DSMA-523A AIRFOIL (dsma523a-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: DSMA-523A AIRFOIL (dsma523a-il) Reynolds number: 1,000,000 Max Cl/Cd: 77.55 at α=7.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-dsma523a-il-1000000-n5.txt Download as CSV file: xf-dsma523a-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: DSMA-523A 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 -0.9947 0.12346 0.12058 -0.0490 0.9849 0.0162
-19.500 -1.0406 0.11093 0.10787 -0.0559 0.9852 0.0162
-19.250 -1.0844 0.09929 0.09606 -0.0624 0.9854 0.0162
-19.000 -1.1223 0.08893 0.08554 -0.0681 0.9857 0.0162
-18.750 -1.1532 0.08009 0.07654 -0.0729 0.9860 0.0161
-18.500 -1.1775 0.07257 0.06887 -0.0770 0.9864 0.0161
-18.250 -1.1950 0.06637 0.06254 -0.0802 0.9867 0.0162
-18.000 -1.2078 0.06118 0.05722 -0.0827 0.9871 0.0162
-17.750 -1.2172 0.05676 0.05268 -0.0846 0.9874 0.0162
-17.500 -1.2237 0.05295 0.04876 -0.0859 0.9877 0.0163
-17.250 -1.2282 0.04963 0.04534 -0.0868 0.9880 0.0163
-17.000 -1.2302 0.04678 0.04240 -0.0873 0.9883 0.0163
-16.750 -1.2312 0.04424 0.03978 -0.0874 0.9885 0.0164
-16.500 -1.2351 0.04172 0.03717 -0.0870 0.9887 0.0165
-16.250 -1.2381 0.03953 0.03490 -0.0861 0.9889 0.0166
-16.000 -1.2393 0.03761 0.03291 -0.0850 0.9891 0.0167
-15.750 -1.2391 0.03590 0.03113 -0.0837 0.9892 0.0168
-15.500 -1.2376 0.03435 0.02952 -0.0824 0.9894 0.0169
-15.250 -1.2341 0.03297 0.02808 -0.0811 0.9895 0.0171
-15.000 -1.2298 0.03167 0.02672 -0.0797 0.9896 0.0172
-14.750 -1.2240 0.03050 0.02550 -0.0783 0.9897 0.0173
-14.500 -1.2174 0.02940 0.02435 -0.0769 0.9898 0.0175
-14.250 -1.2102 0.02836 0.02326 -0.0754 0.9898 0.0176
-14.000 -1.2004 0.02740 0.02227 -0.0742 0.9897 0.0178
-13.750 -1.1905 0.02647 0.02129 -0.0730 0.9895 0.0180
-13.500 -1.1803 0.02558 0.02036 -0.0717 0.9893 0.0181
-13.250 -1.1700 0.02479 0.01953 -0.0702 0.9891 0.0183
-13.000 -1.1586 0.02402 0.01871 -0.0689 0.9887 0.0185
-12.750 -1.1435 0.02329 0.01793 -0.0682 0.9880 0.0188
-12.500 -1.1257 0.02257 0.01717 -0.0679 0.9873 0.0190
-12.250 -1.1047 0.02185 0.01641 -0.0681 0.9868 0.0193
-12.000 -1.0830 0.02118 0.01570 -0.0683 0.9864 0.0195
-11.750 -1.0601 0.02052 0.01500 -0.0688 0.9861 0.0198
-11.500 -1.0366 0.01979 0.01424 -0.0695 0.9857 0.0202
-11.250 -1.0165 0.01916 0.01360 -0.0692 0.9851 0.0205
-11.000 -0.9982 0.01859 0.01300 -0.0685 0.9841 0.0209
-10.750 -0.9756 0.01803 0.01243 -0.0686 0.9833 0.0212
-10.500 -0.9507 0.01751 0.01189 -0.0690 0.9825 0.0216
-10.250 -0.9233 0.01700 0.01136 -0.0699 0.9818 0.0221
-10.000 -0.8953 0.01652 0.01086 -0.0708 0.9812 0.0225
-9.750 -0.8664 0.01607 0.01038 -0.0719 0.9807 0.0229
-9.500 -0.8363 0.01564 0.00993 -0.0732 0.9803 0.0233
-9.250 -0.8056 0.01516 0.00944 -0.0746 0.9798 0.0239
-9.000 -0.7745 0.01472 0.00901 -0.0760 0.9795 0.0246
-8.750 -0.7433 0.01433 0.00862 -0.0774 0.9791 0.0254
-8.500 -0.7119 0.01398 0.00825 -0.0787 0.9789 0.0261
-8.250 -0.6802 0.01365 0.00791 -0.0801 0.9786 0.0268
-8.000 -0.6530 0.01334 0.00759 -0.0804 0.9776 0.0274
-7.750 -0.6251 0.01300 0.00726 -0.0809 0.9764 0.0284
-7.500 -0.5950 0.01269 0.00696 -0.0818 0.9757 0.0295
-7.250 -0.5641 0.01242 0.00669 -0.0828 0.9751 0.0306
-7.000 -0.5327 0.01216 0.00644 -0.0839 0.9747 0.0317
-6.750 -0.5007 0.01190 0.00621 -0.0851 0.9742 0.0336
-6.500 -0.4684 0.01167 0.00600 -0.0864 0.9739 0.0356
-6.250 -0.4359 0.01147 0.00585 -0.0876 0.9735 0.0381
-6.000 -0.4036 0.01129 0.00570 -0.0887 0.9732 0.0410
-5.750 -0.3715 0.01115 0.00560 -0.0897 0.9729 0.0436
-5.500 -0.3392 0.01102 0.00547 -0.0908 0.9726 0.0459
-5.250 -0.3067 0.01088 0.00535 -0.0919 0.9724 0.0475
-5.000 -0.2802 0.01077 0.00527 -0.0917 0.9706 0.0493
-4.750 -0.2498 0.01067 0.00519 -0.0923 0.9696 0.0511
-4.500 -0.2182 0.01058 0.00511 -0.0932 0.9690 0.0522
-4.250 -0.1849 0.01036 0.00492 -0.0945 0.9686 0.0536
-4.000 -0.1521 0.01020 0.00479 -0.0957 0.9682 0.0548
-3.750 -0.1194 0.01006 0.00467 -0.0968 0.9679 0.0560
-3.500 -0.0865 0.00992 0.00456 -0.0979 0.9676 0.0569
-3.250 -0.0535 0.00980 0.00446 -0.0991 0.9673 0.0577
-3.000 -0.0163 0.00964 0.00432 -0.1011 0.9670 0.0585
-2.750 -0.0359 0.00955 0.00423 -0.0909 0.9442 0.0587
-2.500 0.0024 0.00904 0.00375 -0.0929 0.9362 0.0601
-2.250 0.0477 0.00854 0.00329 -0.0964 0.9322 0.0617
-2.000 0.1103 0.00792 0.00268 -0.1035 0.9275 0.0628
-1.750 0.1843 0.00760 0.00228 -0.1133 0.9130 0.0639
-1.500 0.2039 0.00773 0.00217 -0.1112 0.8180 0.0646
-1.250 0.2070 0.00940 0.00242 -0.1060 0.4730 0.0651
-1.000 0.2318 0.00993 0.00249 -0.1055 0.3445 0.0664
-0.750 0.2594 0.01020 0.00252 -0.1056 0.2722 0.0682
-0.500 0.2877 0.01042 0.00254 -0.1057 0.2136 0.0710
-0.250 0.3177 0.01057 0.00258 -0.1064 0.1577 0.1035
0.000 0.3472 0.01073 0.00263 -0.1068 0.1131 0.1228
0.250 0.4157 0.00915 0.00238 -0.1182 0.0845 0.6102
0.500 0.4439 0.00934 0.00256 -0.1181 0.0756 0.6298
0.750 0.4719 0.00952 0.00271 -0.1179 0.0699 0.6372
1.000 0.5002 0.00969 0.00283 -0.1177 0.0646 0.6428
1.250 0.5284 0.00984 0.00295 -0.1176 0.0609 0.6465
1.500 0.5561 0.01004 0.00312 -0.1173 0.0566 0.6499
1.750 0.5837 0.01024 0.00331 -0.1170 0.0537 0.6548
2.000 0.6115 0.01044 0.00346 -0.1167 0.0507 0.6585
2.250 0.6394 0.01064 0.00361 -0.1165 0.0479 0.6612
2.500 0.6674 0.01081 0.00376 -0.1163 0.0462 0.6629
2.750 0.6949 0.01099 0.00394 -0.1160 0.0443 0.6646
3.000 0.7221 0.01121 0.00414 -0.1157 0.0425 0.6664
3.250 0.7494 0.01143 0.00435 -0.1153 0.0410 0.6678
3.500 0.7770 0.01161 0.00453 -0.1150 0.0400 0.6689
3.750 0.8043 0.01181 0.00474 -0.1147 0.0389 0.6705
4.000 0.8313 0.01204 0.00496 -0.1143 0.0378 0.6727
4.250 0.8583 0.01229 0.00520 -0.1139 0.0366 0.6750
4.500 0.8853 0.01255 0.00543 -0.1135 0.0352 0.6759
4.750 0.9128 0.01274 0.00562 -0.1133 0.0345 0.6766
5.000 0.9400 0.01294 0.00583 -0.1130 0.0336 0.6772
5.250 0.9672 0.01316 0.00604 -0.1127 0.0326 0.6777
5.500 0.9941 0.01339 0.00625 -0.1123 0.0316 0.6781
5.750 1.0208 0.01366 0.00650 -0.1119 0.0306 0.6785
6.000 1.0474 0.01393 0.00679 -0.1115 0.0299 0.6788
6.250 1.0741 0.01417 0.00704 -0.1111 0.0294 0.6791
6.500 1.1006 0.01443 0.00731 -0.1107 0.0288 0.6794
6.750 1.1271 0.01468 0.00757 -0.1102 0.0281 0.6800
7.000 1.1534 0.01494 0.00784 -0.1098 0.0274 0.6807
7.250 1.1794 0.01522 0.00813 -0.1093 0.0268 0.6813
7.500 1.2051 0.01554 0.00845 -0.1087 0.0262 0.6818
7.750 1.2303 0.01592 0.00885 -0.1081 0.0255 0.6823
8.000 1.2558 0.01622 0.00919 -0.1075 0.0252 0.6829
8.250 1.2811 0.01655 0.00955 -0.1069 0.0249 0.6834
8.500 1.3062 0.01688 0.00993 -0.1062 0.0244 0.6838
8.750 1.3310 0.01724 0.01032 -0.1055 0.0240 0.6844
9.000 1.3556 0.01760 0.01071 -0.1048 0.0236 0.6850
9.250 1.3800 0.01798 0.01112 -0.1040 0.0232 0.6856
9.500 1.4041 0.01837 0.01154 -0.1032 0.0228 0.6862
9.750 1.4279 0.01878 0.01198 -0.1023 0.0225 0.6868
10.000 1.4512 0.01923 0.01246 -0.1014 0.0220 0.6873
10.250 1.4738 0.01976 0.01302 -0.1004 0.0216 0.6878
10.500 1.4963 0.02026 0.01357 -0.0993 0.0213 0.6883
10.750 1.5189 0.02071 0.01407 -0.0983 0.0211 0.6889
11.000 1.5411 0.02118 0.01461 -0.0972 0.0209 0.6894
11.250 1.5628 0.02168 0.01517 -0.0960 0.0207 0.6900
11.500 1.5840 0.02221 0.01575 -0.0948 0.0204 0.6905
11.750 1.6053 0.02269 0.01629 -0.0936 0.0201 0.6910
12.000 1.6258 0.02322 0.01688 -0.0922 0.0198 0.6916
12.250 1.6457 0.02377 0.01748 -0.0908 0.0196 0.6921
12.500 1.6650 0.02435 0.01811 -0.0893 0.0193 0.6926
12.750 1.6835 0.02496 0.01878 -0.0877 0.0191 0.6931
13.000 1.7011 0.02561 0.01948 -0.0860 0.0188 0.6937
13.250 1.7175 0.02631 0.02024 -0.0841 0.0187 0.6941
13.500 1.7328 0.02704 0.02104 -0.0820 0.0185 0.6946
13.750 1.7435 0.02780 0.02187 -0.0791 0.0183 0.6950
14.000 1.7528 0.02866 0.02281 -0.0761 0.0181 0.6954
14.250 1.7611 0.02964 0.02386 -0.0731 0.0179 0.6958
14.500 1.7681 0.03071 0.02503 -0.0699 0.0178 0.6962
14.750 1.7769 0.03166 0.02608 -0.0672 0.0177 0.6965
15.000 1.7844 0.03272 0.02723 -0.0643 0.0176 0.6968
15.250 1.7909 0.03385 0.02846 -0.0615 0.0176 0.6971
15.500 1.7964 0.03509 0.02979 -0.0586 0.0175 0.6974
15.750 1.8008 0.03643 0.03124 -0.0559 0.0174 0.6981
16.000 1.8039 0.03793 0.03286 -0.0532 0.0173 0.6989
16.250 1.8053 0.03961 0.03465 -0.0506 0.0173 0.6996
16.500 1.8053 0.04150 0.03666 -0.0482 0.0172 0.7001
16.750 1.8034 0.04365 0.03893 -0.0460 0.0171 0.7006
17.000 1.7998 0.04608 0.04149 -0.0441 0.0171 0.7011
17.250 1.7935 0.04900 0.04454 -0.0427 0.0170 0.7015
17.500 1.7843 0.05247 0.04816 -0.0418 0.0169 0.7019
17.750 1.7735 0.05653 0.05236 -0.0419 0.0169 0.7023
18.000 1.7567 0.06196 0.05797 -0.0433 0.0168 0.7026
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