0.1477 Cm(c/4)=0.1081 Cs=-0.0287 Ch=-0.0317 Main component: Cl=0.4385 Cdp=0.1398 Cm=-0.0618 Flap component: Cl=-0.1170 Cdp=0.0079 Cm=0.0818 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.4925 0.5871, 0.07930, -0.4843 0.5501, 0.08690, -0.4965 0.5112, 0.09370, -0.5011 0.4731, 0.09830, -0.4972 0.4349, 0.10070, -0.4909 0.3960, 0.10120, -0.4895 0.3566, 0.10020, -0.4811 0.3172, 0.09790, -0.4857 0.2778, 0.09440, -0.5015 0.2393, 0.08960, -0.5240 0.2056, 0.08360, -0.5737 0.1633, 0.07610, -0.6772 0.1261, 0.06710, -0.8271 0.0900, 0.05640, -1.0823 0.0571, 0.04390, -1.4515 0.0283, 0.02940, -1.9591 0.0142, 0.01970, -2.5659 0.0081, 0.01410, -3.0210 0.0026, 0.00780, -3.0466 0.0000, 0.00000, -4.2549 0.0037, -0.00840, -0.1486 0.0112, -0.01420, 0.7747 0.0191, -0.01930, 0.9757 0.0397, -0.03030, 1.0064 0.0706, -0.04420, 0.8682 0.1037, -0.05710, 0.7283 0.1384, -0.06890, 0.5634 0.1741, -0.07950, 0.4048 0.2102, -0.08660, 0.2340 0.2472, -0.09640, 0.0553 0.2844, -0.10270, -0.0928 0.3225, -0.10690, -0.2412 0.3608, -0.10890, -0.3817 0.3991, -0.10830, -0.4862 0.4373, -0.10510, -0.5168 0.4757, -0.09890, -0.4590 0.5137, -0.09070, -0.3851 0.5514, -0.08120, -0.3724 0.5917, -0.06870, -0.4757 0.5917, -0.02380, -0.4963 0.5917, 0.02120, -0.4922 16 Flap element taps 1.0000, 0.00130, -0.2724 0.9365, 0.01390, -0.2570 0.8333, 0.03280, -0.3562 0.7436, 0.04930, -0.4893 0.7049, 0.05670, -0.7399 0.6667, 0.05450, -0.7434 0.6302, 0.03770, -0.7294 0.6083, 0.01980, -0.8916 0.6000, 0.00000, 0.9893 0.6076, -0.01900, -0.6303 0.6285, -0.03060, -1.1415 0.6667, -0.04090, -1.1573 0.7046, -0.04120, -1.0690 0.7429, -0.03210, -1.0581 0.8333, -0.01400, -0.7673 0.9311, -0.00120, -0.3154 --------- Run Conditions: vel=115.0 ft/s Re=1.001x10^6 AOA=23.98 Flap deflection=-20.00 Totals: Cl=0.3075 Cdp=0.2334 Cm(c/4)=0.0601 Cs=-0.0883 Ch=-0.0899 Main component: Cl=0.3889 Cdp=0.2366 Cm=-0.0807 Flap component: Cl=-0.0814 Cdp=-0.0033 Cm=0.0469 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.6177 0.5871, 0.07930, -0.5869 0.5501, 0.08690, -0.6136 0.5112, 0.09370, -0.6291 0.4731, 0.09830, -0.6424 0.4349, 0.10070, -0.6544 0.3960, 0.10120, -0.6504 0.3566, 0.10020, -0.6384 0.3172, 0.09790, -0.6448 0.2778, 0.09440, -0.6540 0.2393, 0.08960, -0.6679 0.2056, 0.08360, -0.6781 0.1633, 0.07610, -0.6923 0.1261, 0.06710, -0.7158 0.0900, 0.05640, -0.7260 0.0571, 0.04390, -0.7678 0.0283, 0.02940, -0.9803 0.0142, 0.01970, -1.4116 0.0081, 0.01410, -1.8442 0.0026, 0.00780, -2.1103 0.0000, 0.00000, -3.3564 0.0037, -0.00840, -0.0652 0.0112, -0.01420, 0.7700 0.0191, -0.01930, 0.9621 0.0397, -0.03030, 1.0098 0.0706, -0.04420, 0.9007 0.1037, -0.05710, 0.7727 0.1384, -0.06890, 0.6120 0.1741, -0.07950, 0.4712 0.2102, -0.08660, 0.3007 0.2472, -0.09640, 0.1224 0.2844, -0.10270, -0.0366 0.3225, -0.10690, -0.1941 0.3608, -0.10890, -0.3490 0.3991, -0.10830, -0.4601 0.4373, -0.10510, -0.5117 0.4757, -0.09890, -0.4838 0.5137, -0.09070, -0.4132 0.5514, -0.08120, -0.3854 0.5917, -0.06870, -0.5700 0.5917, -0.02380, -0.6028 0.5917, 0.02120, -0.5970 16 Flap element taps 1.0000, 0.00130, -0.4052 0.9365, 0.01390, -0.4471 0.8333, 0.03280, -0.5410 0.7436, 0.04930, -0.6269 0.7049, 0.05670, -0.8774 0.6667, 0.05450, -0.8574 0.6302, 0.03770, -0.8461 0.6083, 0.01980, -0.9945 0.6000, 0.00000, 0.9910 0.6076, -0.01900, -0.7903 0.6285, -0.03060, -1.4023 0.6667, -0.04090, -1.7651 0.7046, -0.04120, -1.5221 0.7429, -0.03210, -1.3435 0.8333, -0.01400, -0.3609 0.9311, -0.00120, -0.2029 --------- Run Conditions: vel=114.0 ft/s Re=0.992x10^6 AOA=26.96 Flap deflection=-20.00 Totals: Cl=0.3131 Cdp=0.2965 Cm(c/4)=0.0426 Cs=-0.1223 Ch=-0.0863 Main component: Cl=0.3700 Cdp=0.2996 Cm=-0.0892 Flap component: Cl=-0.0569 Cdp=-0.0031 Cm=0.0285 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.6960 0.5871, 0.07930, -0.6090 0.5501, 0.08690, -0.6217 0.5112, 0.09370, -0.6315 0.4731, 0.09830, -0.6409 0.4349, 0.10070, -0.6462 0.3960, 0.10120, -0.6673 0.3566, 0.10020, -0.6481 0.3172, 0.09790, -0.6507 0.2778, 0.09440, -0.6682 0.2393, 0.08960, -0.6859 0.2056, 0.08360, -0.6956 0.1633, 0.07610, -0.6923 0.1261, 0.06710, -0.7149 0.0900, 0.05640, -0.7229 0.0571, 0.04390, -0.7605 0.0283, 0.02940, -0.8157 0.0142, 0.01970, -0.9194 0.0081, 0.01410, -1.0229 0.0026, 0.00780, -1.0687 0.0000, 0.00000, -2.2194 0.0037, -0.00840, 0.0616 0.0112, -0.01420, 0.7661 0.0191, -0.01930, 0.9536 0.0397, -0.03030, 1.0170 0.0706, -0.04420, 0.9219 0.1037, -0.05710, 0.8127 0.1384, -0.06890, 0.6825 0.1741, -0.07950, 0.5362 0.2102, -0.08660, 0.3637 0.2472, -0.09640, 0.1967 0.2844, -0.10270, 0.0390 0.3225, -0.10690, -0.1111 0.3608, -0.10890, -0.2725 0.3991, -0.10830, -0.3992 0.4373, -0.10510, -0.4676 0.4757, -0.09890, -0.4452 0.5137, -0.09070, -0.3836 0.5514, -0.08120, -0.3479 0.5917, -0.06870, -0.6408 0.5917, -0.02380, -0.6641 0.5917, 0.02120, -0.6673 16 Flap element taps 1.0000, 0.00130, -0.5189 0.9365, 0.01390, -0.5415 0.8333, 0.03280, -0.6332 0.7436, 0.04930, -0.6861 0.7049, 0.05670, -0.9407 0.6667, 0.05450, -0.9490 0.6302, 0.03770, -0.9352 0.6083, 0.01980, -1.0979 0.6000, 0.00000, 0.9851 0.6076, -0.01900, -0.7494 0.6285, -0.03060, -1.3906 0.6667, -0.04090, -1.8047 0.7046, -0.04120, -1.5744 0.7429, -0.03210, -1.3387 0.8333, -0.01400, -0.3587 0.9311, -0.00120, -0.2471