SIKORSKY SC1095 AIRFOIL (sc1095-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: SIKORSKY SC1095 AIRFOIL (sc1095-il) Reynolds number: 1,000,000 Max Cl/Cd: 86.95 at α=9.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-sc1095-il-1000000.txt Download as CSV file: xf-sc1095-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: SIKORSKY SC1095 AIRFOIL
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
------ -------- --------- --------- -------- -------- --------
-15.000 -1.0592 0.09552 0.09313 0.0115 1.0000 0.0051
-14.750 -1.0997 0.08387 0.08138 0.0050 1.0000 0.0050
-14.500 -1.1398 0.07172 0.06911 -0.0020 1.0000 0.0050
-14.250 -1.1697 0.05929 0.05650 -0.0106 1.0000 0.0049
-14.000 -1.1881 0.04848 0.04546 -0.0210 1.0000 0.0048
-13.750 -1.2047 0.04178 0.03854 -0.0265 1.0000 0.0048
-13.500 -1.2174 0.03755 0.03413 -0.0280 1.0000 0.0048
-13.250 -1.2274 0.03457 0.03098 -0.0268 1.0000 0.0049
-13.000 -1.2316 0.03203 0.02825 -0.0249 1.0000 0.0049
-12.750 -1.2277 0.02970 0.02573 -0.0235 1.0000 0.0049
-12.500 -1.2184 0.02772 0.02359 -0.0224 1.0000 0.0050
-12.250 -1.2056 0.02599 0.02169 -0.0214 1.0000 0.0051
-12.000 -1.1901 0.02447 0.02002 -0.0205 1.0000 0.0051
-11.750 -1.1723 0.02312 0.01855 -0.0198 1.0000 0.0052
-11.500 -1.1530 0.02192 0.01722 -0.0191 1.0000 0.0053
-11.250 -1.1323 0.02084 0.01603 -0.0185 1.0000 0.0054
-11.000 -1.1106 0.01985 0.01493 -0.0180 1.0000 0.0055
-10.750 -1.0881 0.01894 0.01392 -0.0176 1.0000 0.0055
-10.500 -1.0649 0.01809 0.01297 -0.0172 1.0000 0.0056
-10.250 -1.0410 0.01730 0.01209 -0.0168 1.0000 0.0057
-10.000 -1.0167 0.01657 0.01127 -0.0165 1.0000 0.0058
-9.750 -0.9918 0.01589 0.01051 -0.0162 1.0000 0.0059
-9.500 -0.9665 0.01525 0.00979 -0.0159 1.0000 0.0061
-9.250 -0.9409 0.01466 0.00912 -0.0157 1.0000 0.0062
-9.000 -0.9149 0.01411 0.00851 -0.0155 1.0000 0.0064
-8.750 -0.8886 0.01361 0.00795 -0.0153 1.0000 0.0066
-8.500 -0.8622 0.01309 0.00737 -0.0152 1.0000 0.0069
-8.250 -0.8357 0.01257 0.00680 -0.0150 1.0000 0.0075
-8.000 -0.8090 0.01210 0.00629 -0.0148 1.0000 0.0083
-7.750 -0.7827 0.01152 0.00572 -0.0147 1.0000 0.0125
-7.500 -0.7563 0.01097 0.00527 -0.0146 1.0000 0.0239
-7.250 -0.7292 0.01063 0.00496 -0.0145 1.0000 0.0286
-7.000 -0.7016 0.01040 0.00472 -0.0145 1.0000 0.0312
-6.750 -0.6746 0.01006 0.00440 -0.0144 1.0000 0.0348
-6.500 -0.6478 0.00980 0.00414 -0.0142 1.0000 0.0379
-6.250 -0.6217 0.00951 0.00388 -0.0139 1.0000 0.0430
-6.000 -0.5969 0.00924 0.00366 -0.0133 1.0000 0.0502
-5.750 -0.5731 0.00904 0.00349 -0.0125 1.0000 0.0580
-5.500 -0.5459 0.00883 0.00334 -0.0125 0.9992 0.0665
-5.250 -0.5111 0.00866 0.00318 -0.0140 0.9969 0.0726
-5.000 -0.4757 0.00849 0.00305 -0.0156 0.9950 0.0788
-4.750 -0.4404 0.00837 0.00293 -0.0172 0.9925 0.0832
-4.500 -0.4069 0.00819 0.00280 -0.0184 0.9878 0.0899
-4.250 -0.3722 0.00808 0.00269 -0.0197 0.9819 0.0938
-4.000 -0.3442 0.00802 0.00259 -0.0195 0.9707 0.0963
-3.750 -0.3208 0.00788 0.00245 -0.0182 0.9579 0.1012
-3.500 -0.2950 0.00774 0.00233 -0.0175 0.9477 0.1055
-3.250 -0.2686 0.00765 0.00221 -0.0170 0.9383 0.1088
-3.000 -0.2427 0.00750 0.00207 -0.0163 0.9289 0.1152
-2.750 -0.2160 0.00737 0.00195 -0.0159 0.9183 0.1219
-2.500 -0.1889 0.00722 0.00183 -0.0155 0.9072 0.1334
-2.250 -0.1618 0.00706 0.00171 -0.0152 0.8961 0.1502
-2.000 -0.1347 0.00686 0.00160 -0.0149 0.8840 0.1810
-1.750 -0.1074 0.00663 0.00149 -0.0147 0.8694 0.2272
-1.500 -0.0802 0.00637 0.00139 -0.0145 0.8501 0.2845
-1.250 -0.0530 0.00612 0.00130 -0.0143 0.8268 0.3521
-1.000 -0.0255 0.00582 0.00121 -0.0143 0.8038 0.4351
-0.750 0.0019 0.00549 0.00115 -0.0143 0.7800 0.5360
-0.500 0.0296 0.00524 0.00111 -0.0142 0.7528 0.6270
-0.250 0.0573 0.00511 0.00110 -0.0140 0.7228 0.6934
0.000 0.0850 0.00508 0.00110 -0.0138 0.6848 0.7436
0.250 0.1126 0.00514 0.00112 -0.0136 0.6397 0.7820
0.500 0.1400 0.00526 0.00115 -0.0134 0.5862 0.8141
0.750 0.1669 0.00543 0.00120 -0.0131 0.5284 0.8446
1.000 0.1937 0.00564 0.00127 -0.0127 0.4729 0.8699
1.250 0.2202 0.00584 0.00134 -0.0123 0.4237 0.8896
1.500 0.2454 0.00600 0.00143 -0.0115 0.3864 0.9145
1.750 0.2689 0.00616 0.00151 -0.0103 0.3553 0.9369
2.000 0.2929 0.00632 0.00158 -0.0092 0.3283 0.9548
2.250 0.3166 0.00645 0.00163 -0.0081 0.3024 0.9718
2.500 0.3472 0.00660 0.00167 -0.0085 0.2745 0.9847
3.000 0.4196 0.00705 0.00186 -0.0122 0.2152 0.9973
3.250 0.4533 0.00731 0.00198 -0.0135 0.1872 1.0000
3.500 0.4779 0.00750 0.00208 -0.0129 0.1696 1.0000
3.750 0.5040 0.00770 0.00221 -0.0126 0.1550 1.0000
4.000 0.5311 0.00791 0.00235 -0.0125 0.1427 1.0000
4.250 0.5588 0.00809 0.00248 -0.0125 0.1333 1.0000
4.500 0.5867 0.00827 0.00264 -0.0125 0.1251 1.0000
4.750 0.6146 0.00850 0.00281 -0.0126 0.1162 1.0000
5.000 0.6428 0.00867 0.00297 -0.0127 0.1110 1.0000
5.250 0.6707 0.00891 0.00316 -0.0127 0.1044 1.0000
5.500 0.6988 0.00911 0.00337 -0.0128 0.0998 1.0000
5.750 0.7268 0.00931 0.00355 -0.0128 0.0957 1.0000
6.000 0.7546 0.00957 0.00378 -0.0129 0.0909 1.0000
6.250 0.7823 0.00983 0.00405 -0.0129 0.0875 1.0000
6.500 0.8103 0.00999 0.00423 -0.0129 0.0849 1.0000
6.750 0.8380 0.01021 0.00444 -0.0130 0.0813 1.0000
7.000 0.8653 0.01053 0.00474 -0.0129 0.0774 1.0000
7.250 0.8926 0.01081 0.00505 -0.0129 0.0751 1.0000
7.500 0.9204 0.01097 0.00524 -0.0129 0.0733 1.0000
7.750 0.9480 0.01117 0.00544 -0.0129 0.0702 1.0000
8.000 0.9750 0.01147 0.00571 -0.0129 0.0662 1.0000
8.250 1.0019 0.01175 0.00602 -0.0128 0.0633 1.0000
8.500 1.0294 0.01192 0.00621 -0.0128 0.0610 1.0000
8.750 1.0563 0.01218 0.00646 -0.0128 0.0577 1.0000
9.000 1.0826 0.01253 0.00680 -0.0127 0.0530 1.0000
9.250 1.1095 0.01276 0.00705 -0.0126 0.0493 1.0000
9.500 1.1349 0.01322 0.00743 -0.0124 0.0387 1.0000
9.750 1.1540 0.01473 0.00870 -0.0116 0.0127 1.0000
10.000 1.1776 0.01547 0.00948 -0.0111 0.0100 1.0000
10.250 1.2015 0.01612 0.01019 -0.0107 0.0090 1.0000
10.500 1.2241 0.01694 0.01109 -0.0101 0.0081 1.0000
10.750 1.2475 0.01759 0.01182 -0.0096 0.0078 1.0000
11.000 1.2705 0.01825 0.01256 -0.0091 0.0074 1.0000
11.250 1.2929 0.01897 0.01335 -0.0086 0.0071 1.0000
11.500 1.3144 0.01974 0.01420 -0.0079 0.0067 1.0000
11.750 1.3347 0.02064 0.01518 -0.0072 0.0064 1.0000
12.000 1.3528 0.02175 0.01640 -0.0062 0.0062 1.0000
12.250 1.3673 0.02319 0.01799 -0.0049 0.0059 1.0000
12.500 1.3815 0.02452 0.01945 -0.0036 0.0058 1.0000
12.750 1.3971 0.02559 0.02062 -0.0025 0.0058 1.0000
13.000 1.4107 0.02676 0.02190 -0.0012 0.0057 1.0000
13.250 1.4215 0.02804 0.02330 0.0004 0.0056 1.0000
13.500 1.4266 0.02942 0.02480 0.0027 0.0056 1.0000
13.750 1.4280 0.03105 0.02654 0.0049 0.0055 1.0000
14.000 1.4277 0.03301 0.02863 0.0066 0.0054 1.0000
14.250 1.4252 0.03544 0.03119 0.0075 0.0054 1.0000
14.500 1.4204 0.03847 0.03437 0.0076 0.0054 1.0000
14.750 1.4129 0.04233 0.03837 0.0065 0.0053 1.0000
15.000 1.4011 0.04747 0.04368 0.0039 0.0053 1.0000
15.250 1.3833 0.05460 0.05099 -0.0009 0.0053 1.0000
15.500 1.3564 0.06430 0.06090 -0.0075 0.0053 1.0000
15.750 1.3188 0.07597 0.07278 -0.0145 0.0054 1.0000
16.000 1.2745 0.08823 0.08522 -0.0210 0.0055 1.0000
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