SM701 (sm701-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: SM701 (sm701-il) Reynolds number: 1,000,000 Max Cl/Cd: 93.6 at α=5.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-sm701-il-1000000-n5.txt Download as CSV file: xf-sm701-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: SM701
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 1.000 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-17.000 -0.7432 0.08807 0.08554 -0.0777 0.9978 0.0094
-16.750 -0.7846 0.07536 0.07259 -0.0864 0.9971 0.0094
-16.500 -0.8004 0.06767 0.06474 -0.0922 0.9963 0.0094
-16.250 -0.8071 0.06185 0.05880 -0.0970 0.9954 0.0095
-16.000 -0.8171 0.05592 0.05271 -0.1017 0.9945 0.0095
-15.750 -0.8194 0.05136 0.04802 -0.1056 0.9936 0.0096
-15.500 -0.8213 0.04782 0.04438 -0.1077 0.9923 0.0096
-15.250 -0.8212 0.04457 0.04101 -0.1097 0.9908 0.0097
-15.000 -0.8202 0.04136 0.03769 -0.1119 0.9892 0.0098
-14.750 -0.8052 0.03960 0.03587 -0.1138 0.9879 0.0100
-14.500 -0.7940 0.03737 0.03355 -0.1158 0.9866 0.0101
-14.250 -0.7862 0.03466 0.03071 -0.1182 0.9853 0.0102
-14.000 -0.7734 0.03245 0.02839 -0.1203 0.9842 0.0102
-13.750 -0.7556 0.03089 0.02674 -0.1222 0.9834 0.0104
-13.500 -0.7448 0.02933 0.02510 -0.1227 0.9813 0.0105
-13.250 -0.7347 0.02779 0.02347 -0.1229 0.9784 0.0106
-13.000 -0.7178 0.02643 0.02202 -0.1240 0.9762 0.0107
-12.750 -0.6971 0.02518 0.02070 -0.1255 0.9746 0.0107
-12.500 -0.6725 0.02411 0.01955 -0.1274 0.9732 0.0109
-12.250 -0.6515 0.02244 0.01779 -0.1295 0.9718 0.0110
-12.000 -0.6378 0.02130 0.01659 -0.1294 0.9677 0.0112
-11.750 -0.6219 0.02033 0.01558 -0.1292 0.9630 0.0113
-11.500 -0.6000 0.01940 0.01459 -0.1300 0.9596 0.0114
-11.250 -0.5793 0.01866 0.01381 -0.1303 0.9555 0.0116
-11.000 -0.5678 0.01800 0.01310 -0.1287 0.9472 0.0117
-10.750 -0.5509 0.01733 0.01238 -0.1280 0.9399 0.0118
-10.500 -0.5354 0.01673 0.01172 -0.1269 0.9293 0.0120
-10.250 -0.5156 0.01624 0.01118 -0.1263 0.9166 0.0123
-10.000 -0.4932 0.01567 0.01053 -0.1261 0.9019 0.0124
-9.750 -0.4712 0.01519 0.00993 -0.1257 0.8852 0.0127
-9.250 -0.4310 0.01438 0.00890 -0.1240 0.8548 0.0130
-9.000 -0.4106 0.01400 0.00843 -0.1231 0.8427 0.0132
-8.750 -0.3895 0.01366 0.00801 -0.1223 0.8321 0.0133
-8.500 -0.3680 0.01332 0.00759 -0.1215 0.8220 0.0135
-8.250 -0.3453 0.01301 0.00721 -0.1209 0.8137 0.0136
-8.000 -0.3222 0.01273 0.00686 -0.1204 0.8060 0.0138
-7.750 -0.2999 0.01230 0.00638 -0.1198 0.7994 0.0141
-7.500 -0.2766 0.01192 0.00595 -0.1193 0.7928 0.0144
-7.250 -0.2525 0.01162 0.00561 -0.1189 0.7867 0.0147
-7.000 -0.2272 0.01135 0.00532 -0.1187 0.7811 0.0150
-6.750 -0.2017 0.01111 0.00504 -0.1185 0.7752 0.0154
-6.500 -0.1761 0.01090 0.00479 -0.1183 0.7702 0.0158
-6.250 -0.1496 0.01067 0.00454 -0.1183 0.7658 0.0163
-6.000 -0.1230 0.01046 0.00429 -0.1182 0.7612 0.0166
-5.750 -0.0965 0.01027 0.00406 -0.1181 0.7565 0.0169
-5.500 -0.0695 0.01009 0.00385 -0.1181 0.7525 0.0172
-5.250 -0.0424 0.00984 0.00359 -0.1182 0.7483 0.0179
-5.000 -0.0151 0.00965 0.00338 -0.1182 0.7442 0.0186
-4.750 0.0123 0.00950 0.00320 -0.1183 0.7400 0.0193
-4.500 0.0399 0.00936 0.00304 -0.1184 0.7356 0.0202
-4.250 0.0678 0.00922 0.00289 -0.1185 0.7303 0.0211
-4.000 0.0951 0.00908 0.00273 -0.1185 0.7239 0.0235
-3.750 0.1227 0.00893 0.00258 -0.1185 0.7178 0.0286
-3.500 0.1501 0.00870 0.00243 -0.1187 0.7107 0.0512
-3.250 0.1773 0.00850 0.00229 -0.1188 0.7038 0.0757
-3.000 0.2055 0.00826 0.00216 -0.1191 0.6976 0.1095
-2.750 0.2335 0.00802 0.00204 -0.1194 0.6916 0.1513
-2.500 0.2617 0.00770 0.00190 -0.1198 0.6863 0.2151
-2.250 0.2908 0.00716 0.00172 -0.1207 0.6806 0.3265
-2.000 0.3198 0.00666 0.00158 -0.1215 0.6743 0.4486
-1.750 0.3487 0.00657 0.00157 -0.1218 0.6685 0.4885
-1.500 0.3776 0.00652 0.00158 -0.1221 0.6618 0.5204
-1.250 0.4057 0.00653 0.00161 -0.1222 0.6548 0.5456
-1.000 0.4345 0.00654 0.00165 -0.1223 0.6473 0.5652
-0.750 0.4622 0.00660 0.00167 -0.1223 0.6382 0.5736
-0.500 0.4903 0.00664 0.00168 -0.1223 0.6278 0.5763
-0.250 0.5178 0.00670 0.00169 -0.1223 0.6160 0.5788
0.000 0.5444 0.00680 0.00171 -0.1220 0.5995 0.5813
0.250 0.5702 0.00693 0.00174 -0.1216 0.5782 0.5839
0.500 0.5946 0.00713 0.00180 -0.1209 0.5502 0.5860
0.750 0.6187 0.00735 0.00189 -0.1203 0.5224 0.5885
1.000 0.6424 0.00760 0.00201 -0.1195 0.4937 0.5909
1.250 0.6666 0.00783 0.00213 -0.1189 0.4667 0.5935
1.500 0.6910 0.00806 0.00225 -0.1183 0.4450 0.5963
1.750 0.7156 0.00828 0.00237 -0.1177 0.4235 0.5992
2.000 0.7398 0.00851 0.00250 -0.1171 0.4019 0.6019
2.250 0.7642 0.00873 0.00263 -0.1165 0.3830 0.6043
2.500 0.7889 0.00891 0.00276 -0.1160 0.3675 0.6071
2.750 0.8132 0.00912 0.00290 -0.1154 0.3515 0.6100
3.000 0.8371 0.00934 0.00304 -0.1147 0.3351 0.6130
3.250 0.8615 0.00953 0.00319 -0.1142 0.3229 0.6162
3.500 0.8855 0.00973 0.00333 -0.1135 0.3116 0.6193
4.000 0.9323 0.01012 0.00365 -0.1120 0.2877 0.6260
4.250 0.9547 0.01031 0.00380 -0.1111 0.2780 0.6295
4.500 0.9766 0.01051 0.00397 -0.1100 0.2681 0.6331
4.750 0.9987 0.01070 0.00414 -0.1090 0.2593 0.6363
5.000 1.0201 0.01094 0.00434 -0.1080 0.2496 0.6398
5.250 1.0427 0.01114 0.00453 -0.1071 0.2419 0.6438
5.500 1.0641 0.01139 0.00476 -0.1060 0.2342 0.6481
5.750 1.0863 0.01161 0.00497 -0.1051 0.2267 0.6525
6.000 1.1072 0.01188 0.00522 -0.1040 0.2185 0.6568
6.250 1.1295 0.01210 0.00544 -0.1031 0.2126 0.6615
6.500 1.1502 0.01238 0.00571 -0.1020 0.2059 0.6662
6.750 1.1716 0.01263 0.00596 -0.1010 0.1999 0.6707
7.000 1.1924 0.01291 0.00624 -0.0999 0.1934 0.6754
7.250 1.2130 0.01320 0.00654 -0.0988 0.1879 0.6807
7.500 1.2341 0.01346 0.00682 -0.0978 0.1836 0.6861
7.750 1.2540 0.01378 0.00714 -0.0966 0.1780 0.6912
8.000 1.2739 0.01411 0.00747 -0.0955 0.1726 0.6975
8.250 1.2943 0.01441 0.00780 -0.0945 0.1684 0.7040
8.500 1.3135 0.01476 0.00817 -0.0933 0.1638 0.7105
8.750 1.3322 0.01514 0.00857 -0.0920 0.1590 0.7176
9.000 1.3521 0.01548 0.00894 -0.0909 0.1551 0.7241
9.250 1.3706 0.01587 0.00936 -0.0897 0.1507 0.7314
9.500 1.3881 0.01633 0.00983 -0.0883 0.1460 0.7389
9.750 1.4070 0.01672 0.01026 -0.0872 0.1427 0.7467
10.000 1.4249 0.01716 0.01074 -0.0860 0.1388 0.7553
10.250 1.4418 0.01767 0.01128 -0.0846 0.1346 0.7647
10.500 1.4585 0.01819 0.01184 -0.0833 0.1302 0.7745
10.750 1.4752 0.01872 0.01240 -0.0820 0.1256 0.7857
11.000 1.4898 0.01937 0.01308 -0.0805 0.1201 0.7968
11.250 1.5057 0.01996 0.01372 -0.0792 0.1161 0.8087
11.500 1.5206 0.02062 0.01441 -0.0778 0.1112 0.8223
11.750 1.5334 0.02141 0.01523 -0.0762 0.1055 0.8378
12.000 1.5470 0.02212 0.01601 -0.0747 0.1004 0.8569
12.250 1.5579 0.02294 0.01689 -0.0729 0.0954 0.8862
12.500 1.5649 0.02356 0.01766 -0.0702 0.0917 1.0000
12.750 1.5776 0.02450 0.01861 -0.0689 0.0869 1.0000
13.000 1.5887 0.02558 0.01968 -0.0676 0.0820 1.0000
13.250 1.6015 0.02656 0.02069 -0.0664 0.0784 1.0000
13.500 1.6114 0.02778 0.02190 -0.0651 0.0734 1.0000
13.750 1.6217 0.02899 0.02312 -0.0639 0.0690 1.0000
14.000 1.6314 0.03028 0.02443 -0.0627 0.0649 1.0000
14.250 1.6399 0.03170 0.02585 -0.0615 0.0608 1.0000
14.500 1.6482 0.03318 0.02734 -0.0604 0.0563 1.0000
14.750 1.6531 0.03497 0.02912 -0.0592 0.0509 1.0000
15.000 1.6570 0.03691 0.03107 -0.0580 0.0456 1.0000
15.250 1.6625 0.03876 0.03294 -0.0570 0.0415 1.0000
15.500 1.6643 0.04101 0.03520 -0.0559 0.0368 1.0000
15.750 1.6663 0.04330 0.03750 -0.0551 0.0327 1.0000
16.000 1.6681 0.04570 0.03994 -0.0543 0.0292 1.0000
16.250 1.6685 0.04833 0.04259 -0.0537 0.0262 1.0000
16.500 1.6703 0.05088 0.04520 -0.0532 0.0237 1.0000
16.750 1.6686 0.05389 0.04825 -0.0529 0.0210 1.0000
17.000 1.6672 0.05697 0.05139 -0.0527 0.0186 1.0000
17.250 1.6655 0.06020 0.05469 -0.0527 0.0169 1.0000
17.500 1.6603 0.06400 0.05854 -0.0529 0.0146 1.0000
17.750 1.6560 0.06778 0.06240 -0.0534 0.0128 1.0000
18.000 1.6482 0.07218 0.06688 -0.0541 0.0108 1.0000
18.250 1.6388 0.07698 0.07176 -0.0552 0.0090 1.0000
18.750 1.6178 0.08737 0.08234 -0.0582 0.0065 1.0000
19.000 1.6054 0.09308 0.08817 -0.0602 0.0058 1.0000
19.250 1.5939 0.09880 0.09400 -0.0623 0.0053 1.0000
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