RONCZ 1080 VOYAGER INNER AFT WING AIRFOIL (r1080-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: RONCZ 1080 VOYAGER INNER AFT WING AIRFOIL (r1080-il) Reynolds number: 1,000,000 Max Cl/Cd: 127.05 at α=6° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-r1080-il-1000000-n5.txt Download as CSV file: xf-r1080-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: RONCZ 1080 VOYAGER INNER AFT WING 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 = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-18.500 -0.5683 0.11590 0.11250 -0.0791 0.7430 0.0065
-18.250 -0.6040 0.10484 0.10128 -0.0848 0.7407 0.0063
-18.000 -0.6296 0.09608 0.09240 -0.0895 0.7367 0.0063
-17.750 -0.6656 0.08577 0.08194 -0.0952 0.7338 0.0063
-17.500 -0.6962 0.07649 0.07250 -0.1005 0.7296 0.0063
-17.250 -0.7190 0.06875 0.06459 -0.1051 0.7241 0.0063
-17.000 -0.7363 0.06221 0.05790 -0.1091 0.7187 0.0063
-16.750 -0.7540 0.05616 0.05169 -0.1125 0.7133 0.0063
-16.500 -0.7624 0.05183 0.04722 -0.1146 0.7072 0.0063
-16.250 -0.7752 0.04739 0.04263 -0.1164 0.7020 0.0063
-16.000 -0.7790 0.04430 0.03941 -0.1172 0.6969 0.0063
-15.750 -0.7917 0.04063 0.03559 -0.1176 0.6920 0.0064
-15.500 -0.7953 0.03813 0.03297 -0.1174 0.6870 0.0063
-15.250 -0.7924 0.03632 0.03106 -0.1170 0.6828 0.0063
-15.000 -0.8019 0.03367 0.02828 -0.1160 0.6789 0.0065
-14.750 -0.8034 0.03176 0.02625 -0.1148 0.6746 0.0065
-14.500 -0.7993 0.03034 0.02473 -0.1136 0.6704 0.0065
-14.250 -0.7974 0.02880 0.02309 -0.1121 0.6672 0.0065
-14.000 -0.7905 0.02764 0.02186 -0.1109 0.6639 0.0066
-13.750 -0.7822 0.02658 0.02074 -0.1096 0.6607 0.0067
-13.500 -0.7745 0.02553 0.01960 -0.1081 0.6572 0.0068
-13.250 -0.7629 0.02474 0.01874 -0.1069 0.6540 0.0068
-13.000 -0.7556 0.02369 0.01759 -0.1051 0.6508 0.0069
-12.750 -0.7433 0.02294 0.01679 -0.1038 0.6485 0.0070
-12.500 -0.7320 0.02213 0.01591 -0.1022 0.6458 0.0070
-12.250 -0.7185 0.02147 0.01520 -0.1009 0.6432 0.0071
-12.000 -0.7051 0.02081 0.01448 -0.0995 0.6406 0.0072
-11.750 -0.6927 0.02010 0.01369 -0.0978 0.6384 0.0072
-11.500 -0.6775 0.01957 0.01310 -0.0965 0.6361 0.0074
-11.250 -0.6632 0.01897 0.01243 -0.0950 0.6339 0.0075
-11.000 -0.6484 0.01838 0.01179 -0.0935 0.6325 0.0075
-10.750 -0.6321 0.01788 0.01125 -0.0921 0.6308 0.0077
-10.500 -0.6153 0.01742 0.01074 -0.0908 0.6291 0.0077
-10.250 -0.5992 0.01691 0.01018 -0.0893 0.6274 0.0079
-10.000 -0.5826 0.01645 0.00967 -0.0878 0.6256 0.0080
-9.750 -0.5653 0.01603 0.00921 -0.0864 0.6240 0.0080
-9.500 -0.5477 0.01565 0.00878 -0.0850 0.6224 0.0082
-9.250 -0.5306 0.01525 0.00833 -0.0835 0.6207 0.0083
-9.000 -0.5126 0.01492 0.00795 -0.0820 0.6191 0.0084
-8.500 -0.4802 0.01416 0.00713 -0.0784 0.6165 0.0089
-8.250 -0.4626 0.01386 0.00681 -0.0767 0.6154 0.0091
-8.000 -0.4429 0.01359 0.00652 -0.0755 0.6142 0.0095
-7.750 -0.4217 0.01332 0.00624 -0.0745 0.6128 0.0097
-7.500 -0.4002 0.01306 0.00595 -0.0735 0.6115 0.0100
-7.250 -0.3783 0.01281 0.00567 -0.0726 0.6102 0.0104
-7.000 -0.3558 0.01258 0.00542 -0.0718 0.6090 0.0107
-6.750 -0.3334 0.01234 0.00516 -0.0710 0.6078 0.0110
-6.500 -0.3110 0.01209 0.00489 -0.0702 0.6067 0.0116
-6.250 -0.2879 0.01187 0.00466 -0.0695 0.6055 0.0123
-6.000 -0.2643 0.01168 0.00445 -0.0689 0.6044 0.0129
-5.750 -0.2407 0.01149 0.00425 -0.0683 0.6032 0.0139
-5.500 -0.2169 0.01131 0.00406 -0.0677 0.6020 0.0153
-5.250 -0.1929 0.01114 0.00388 -0.0671 0.6008 0.0176
-5.000 -0.1687 0.01093 0.00370 -0.0666 0.6002 0.0220
-4.750 -0.1447 0.01070 0.00352 -0.0661 0.5995 0.0301
-4.500 -0.1204 0.01049 0.00336 -0.0656 0.5987 0.0399
-4.250 -0.0960 0.01029 0.00321 -0.0652 0.5979 0.0520
-4.000 -0.0714 0.01009 0.00308 -0.0647 0.5971 0.0652
-3.750 -0.0464 0.00991 0.00295 -0.0644 0.5961 0.0803
-3.500 -0.0219 0.00970 0.00283 -0.0640 0.5951 0.1005
-3.250 0.0024 0.00946 0.00270 -0.0635 0.5941 0.1283
-3.000 0.0258 0.00918 0.00258 -0.0630 0.5931 0.1705
-2.750 0.0485 0.00884 0.00244 -0.0623 0.5922 0.2269
-2.500 0.0701 0.00843 0.00230 -0.0615 0.5913 0.3025
-2.250 0.0921 0.00802 0.00216 -0.0607 0.5904 0.3799
-2.000 0.1140 0.00759 0.00202 -0.0599 0.5895 0.4644
-1.750 0.1367 0.00721 0.00189 -0.0592 0.5887 0.5446
-1.500 0.1595 0.00684 0.00181 -0.0585 0.5878 0.6273
-1.250 0.1854 0.00674 0.00186 -0.0582 0.5868 0.6813
-1.000 0.2135 0.00676 0.00190 -0.0584 0.5858 0.7020
-0.750 0.2423 0.00681 0.00194 -0.0587 0.5847 0.7135
-0.500 0.2711 0.00685 0.00197 -0.0590 0.5840 0.7243
-0.250 0.2998 0.00688 0.00202 -0.0592 0.5833 0.7336
0.000 0.3287 0.00693 0.00207 -0.0595 0.5826 0.7422
0.250 0.3574 0.00697 0.00213 -0.0598 0.5819 0.7489
0.500 0.3862 0.00703 0.00219 -0.0601 0.5811 0.7547
0.750 0.4152 0.00707 0.00223 -0.0605 0.5802 0.7585
1.000 0.4442 0.00711 0.00225 -0.0609 0.5791 0.7606
1.250 0.4732 0.00714 0.00227 -0.0613 0.5780 0.7623
1.500 0.5020 0.00715 0.00229 -0.0617 0.5767 0.7642
1.750 0.5307 0.00716 0.00231 -0.0620 0.5751 0.7658
2.000 0.5592 0.00719 0.00234 -0.0623 0.5732 0.7672
2.250 0.5877 0.00723 0.00236 -0.0626 0.5714 0.7685
2.500 0.6161 0.00728 0.00240 -0.0629 0.5693 0.7698
2.750 0.6446 0.00731 0.00244 -0.0633 0.5675 0.7711
3.000 0.6730 0.00732 0.00248 -0.0636 0.5653 0.7722
3.250 0.7015 0.00734 0.00251 -0.0639 0.5629 0.7733
3.500 0.7297 0.00735 0.00254 -0.0642 0.5601 0.7744
3.750 0.7576 0.00738 0.00256 -0.0644 0.5569 0.7755
4.000 0.7849 0.00744 0.00260 -0.0645 0.5533 0.7767
4.250 0.8130 0.00746 0.00265 -0.0648 0.5501 0.7778
4.500 0.8410 0.00748 0.00270 -0.0651 0.5457 0.7787
4.750 0.8682 0.00752 0.00274 -0.0652 0.5411 0.7797
5.000 0.8949 0.00756 0.00279 -0.0652 0.5366 0.7809
5.250 0.9223 0.00759 0.00286 -0.0653 0.5308 0.7820
5.500 0.9480 0.00766 0.00292 -0.0651 0.5232 0.7832
5.750 0.9737 0.00773 0.00301 -0.0650 0.5126 0.7844
6.000 0.9973 0.00785 0.00310 -0.0644 0.4976 0.7857
6.250 1.0152 0.00814 0.00328 -0.0628 0.4696 0.7871
6.500 1.0276 0.00861 0.00360 -0.0601 0.4362 0.7889
6.750 1.0376 0.00913 0.00398 -0.0571 0.4051 0.7908
7.000 1.0423 0.00964 0.00436 -0.0530 0.3755 0.7926
7.250 1.0465 0.01016 0.00478 -0.0488 0.3515 0.7944
7.500 1.0511 0.01073 0.00525 -0.0449 0.3278 0.7960
7.750 1.0548 0.01133 0.00578 -0.0410 0.3071 0.7979
8.000 1.0563 0.01203 0.00640 -0.0369 0.2861 0.8002
8.250 1.0572 0.01282 0.00713 -0.0329 0.2663 0.8025
8.500 1.0597 0.01366 0.00793 -0.0295 0.2501 0.8049
8.750 1.0613 0.01464 0.00887 -0.0263 0.2339 0.8074
9.000 1.0636 0.01572 0.00990 -0.0234 0.2190 0.8102
9.250 1.0654 0.01693 0.01106 -0.0206 0.2036 0.8127
9.500 1.0697 0.01808 0.01219 -0.0183 0.1916 0.8153
9.750 1.0743 0.01926 0.01336 -0.0162 0.1806 0.8182
10.000 1.0786 0.02051 0.01458 -0.0141 0.1683 0.8212
10.250 1.0847 0.02170 0.01576 -0.0123 0.1579 0.8242
10.500 1.0910 0.02291 0.01695 -0.0106 0.1488 0.8274
11.000 1.1044 0.02532 0.01935 -0.0075 0.1307 0.8339
11.250 1.1100 0.02661 0.02063 -0.0059 0.1219 0.8379
11.500 1.1174 0.02782 0.02183 -0.0045 0.1141 0.8421
11.750 1.1256 0.02904 0.02306 -0.0033 0.1074 0.8465
12.000 1.1326 0.03031 0.02433 -0.0020 0.0998 0.8512
12.250 1.1413 0.03151 0.02556 -0.0009 0.0940 0.8572
12.500 1.1494 0.03278 0.02683 0.0002 0.0883 0.8639
12.750 1.1578 0.03400 0.02810 0.0013 0.0821 0.8724
13.000 1.1638 0.03541 0.02952 0.0025 0.0754 0.8836
13.250 1.1724 0.03659 0.03076 0.0036 0.0703 0.9005
13.500 1.1851 0.03803 0.03231 0.0033 0.0645 0.9378
13.750 1.2141 0.04001 0.03431 -0.0011 0.0570 0.9648
14.250 1.2359 0.04288 0.03719 -0.0007 0.0503 1.0000
14.750 1.2551 0.04576 0.04010 0.0003 0.0448 1.0000
15.250 1.2730 0.04885 0.04324 0.0010 0.0409 1.0000
15.750 1.2891 0.05215 0.04656 0.0017 0.0357 1.0000
16.000 1.2975 0.05382 0.04826 0.0020 0.0342 1.0000
16.250 1.3061 0.05548 0.04995 0.0022 0.0327 1.0000
16.500 1.3126 0.05735 0.05184 0.0025 0.0306 1.0000
16.750 1.3202 0.05918 0.05371 0.0026 0.0293 1.0000
17.000 1.3275 0.06103 0.05559 0.0027 0.0276 1.0000
17.250 1.3325 0.06313 0.05771 0.0028 0.0257 1.0000
17.500 1.3389 0.06514 0.05977 0.0028 0.0245 1.0000
17.750 1.3451 0.06718 0.06185 0.0028 0.0232 1.0000
18.000 1.3485 0.06958 0.06428 0.0027 0.0214 1.0000
18.250 1.3534 0.07184 0.06658 0.0025 0.0198 1.0000
18.500 1.3560 0.07438 0.06915 0.0023 0.0184 1.0000
18.750 1.3596 0.07685 0.07167 0.0020 0.0171 1.0000
19.000 1.3620 0.07950 0.07437 0.0017 0.0159 1.0000
19.250 1.3633 0.08234 0.07725 0.0012 0.0145 1.0000
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