DSMA-523B AIRFOIL (dsma523b-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: DSMA-523B AIRFOIL (dsma523b-il) Reynolds number: 1,000,000 Max Cl/Cd: 77.27 at α=7.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-dsma523b-il-1000000-n5.txt Download as CSV file: xf-dsma523b-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: DSMA-523B 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
------ -------- --------- --------- -------- -------- --------
-19.750 -1.0242 0.11704 0.11412 -0.0527 0.9847 0.0166
-19.500 -1.0762 0.10358 0.10048 -0.0601 0.9849 0.0166
-19.250 -1.1218 0.09165 0.08836 -0.0668 0.9852 0.0165
-19.000 -1.1576 0.08177 0.07830 -0.0723 0.9856 0.0165
-18.750 -1.1833 0.07387 0.07025 -0.0766 0.9859 0.0165
-18.500 -1.2031 0.06721 0.06346 -0.0802 0.9863 0.0166
-18.250 -1.2170 0.06172 0.05784 -0.0830 0.9866 0.0166
-18.000 -1.2278 0.05700 0.05301 -0.0851 0.9869 0.0167
-17.750 -1.2347 0.05310 0.04900 -0.0865 0.9872 0.0167
-17.500 -1.2401 0.04964 0.04544 -0.0875 0.9875 0.0168
-17.250 -1.2434 0.04666 0.04237 -0.0880 0.9877 0.0169
-17.000 -1.2454 0.04410 0.03973 -0.0880 0.9880 0.0170
-16.750 -1.2485 0.04184 0.03739 -0.0873 0.9881 0.0171
-16.500 -1.2506 0.03985 0.03533 -0.0863 0.9882 0.0172
-16.250 -1.2512 0.03808 0.03349 -0.0851 0.9884 0.0173
-16.000 -1.2516 0.03637 0.03171 -0.0838 0.9885 0.0174
-15.750 -1.2501 0.03483 0.03010 -0.0824 0.9887 0.0175
-15.500 -1.2473 0.03345 0.02866 -0.0810 0.9888 0.0176
-15.250 -1.2441 0.03213 0.02727 -0.0794 0.9889 0.0177
-15.000 -1.2407 0.03087 0.02595 -0.0778 0.9889 0.0179
-14.750 -1.2359 0.02977 0.02480 -0.0760 0.9890 0.0180
-14.500 -1.2331 0.02868 0.02365 -0.0739 0.9889 0.0182
-14.250 -1.2314 0.02771 0.02263 -0.0713 0.9888 0.0183
-14.000 -1.2226 0.02668 0.02154 -0.0700 0.9886 0.0185
-13.750 -1.2051 0.02565 0.02045 -0.0702 0.9882 0.0186
-13.500 -1.1874 0.02475 0.01950 -0.0702 0.9880 0.0187
-13.250 -1.1678 0.02384 0.01853 -0.0707 0.9878 0.0189
-13.000 -1.1456 0.02279 0.01744 -0.0718 0.9875 0.0192
-12.750 -1.1209 0.02189 0.01650 -0.0730 0.9872 0.0195
-12.500 -1.0958 0.02110 0.01567 -0.0742 0.9870 0.0198
-12.250 -1.0693 0.02039 0.01493 -0.0754 0.9869 0.0201
-12.000 -1.0411 0.01971 0.01423 -0.0769 0.9867 0.0204
-11.750 -1.0118 0.01908 0.01356 -0.0785 0.9865 0.0207
-11.500 -0.9817 0.01849 0.01294 -0.0801 0.9863 0.0211
-11.250 -0.9515 0.01793 0.01235 -0.0817 0.9862 0.0215
-11.000 -0.9213 0.01741 0.01179 -0.0832 0.9861 0.0218
-10.750 -0.8907 0.01692 0.01127 -0.0847 0.9860 0.0221
-10.500 -0.8599 0.01647 0.01079 -0.0862 0.9859 0.0224
-10.250 -0.8286 0.01595 0.01026 -0.0878 0.9858 0.0230
-10.000 -0.7973 0.01552 0.00982 -0.0893 0.9857 0.0236
-9.750 -0.7661 0.01513 0.00943 -0.0907 0.9856 0.0242
-9.500 -0.7347 0.01478 0.00907 -0.0920 0.9855 0.0249
-9.250 -0.7032 0.01445 0.00872 -0.0934 0.9854 0.0255
-9.000 -0.6718 0.01416 0.00841 -0.0946 0.9853 0.0261
-8.750 -0.6433 0.01385 0.00811 -0.0952 0.9849 0.0267
-8.500 -0.6136 0.01354 0.00780 -0.0960 0.9844 0.0276
-8.250 -0.5832 0.01326 0.00753 -0.0970 0.9840 0.0285
-8.000 -0.5525 0.01301 0.00728 -0.0979 0.9837 0.0295
-7.750 -0.5215 0.01278 0.00705 -0.0989 0.9833 0.0304
-7.500 -0.4898 0.01254 0.00682 -0.1001 0.9829 0.0319
-7.250 -0.4580 0.01232 0.00663 -0.1012 0.9826 0.0336
-7.000 -0.4260 0.01212 0.00645 -0.1024 0.9822 0.0352
-6.750 -0.3938 0.01195 0.00632 -0.1035 0.9818 0.0379
-6.500 -0.3616 0.01181 0.00622 -0.1046 0.9814 0.0408
-6.250 -0.3298 0.01170 0.00614 -0.1056 0.9811 0.0439
-6.000 -0.2978 0.01159 0.00604 -0.1066 0.9808 0.0460
-5.750 -0.2659 0.01150 0.00599 -0.1076 0.9804 0.0481
-5.500 -0.2341 0.01142 0.00592 -0.1085 0.9801 0.0500
-5.250 -0.2021 0.01134 0.00585 -0.1095 0.9798 0.0510
-5.000 -0.1687 0.01117 0.00570 -0.1109 0.9796 0.0523
-4.750 -0.1357 0.01105 0.00561 -0.1121 0.9794 0.0536
-4.500 -0.1026 0.01093 0.00552 -0.1133 0.9792 0.0549
-4.250 -0.0692 0.01082 0.00543 -0.1146 0.9789 0.0559
-4.000 -0.0359 0.01072 0.00535 -0.1158 0.9787 0.0566
-3.750 -0.0026 0.01062 0.00527 -0.1171 0.9785 0.0574
-3.500 0.0324 0.01046 0.00514 -0.1187 0.9783 0.0588
-3.250 0.0726 0.01011 0.00483 -0.1214 0.9750 0.0599
-3.000 0.1554 0.00915 0.00389 -0.1336 0.9726 0.0621
-2.750 0.0907 0.01023 0.00499 -0.1128 0.9392 0.0615
-2.500 0.1376 0.00965 0.00444 -0.1167 0.9338 0.0627
-2.250 0.2506 0.00819 0.00294 -0.1353 0.9252 0.0641
-2.000 0.2892 0.00807 0.00277 -0.1376 0.8953 0.0653
-1.750 0.2918 0.01043 0.00312 -0.1320 0.4100 0.0660
-1.500 0.3196 0.01083 0.00318 -0.1321 0.3129 0.0674
-1.250 0.3484 0.01113 0.00323 -0.1323 0.2406 0.0695
-0.750 0.4095 0.01150 0.00334 -0.1337 0.1341 0.1166
-0.500 0.4424 0.01158 0.00341 -0.1350 0.0946 0.1683
-0.250 0.4973 0.01064 0.00331 -0.1426 0.0800 0.4816
0.000 0.5324 0.01057 0.00358 -0.1443 0.0722 0.6188
0.250 0.5611 0.01074 0.00370 -0.1443 0.0673 0.6293
0.500 0.5893 0.01094 0.00388 -0.1441 0.0618 0.6353
0.750 0.6176 0.01112 0.00403 -0.1440 0.0580 0.6403
1.000 0.6460 0.01130 0.00417 -0.1438 0.0545 0.6441
1.250 0.6744 0.01149 0.00431 -0.1437 0.0514 0.6471
1.500 0.7027 0.01166 0.00447 -0.1436 0.0495 0.6500
1.750 0.7303 0.01187 0.00468 -0.1433 0.0469 0.6536
2.000 0.7581 0.01210 0.00487 -0.1430 0.0443 0.6556
2.250 0.7862 0.01227 0.00503 -0.1428 0.0429 0.6571
2.500 0.8142 0.01245 0.00520 -0.1427 0.0411 0.6586
2.750 0.8420 0.01267 0.00539 -0.1424 0.0393 0.6604
3.000 0.8697 0.01290 0.00560 -0.1422 0.0378 0.6622
3.250 0.8976 0.01309 0.00578 -0.1420 0.0369 0.6635
3.500 0.9253 0.01330 0.00599 -0.1417 0.0358 0.6652
3.750 0.9529 0.01352 0.00619 -0.1414 0.0346 0.6662
4.000 0.9805 0.01375 0.00640 -0.1412 0.0336 0.6668
4.250 1.0079 0.01400 0.00663 -0.1409 0.0324 0.6672
4.500 1.0355 0.01420 0.00684 -0.1406 0.0319 0.6678
4.750 1.0629 0.01441 0.00706 -0.1403 0.0312 0.6684
5.000 1.0901 0.01464 0.00730 -0.1400 0.0305 0.6690
5.250 1.1172 0.01487 0.00754 -0.1397 0.0297 0.6695
5.500 1.1441 0.01513 0.00780 -0.1393 0.0289 0.6700
5.750 1.1708 0.01541 0.00808 -0.1389 0.0281 0.6705
6.000 1.1973 0.01572 0.00839 -0.1384 0.0273 0.6710
6.250 1.2238 0.01599 0.00868 -0.1379 0.0269 0.6716
6.500 1.2501 0.01627 0.00899 -0.1374 0.0264 0.6722
6.750 1.2763 0.01657 0.00932 -0.1369 0.0259 0.6728
7.000 1.3023 0.01687 0.00964 -0.1363 0.0253 0.6734
7.250 1.3281 0.01719 0.00997 -0.1357 0.0248 0.6740
7.500 1.3537 0.01752 0.01032 -0.1351 0.0242 0.6745
7.750 1.3790 0.01789 0.01070 -0.1344 0.0237 0.6750
8.000 1.4038 0.01831 0.01114 -0.1337 0.0232 0.6755
8.250 1.4288 0.01868 0.01155 -0.1329 0.0229 0.6761
8.500 1.4535 0.01907 0.01198 -0.1322 0.0226 0.6766
8.750 1.4779 0.01945 0.01241 -0.1313 0.0223 0.6772
9.000 1.5021 0.01986 0.01286 -0.1305 0.0220 0.6777
9.250 1.5260 0.02028 0.01332 -0.1295 0.0217 0.6783
9.500 1.5496 0.02071 0.01379 -0.1286 0.0214 0.6789
9.750 1.5729 0.02116 0.01428 -0.1276 0.0211 0.6794
10.000 1.5958 0.02162 0.01479 -0.1265 0.0208 0.6800
10.250 1.6183 0.02211 0.01531 -0.1254 0.0205 0.6806
10.500 1.6405 0.02261 0.01585 -0.1242 0.0203 0.6811
10.750 1.6620 0.02315 0.01643 -0.1229 0.0199 0.6817
11.000 1.6825 0.02376 0.01709 -0.1214 0.0195 0.6822
11.250 1.7024 0.02440 0.01778 -0.1198 0.0192 0.6827
11.500 1.7225 0.02495 0.01840 -0.1183 0.0191 0.6833
11.750 1.7417 0.02553 0.01905 -0.1166 0.0189 0.6839
12.000 1.7605 0.02611 0.01969 -0.1149 0.0187 0.6844
12.250 1.7779 0.02675 0.02041 -0.1129 0.0185 0.6848
12.500 1.7944 0.02741 0.02115 -0.1107 0.0184 0.6852
12.750 1.8098 0.02811 0.02192 -0.1084 0.0182 0.6855
13.000 1.8244 0.02883 0.02272 -0.1060 0.0180 0.6860
13.250 1.8379 0.02958 0.02355 -0.1035 0.0179 0.6867
13.500 1.8499 0.03039 0.02444 -0.1007 0.0177 0.6875
13.750 1.8583 0.03120 0.02535 -0.0972 0.0175 0.6882
14.000 1.8664 0.03212 0.02635 -0.0939 0.0174 0.6889
14.250 1.8742 0.03313 0.02745 -0.0906 0.0173 0.6896
14.500 1.8816 0.03420 0.02862 -0.0874 0.0172 0.6902
14.750 1.8884 0.03533 0.02983 -0.0842 0.0170 0.6908
15.000 1.8936 0.03660 0.03120 -0.0810 0.0169 0.6915
15.250 1.8982 0.03794 0.03263 -0.0778 0.0167 0.6921
15.500 1.9007 0.03947 0.03427 -0.0745 0.0167 0.6927
15.750 1.9020 0.04114 0.03604 -0.0713 0.0165 0.6933
16.000 1.9014 0.04303 0.03804 -0.0682 0.0164 0.6939
16.250 1.8987 0.04519 0.04032 -0.0653 0.0163 0.6944
16.500 1.8940 0.04765 0.04291 -0.0625 0.0162 0.6950
16.750 1.8860 0.05060 0.04599 -0.0601 0.0161 0.6955
17.000 1.8754 0.05405 0.04958 -0.0582 0.0160 0.6960
17.250 1.8618 0.05817 0.05385 -0.0571 0.0159 0.6964
17.500 1.8419 0.06367 0.05952 -0.0573 0.0158 0.6968
17.750 1.8202 0.07034 0.06638 -0.0594 0.0158 0.6972
18.000 1.7901 0.07964 0.07591 -0.0643 0.0158 0.6975
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