ARA-D 6% AIRFOIL (arad6-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: ARA-D 6% AIRFOIL (arad6-il) Reynolds number: 1,000,000 Max Cl/Cd: 139.66 at α=2° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-arad6-il-1000000.txt Download as CSV file: xf-arad6-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: ARA-D 6% 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
------ -------- --------- --------- -------- -------- --------
-9.000 -0.3543 0.10592 0.10426 -0.0266 1.0000 0.0096
-8.750 -0.3577 0.10421 0.10259 -0.0249 1.0000 0.0097
-8.500 -0.3599 0.10233 0.10073 -0.0236 0.9998 0.0099
-8.250 -0.3462 0.09874 0.09714 -0.0270 0.9985 0.0102
-8.000 -0.3322 0.09501 0.09341 -0.0308 0.9968 0.0106
-7.750 -0.3174 0.09113 0.08954 -0.0350 0.9951 0.0111
-7.500 -0.2988 0.08620 0.08461 -0.0422 0.9915 0.0120
-7.250 -0.2759 0.08140 0.07979 -0.0498 0.9888 0.0122
-7.000 -0.2502 0.07633 0.07471 -0.0577 0.9868 0.0122
-6.750 -0.2267 0.06970 0.06806 -0.0664 0.9854 0.0126
-6.500 -0.2008 0.06659 0.06494 -0.0712 0.9841 0.0129
-6.250 -0.1759 0.06338 0.06171 -0.0760 0.9806 0.0133
-6.000 -0.1480 0.05974 0.05804 -0.0818 0.9767 0.0138
-5.750 -0.1166 0.05562 0.05388 -0.0886 0.9732 0.0146
-5.500 -0.0729 0.04990 0.04807 -0.0988 0.9695 0.0163
-5.250 -0.0390 0.04496 0.04305 -0.1053 0.9640 0.0164
-5.000 0.0007 0.03645 0.03434 -0.1156 0.9596 0.0172
-4.750 0.0644 0.01874 0.01561 -0.1313 0.9578 0.0167
-4.500 0.0997 0.01382 0.01000 -0.1345 0.9541 0.0151
-4.250 0.1301 0.01208 0.00791 -0.1352 0.9492 0.0150
-4.000 0.1589 0.01122 0.00685 -0.1354 0.9444 0.0153
-3.750 0.1880 0.01039 0.00584 -0.1356 0.9395 0.0155
-3.500 0.2171 0.00966 0.00496 -0.1357 0.9339 0.0158
-3.250 0.2455 0.00919 0.00438 -0.1356 0.9287 0.0162
-3.000 0.2745 0.00870 0.00380 -0.1358 0.9228 0.0167
-2.750 0.3036 0.00815 0.00315 -0.1359 0.9167 0.0179
-2.500 0.3322 0.00791 0.00285 -0.1359 0.9107 0.0189
-2.250 0.3607 0.00770 0.00261 -0.1359 0.9037 0.0201
-2.000 0.3892 0.00755 0.00241 -0.1359 0.8972 0.0216
-1.750 0.4181 0.00732 0.00217 -0.1359 0.8897 0.0279
-1.500 0.4468 0.00713 0.00204 -0.1360 0.8827 0.0513
-1.250 0.4751 0.00704 0.00197 -0.1360 0.8738 0.0642
-1.000 0.5030 0.00698 0.00189 -0.1358 0.8599 0.0778
-0.750 0.5307 0.00693 0.00183 -0.1356 0.8436 0.0954
-0.500 0.5587 0.00690 0.00180 -0.1356 0.8292 0.1154
-0.250 0.5867 0.00689 0.00177 -0.1355 0.8138 0.1333
0.000 0.6148 0.00689 0.00176 -0.1354 0.7979 0.1526
0.250 0.6429 0.00690 0.00175 -0.1354 0.7822 0.1705
0.500 0.6711 0.00691 0.00176 -0.1354 0.7671 0.1913
0.750 0.6993 0.00692 0.00179 -0.1355 0.7507 0.2218
1.000 0.7275 0.00688 0.00184 -0.1356 0.7330 0.2836
1.250 0.7496 0.00545 0.00190 -0.1347 0.7161 1.0000
1.500 0.7773 0.00561 0.00194 -0.1345 0.6953 1.0000
1.750 0.8050 0.00577 0.00199 -0.1344 0.6727 1.0000
2.000 0.8324 0.00596 0.00206 -0.1343 0.6466 1.0000
2.250 0.8596 0.00618 0.00215 -0.1341 0.6184 1.0000
2.500 0.8865 0.00645 0.00225 -0.1340 0.5837 1.0000
2.750 0.9132 0.00675 0.00239 -0.1337 0.5453 1.0000
3.000 0.9394 0.00713 0.00255 -0.1335 0.4982 1.0000
3.250 0.9646 0.00766 0.00277 -0.1331 0.4340 1.0000
3.500 0.9892 0.00829 0.00305 -0.1327 0.3607 1.0000
3.750 1.0137 0.00893 0.00336 -0.1323 0.2928 1.0000
4.000 1.0393 0.00937 0.00361 -0.1320 0.2541 1.0000
4.250 1.0653 0.00974 0.00384 -0.1317 0.2261 1.0000
4.500 1.0913 0.01009 0.00407 -0.1315 0.2037 1.0000
4.750 1.1177 0.01038 0.00430 -0.1313 0.1879 1.0000
5.000 1.1438 0.01067 0.00452 -0.1311 0.1729 1.0000
5.250 1.1699 0.01096 0.00476 -0.1308 0.1590 1.0000
5.500 1.1958 0.01126 0.00500 -0.1306 0.1466 1.0000
5.750 1.2218 0.01154 0.00525 -0.1303 0.1364 1.0000
6.000 1.2476 0.01182 0.00550 -0.1300 0.1260 1.0000
6.250 1.2731 0.01214 0.00578 -0.1297 0.1152 1.0000
6.500 1.2983 0.01248 0.00607 -0.1293 0.1049 1.0000
6.750 1.3231 0.01284 0.00640 -0.1289 0.0944 1.0000
7.000 1.3478 0.01321 0.00672 -0.1284 0.0841 1.0000
7.250 1.3723 0.01359 0.00707 -0.1279 0.0746 1.0000
7.500 1.3963 0.01400 0.00744 -0.1273 0.0657 1.0000
7.750 1.4197 0.01446 0.00787 -0.1267 0.0567 1.0000
8.000 1.4436 0.01485 0.00826 -0.1261 0.0511 1.0000
8.250 1.4668 0.01531 0.00869 -0.1254 0.0446 1.0000
8.500 1.4895 0.01578 0.00915 -0.1246 0.0393 1.0000
8.750 1.5123 0.01623 0.00962 -0.1239 0.0349 1.0000
9.000 1.5346 0.01671 0.01010 -0.1230 0.0310 1.0000
9.250 1.5564 0.01723 0.01063 -0.1221 0.0268 1.0000
9.500 1.5774 0.01779 0.01118 -0.1211 0.0224 1.0000
9.750 1.5970 0.01848 0.01184 -0.1198 0.0164 1.0000
10.000 1.6143 0.01939 0.01272 -0.1181 0.0105 1.0000
10.250 1.6318 0.02021 0.01358 -0.1165 0.0085 1.0000
10.500 1.6490 0.02102 0.01445 -0.1147 0.0075 1.0000
10.750 1.6664 0.02173 0.01524 -0.1131 0.0069 1.0000
11.000 1.6820 0.02254 0.01613 -0.1111 0.0064 1.0000
11.250 1.6954 0.02350 0.01717 -0.1088 0.0059 1.0000
11.500 1.7039 0.02480 0.01860 -0.1057 0.0055 1.0000
11.750 1.7126 0.02585 0.01977 -0.1026 0.0053 1.0000
12.000 1.7205 0.02682 0.02085 -0.0994 0.0052 1.0000
12.250 1.7277 0.02793 0.02206 -0.0963 0.0051 1.0000
12.500 1.7341 0.02914 0.02339 -0.0932 0.0049 1.0000
12.750 1.7396 0.03047 0.02484 -0.0902 0.0048 1.0000
13.000 1.7438 0.03196 0.02644 -0.0872 0.0047 1.0000
13.250 1.7473 0.03356 0.02817 -0.0844 0.0046 1.0000
13.500 1.7494 0.03533 0.03005 -0.0816 0.0045 1.0000
13.750 1.7505 0.03728 0.03212 -0.0790 0.0044 1.0000
14.000 1.7504 0.03940 0.03437 -0.0766 0.0043 1.0000
14.250 1.7483 0.04181 0.03691 -0.0743 0.0042 1.0000
14.500 1.7451 0.04447 0.03970 -0.0723 0.0041 1.0000
14.750 1.7395 0.04751 0.04289 -0.0705 0.0041 1.0000
15.000 1.7321 0.05094 0.04647 -0.0690 0.0040 1.0000
15.250 1.7222 0.05490 0.05057 -0.0680 0.0040 1.0000
15.500 1.7098 0.05940 0.05522 -0.0676 0.0039 1.0000
15.750 1.6951 0.06455 0.06054 -0.0677 0.0039 1.0000
16.000 1.6795 0.07026 0.06641 -0.0686 0.0038 1.0000
16.250 1.6611 0.07680 0.07311 -0.0702 0.0038 1.0000
16.500 1.6409 0.08402 0.08051 -0.0726 0.0038 1.0000
16.750 1.6214 0.09160 0.08824 -0.0756 0.0038 1.0000
17.000 1.6000 0.09990 0.09670 -0.0792 0.0038 1.0000
17.250 1.5774 0.10873 0.10570 -0.0833 0.0038 1.0000
17.500 1.5541 0.11808 0.11521 -0.0880 0.0038 1.0000
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