SIKORSKY SC1095 AIRFOIL (sc1095-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: SIKORSKY SC1095 AIRFOIL (sc1095-il) Reynolds number: 500,000 Max Cl/Cd: 70.18 at α=8.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-sc1095-il-500000-n5.txt Download as CSV file: xf-sc1095-il-500000-n5.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 = 0.500 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-14.250 -0.9868 0.09701 0.09401 0.0120 1.0000 0.0047
-14.000 -1.0529 0.08036 0.07725 0.0022 1.0000 0.0046
-13.750 -1.1568 0.05026 0.04668 -0.0211 1.0000 0.0044
-13.500 -1.1787 0.04297 0.03913 -0.0268 1.0000 0.0044
-13.250 -1.1900 0.03907 0.03504 -0.0277 1.0000 0.0044
-13.000 -1.1961 0.03639 0.03217 -0.0265 1.0000 0.0044
-12.750 -1.1937 0.03417 0.02978 -0.0253 1.0000 0.0045
-12.500 -1.1858 0.03220 0.02761 -0.0243 1.0000 0.0045
-12.250 -1.1745 0.03043 0.02568 -0.0234 1.0000 0.0045
-12.000 -1.1606 0.02885 0.02393 -0.0226 1.0000 0.0046
-11.750 -1.1444 0.02743 0.02236 -0.0219 1.0000 0.0046
-11.500 -1.1266 0.02616 0.02094 -0.0212 1.0000 0.0047
-11.250 -1.1080 0.02488 0.01952 -0.0206 1.0000 0.0048
-11.000 -1.0894 0.02350 0.01799 -0.0199 1.0000 0.0050
-10.750 -1.0691 0.02232 0.01666 -0.0194 1.0000 0.0051
-10.500 -1.0475 0.02128 0.01549 -0.0189 1.0000 0.0053
-10.250 -1.0249 0.02035 0.01444 -0.0185 1.0000 0.0055
-10.000 -1.0016 0.01950 0.01347 -0.0181 1.0000 0.0056
-9.750 -0.9777 0.01872 0.01258 -0.0177 1.0000 0.0058
-9.500 -0.9534 0.01798 0.01174 -0.0174 1.0000 0.0060
-9.250 -0.9286 0.01731 0.01095 -0.0171 1.0000 0.0062
-9.000 -0.9035 0.01667 0.01023 -0.0168 1.0000 0.0065
-8.750 -0.8783 0.01602 0.00950 -0.0166 1.0000 0.0071
-8.500 -0.8531 0.01536 0.00879 -0.0163 1.0000 0.0084
-8.250 -0.8279 0.01466 0.00810 -0.0160 1.0000 0.0125
-8.000 -0.8022 0.01411 0.00756 -0.0158 1.0000 0.0190
-7.750 -0.7759 0.01369 0.00714 -0.0157 1.0000 0.0234
-7.500 -0.7494 0.01329 0.00672 -0.0155 1.0000 0.0266
-7.250 -0.7228 0.01293 0.00634 -0.0154 1.0000 0.0293
-7.000 -0.6961 0.01261 0.00598 -0.0152 1.0000 0.0314
-6.750 -0.6697 0.01223 0.00560 -0.0150 1.0000 0.0344
-6.500 -0.6433 0.01191 0.00527 -0.0148 1.0000 0.0378
-6.250 -0.6173 0.01157 0.00496 -0.0145 1.0000 0.0428
-6.000 -0.5917 0.01125 0.00469 -0.0142 1.0000 0.0502
-5.750 -0.5666 0.01100 0.00447 -0.0137 1.0000 0.0588
-5.500 -0.5371 0.01078 0.00429 -0.0141 0.9974 0.0677
-5.250 -0.5037 0.01055 0.00408 -0.0154 0.9935 0.0739
-5.000 -0.4712 0.01036 0.00388 -0.0164 0.9885 0.0788
-4.750 -0.4377 0.01019 0.00368 -0.0176 0.9839 0.0828
-4.500 -0.4054 0.00997 0.00349 -0.0185 0.9787 0.0875
-4.250 -0.3732 0.00981 0.00331 -0.0194 0.9733 0.0915
-4.000 -0.3429 0.00968 0.00315 -0.0198 0.9663 0.0946
-3.750 -0.3145 0.00951 0.00299 -0.0197 0.9576 0.0992
-3.500 -0.2885 0.00936 0.00285 -0.0191 0.9435 0.1048
-3.250 -0.2639 0.00925 0.00270 -0.0181 0.9245 0.1098
-3.000 -0.2391 0.00908 0.00254 -0.0171 0.9058 0.1170
-2.750 -0.2126 0.00896 0.00240 -0.0166 0.8924 0.1229
-2.500 -0.1858 0.00882 0.00225 -0.0162 0.8794 0.1311
-2.250 -0.1588 0.00869 0.00213 -0.0158 0.8659 0.1418
-2.000 -0.1317 0.00854 0.00201 -0.0155 0.8512 0.1582
-1.750 -0.1044 0.00838 0.00190 -0.0152 0.8358 0.1835
-1.500 -0.0771 0.00817 0.00179 -0.0150 0.8194 0.2222
-1.250 -0.0498 0.00796 0.00170 -0.0149 0.8006 0.2688
-1.000 -0.0227 0.00778 0.00160 -0.0146 0.7738 0.3205
-0.750 0.0039 0.00762 0.00151 -0.0143 0.7334 0.3810
-0.500 0.0307 0.00748 0.00143 -0.0141 0.6863 0.4510
-0.250 0.0578 0.00733 0.00138 -0.0140 0.6422 0.5277
0.000 0.0845 0.00721 0.00138 -0.0138 0.5913 0.6150
0.250 0.1112 0.00719 0.00141 -0.0135 0.5398 0.6846
0.500 0.1381 0.00728 0.00146 -0.0133 0.4897 0.7317
0.750 0.1647 0.00740 0.00153 -0.0129 0.4414 0.7738
1.000 0.1901 0.00749 0.00163 -0.0122 0.3995 0.8251
1.250 0.2143 0.00760 0.00174 -0.0112 0.3643 0.8686
1.500 0.2378 0.00774 0.00184 -0.0099 0.3345 0.9032
1.750 0.2609 0.00790 0.00193 -0.0085 0.3078 0.9323
2.000 0.2858 0.00805 0.00201 -0.0076 0.2833 0.9547
2.250 0.3137 0.00820 0.00207 -0.0074 0.2609 0.9701
2.500 0.3467 0.00838 0.00215 -0.0085 0.2364 0.9785
2.750 0.3803 0.00860 0.00224 -0.0098 0.2101 0.9858
3.000 0.4137 0.00885 0.00236 -0.0111 0.1844 0.9930
3.250 0.4475 0.00908 0.00249 -0.0125 0.1658 0.9992
3.500 0.4744 0.00928 0.00262 -0.0123 0.1541 1.0000
4.000 0.5279 0.00967 0.00293 -0.0120 0.1357 1.0000
4.250 0.5550 0.00989 0.00310 -0.0119 0.1278 1.0000
4.500 0.5824 0.01009 0.00328 -0.0118 0.1199 1.0000
4.750 0.6098 0.01032 0.00347 -0.0118 0.1132 1.0000
5.000 0.6373 0.01053 0.00367 -0.0117 0.1077 1.0000
5.250 0.6646 0.01079 0.00390 -0.0117 0.1022 1.0000
5.500 0.6922 0.01101 0.00413 -0.0117 0.0986 1.0000
5.750 0.7196 0.01124 0.00437 -0.0116 0.0947 1.0000
6.000 0.7468 0.01152 0.00464 -0.0116 0.0909 1.0000
6.250 0.7740 0.01181 0.00493 -0.0115 0.0875 1.0000
6.500 0.8013 0.01205 0.00521 -0.0114 0.0848 1.0000
6.750 0.8284 0.01233 0.00550 -0.0114 0.0821 1.0000
7.000 0.8553 0.01263 0.00583 -0.0113 0.0795 1.0000
7.250 0.8817 0.01302 0.00621 -0.0111 0.0760 1.0000
7.500 0.9087 0.01327 0.00651 -0.0110 0.0737 1.0000
7.750 0.9355 0.01354 0.00681 -0.0110 0.0705 1.0000
8.000 0.9619 0.01386 0.00715 -0.0108 0.0670 1.0000
8.250 0.9880 0.01423 0.00752 -0.0107 0.0633 1.0000
8.500 1.0146 0.01450 0.00785 -0.0106 0.0605 1.0000
8.750 1.0407 0.01483 0.00820 -0.0104 0.0568 1.0000
9.000 1.0664 0.01523 0.00860 -0.0102 0.0525 1.0000
9.250 1.0921 0.01558 0.00899 -0.0100 0.0475 1.0000
9.500 1.1171 0.01605 0.00944 -0.0098 0.0404 1.0000
9.750 1.1401 0.01681 0.01010 -0.0094 0.0267 1.0000
10.000 1.1602 0.01800 0.01121 -0.0087 0.0140 1.0000
10.250 1.1821 0.01888 0.01215 -0.0081 0.0108 1.0000
10.500 1.2046 0.01963 0.01297 -0.0076 0.0093 1.0000
10.750 1.2261 0.02047 0.01390 -0.0069 0.0084 1.0000
11.000 1.2473 0.02130 0.01483 -0.0063 0.0078 1.0000
11.250 1.2683 0.02211 0.01575 -0.0056 0.0074 1.0000
11.500 1.2884 0.02299 0.01673 -0.0049 0.0070 1.0000
11.750 1.3073 0.02394 0.01781 -0.0041 0.0067 1.0000
12.000 1.3249 0.02500 0.01899 -0.0031 0.0064 1.0000
12.250 1.3404 0.02619 0.02030 -0.0020 0.0062 1.0000
12.500 1.3531 0.02759 0.02183 -0.0007 0.0060 1.0000
12.750 1.3640 0.02901 0.02339 0.0007 0.0058 1.0000
13.000 1.3737 0.03035 0.02486 0.0023 0.0057 1.0000
13.250 1.3780 0.03181 0.02645 0.0045 0.0056 1.0000
13.500 1.3803 0.03354 0.02832 0.0062 0.0055 1.0000
13.750 1.3805 0.03562 0.03057 0.0075 0.0054 1.0000
14.000 1.3784 0.03817 0.03326 0.0081 0.0053 1.0000
14.250 1.3734 0.04138 0.03664 0.0079 0.0052 1.0000
14.500 1.3650 0.04554 0.04097 0.0063 0.0052 1.0000
14.750 1.3519 0.05114 0.04677 0.0031 0.0051 1.0000
15.000 1.3306 0.05924 0.05509 -0.0026 0.0051 1.0000
15.250 1.2947 0.07105 0.06716 -0.0105 0.0052 1.0000
15.500 1.2425 0.08550 0.08184 -0.0188 0.0054 1.0000
15.750 1.1865 0.10011 0.09663 -0.0263 0.0056 1.0000
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