DORNIER A-5 AIRFOIL (doa5-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: DORNIER A-5 AIRFOIL (doa5-il) Reynolds number: 1,000,000 Max Cl/Cd: 87.62 at α=1.75° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-doa5-il-1000000.txt Download as CSV file: xf-doa5-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: DORNIER A-5 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
------ -------- --------- --------- -------- -------- --------
-18.000 -0.9165 0.08478 0.08214 -0.0769 1.0000 0.0206
-17.750 -0.9510 0.07621 0.07337 -0.0810 1.0000 0.0206
-17.500 -0.9706 0.07062 0.06764 -0.0830 1.0000 0.0207
-17.250 -0.9898 0.06547 0.06236 -0.0845 1.0000 0.0208
-17.000 -0.9969 0.06222 0.05903 -0.0850 1.0000 0.0210
-16.750 -1.0077 0.05877 0.05547 -0.0852 1.0000 0.0212
-16.500 -1.0219 0.05517 0.05174 -0.0850 1.0000 0.0212
-16.250 -1.0272 0.05189 0.04833 -0.0858 0.9997 0.0213
-16.000 -1.0231 0.04894 0.04524 -0.0878 0.9989 0.0216
-15.750 -1.0162 0.04643 0.04261 -0.0896 0.9978 0.0218
-15.500 -1.0094 0.04398 0.04003 -0.0912 0.9967 0.0219
-15.250 -0.9981 0.04212 0.03806 -0.0928 0.9955 0.0221
-15.000 -0.9969 0.03900 0.03474 -0.0939 0.9945 0.0224
-14.750 -0.9878 0.03665 0.03227 -0.0948 0.9938 0.0227
-14.500 -0.9761 0.03511 0.03069 -0.0950 0.9919 0.0229
-14.250 -0.9606 0.03389 0.02945 -0.0957 0.9901 0.0232
-14.000 -0.9442 0.03264 0.02815 -0.0965 0.9885 0.0234
-13.750 -0.9255 0.03156 0.02703 -0.0975 0.9871 0.0238
-13.500 -0.9062 0.03037 0.02576 -0.0986 0.9860 0.0241
-13.250 -0.8853 0.02922 0.02454 -0.0997 0.9850 0.0243
-13.000 -0.8629 0.02816 0.02341 -0.1010 0.9843 0.0246
-12.750 -0.8396 0.02708 0.02225 -0.1022 0.9837 0.0249
-12.500 -0.8283 0.02622 0.02133 -0.1008 0.9794 0.0252
-12.250 -0.8062 0.02532 0.02037 -0.1014 0.9775 0.0255
-12.000 -0.7816 0.02447 0.01945 -0.1025 0.9760 0.0258
-11.750 -0.7554 0.02369 0.01859 -0.1038 0.9749 0.0260
-11.500 -0.7301 0.02255 0.01738 -0.1045 0.9741 0.0265
-11.250 -0.7038 0.02161 0.01642 -0.1055 0.9734 0.0269
-11.000 -0.6758 0.02087 0.01568 -0.1069 0.9727 0.0274
-10.750 -0.6605 0.02025 0.01505 -0.1057 0.9684 0.0277
-10.500 -0.6359 0.01957 0.01434 -0.1062 0.9663 0.0280
-10.250 -0.6089 0.01889 0.01364 -0.1072 0.9648 0.0284
-10.000 -0.5806 0.01822 0.01294 -0.1084 0.9637 0.0288
-9.750 -0.5507 0.01761 0.01230 -0.1099 0.9626 0.0294
-9.500 -0.5197 0.01702 0.01168 -0.1116 0.9617 0.0298
-9.250 -0.4871 0.01647 0.01110 -0.1135 0.9607 0.0302
-9.000 -0.4734 0.01599 0.01059 -0.1116 0.9542 0.0304
-8.750 -0.4480 0.01508 0.00965 -0.1126 0.9509 0.0311
-8.500 -0.4159 0.01429 0.00885 -0.1149 0.9488 0.0318
-8.250 -0.3811 0.01367 0.00823 -0.1175 0.9470 0.0325
-8.000 -0.3759 0.01322 0.00775 -0.1139 0.9371 0.0328
-7.750 -0.3433 0.01271 0.00721 -0.1158 0.9341 0.0337
-7.500 -0.3220 0.01233 0.00681 -0.1152 0.9277 0.0344
-7.250 -0.2941 0.01193 0.00637 -0.1159 0.9226 0.0350
-7.000 -0.2606 0.01148 0.00588 -0.1178 0.9190 0.0359
-6.750 -0.2437 0.01108 0.00545 -0.1162 0.9116 0.0370
-6.500 -0.2163 0.01075 0.00511 -0.1167 0.9066 0.0384
-6.250 -0.1843 0.01047 0.00479 -0.1181 0.9023 0.0399
-6.000 -0.1688 0.01028 0.00458 -0.1158 0.8943 0.0409
-5.750 -0.1425 0.00995 0.00422 -0.1159 0.8878 0.0436
-5.500 -0.1247 0.00973 0.00401 -0.1140 0.8785 0.0460
-5.250 -0.0993 0.00949 0.00374 -0.1138 0.8707 0.0501
-5.000 -0.0777 0.00927 0.00356 -0.1127 0.8642 0.0563
-4.750 -0.0530 0.00905 0.00336 -0.1123 0.8578 0.0665
-4.500 -0.0270 0.00889 0.00319 -0.1122 0.8528 0.0745
-4.250 -0.0027 0.00868 0.00301 -0.1117 0.8470 0.0838
-4.000 0.0235 0.00849 0.00283 -0.1116 0.8414 0.0974
-3.750 0.0483 0.00821 0.00266 -0.1113 0.8367 0.1302
-3.500 0.0713 0.00788 0.00249 -0.1107 0.8319 0.1798
-3.250 0.0821 0.00631 0.00186 -0.1089 0.8264 0.4550
-3.000 0.1096 0.00607 0.00177 -0.1091 0.8216 0.5140
-2.750 0.1343 0.00597 0.00174 -0.1084 0.8177 0.5385
-2.500 0.1604 0.00591 0.00172 -0.1081 0.8135 0.5569
-2.250 0.1882 0.00589 0.00171 -0.1081 0.8089 0.5750
-2.000 0.2158 0.00590 0.00171 -0.1080 0.8027 0.5903
-1.750 0.2400 0.00587 0.00171 -0.1072 0.7967 0.6039
-1.500 0.2666 0.00587 0.00171 -0.1069 0.7906 0.6133
-1.250 0.2937 0.00589 0.00171 -0.1066 0.7850 0.6204
-1.000 0.3189 0.00588 0.00169 -0.1060 0.7794 0.6255
-0.750 0.3449 0.00587 0.00169 -0.1056 0.7734 0.6316
-0.500 0.3713 0.00588 0.00169 -0.1052 0.7677 0.6377
-0.250 0.3962 0.00587 0.00168 -0.1045 0.7598 0.6423
0.000 0.4210 0.00588 0.00168 -0.1038 0.7520 0.6472
0.250 0.4455 0.00588 0.00169 -0.1031 0.7425 0.6518
0.500 0.4688 0.00592 0.00168 -0.1020 0.7307 0.6571
0.750 0.4901 0.00598 0.00171 -0.1005 0.7162 0.6625
1.000 0.5115 0.00606 0.00175 -0.0991 0.7008 0.6676
1.250 0.5323 0.00616 0.00178 -0.0975 0.6822 0.6733
1.500 0.5493 0.00627 0.00182 -0.0951 0.6613 0.6774
1.750 0.5643 0.00644 0.00191 -0.0922 0.6365 0.6817
2.000 0.5802 0.00665 0.00201 -0.0896 0.6058 0.6858
2.250 0.5941 0.00692 0.00212 -0.0867 0.5720 0.6898
2.500 0.6073 0.00724 0.00229 -0.0836 0.5349 0.6938
2.750 0.6135 0.00779 0.00256 -0.0792 0.4659 0.6975
3.000 0.6226 0.00836 0.00286 -0.0756 0.4053 0.7008
3.250 0.6403 0.00869 0.00307 -0.0736 0.3797 0.7042
3.500 0.6588 0.00899 0.00326 -0.0718 0.3567 0.7073
3.750 0.6784 0.00923 0.00343 -0.0702 0.3398 0.7103
4.000 0.6998 0.00942 0.00361 -0.0690 0.3285 0.7130
4.250 0.7204 0.00966 0.00380 -0.0676 0.3164 0.7157
4.500 0.7419 0.00986 0.00397 -0.0664 0.3049 0.7186
4.750 0.7627 0.01008 0.00416 -0.0651 0.2920 0.7216
5.000 0.7827 0.01035 0.00434 -0.0637 0.2750 0.7243
5.250 0.7995 0.01071 0.00457 -0.0618 0.2441 0.7268
5.500 0.8106 0.01130 0.00494 -0.0588 0.2003 0.7291
5.750 0.8273 0.01169 0.00527 -0.0568 0.1819 0.7314
6.000 0.8459 0.01203 0.00555 -0.0553 0.1705 0.7338
6.250 0.8658 0.01232 0.00582 -0.0539 0.1637 0.7362
6.500 0.8848 0.01263 0.00610 -0.0524 0.1575 0.7386
6.750 0.9045 0.01293 0.00638 -0.0511 0.1520 0.7408
7.000 0.9253 0.01315 0.00662 -0.0499 0.1488 0.7432
7.250 0.9447 0.01344 0.00692 -0.0486 0.1440 0.7453
7.500 0.9626 0.01380 0.00728 -0.0470 0.1381 0.7474
7.750 0.9836 0.01403 0.00754 -0.0459 0.1347 0.7497
8.000 1.0031 0.01433 0.00783 -0.0446 0.1271 0.7519
8.250 1.0222 0.01466 0.00814 -0.0433 0.1203 0.7540
8.500 1.0404 0.01504 0.00846 -0.0419 0.1109 0.7559
8.750 1.0583 0.01544 0.00882 -0.0404 0.1052 0.7574
9.000 1.0752 0.01583 0.00918 -0.0388 0.1000 0.7593
9.250 1.0921 0.01622 0.00960 -0.0373 0.0960 0.7611
9.500 1.1098 0.01660 0.01001 -0.0358 0.0935 0.7629
9.750 1.1264 0.01705 0.01046 -0.0343 0.0903 0.7647
10.000 1.1407 0.01762 0.01103 -0.0324 0.0860 0.7668
10.250 1.1585 0.01802 0.01147 -0.0311 0.0841 0.7687
10.500 1.1768 0.01840 0.01188 -0.0299 0.0818 0.7706
10.750 1.1940 0.01886 0.01235 -0.0286 0.0792 0.7722
11.000 1.2087 0.01943 0.01292 -0.0269 0.0758 0.7736
11.250 1.2245 0.01990 0.01342 -0.0255 0.0735 0.7755
11.500 1.2419 0.02033 0.01388 -0.0243 0.0713 0.7770
11.750 1.2574 0.02086 0.01443 -0.0229 0.0689 0.7786
12.000 1.2709 0.02152 0.01508 -0.0212 0.0656 0.7804
12.250 1.2862 0.02209 0.01570 -0.0199 0.0639 0.7822
12.500 1.3012 0.02269 0.01633 -0.0185 0.0622 0.7840
12.750 1.3149 0.02339 0.01703 -0.0171 0.0599 0.7856
13.000 1.3261 0.02425 0.01789 -0.0154 0.0572 0.7869
13.250 1.3404 0.02494 0.01863 -0.0141 0.0557 0.7880
13.500 1.3548 0.02562 0.01936 -0.0129 0.0540 0.7891
13.750 1.3676 0.02640 0.02016 -0.0116 0.0519 0.7908
14.000 1.3774 0.02740 0.02118 -0.0100 0.0496 0.7923
14.250 1.3904 0.02821 0.02205 -0.0088 0.0481 0.7938
14.500 1.4034 0.02904 0.02293 -0.0077 0.0462 0.7954
14.750 1.4138 0.03006 0.02397 -0.0064 0.0442 0.7969
15.000 1.4231 0.03120 0.02514 -0.0050 0.0422 0.7982
15.250 1.4346 0.03220 0.02619 -0.0039 0.0406 0.7995
15.500 1.4447 0.03333 0.02735 -0.0028 0.0389 0.8007
15.750 1.4512 0.03477 0.02879 -0.0015 0.0369 0.8019
16.000 1.4602 0.03604 0.03012 -0.0005 0.0357 0.8030
16.250 1.4680 0.03744 0.03157 0.0006 0.0344 0.8040
16.500 1.4741 0.03903 0.03320 0.0016 0.0331 0.8057
16.750 1.4771 0.04093 0.03515 0.0026 0.0316 0.8073
17.000 1.4843 0.04251 0.03681 0.0033 0.0308 0.8087
17.250 1.4901 0.04426 0.03863 0.0040 0.0297 0.8100
17.500 1.4936 0.04629 0.04073 0.0046 0.0288 0.8112
17.750 1.4942 0.04866 0.04315 0.0052 0.0276 0.8126
18.000 1.4948 0.05113 0.04569 0.0056 0.0267 0.8140
18.250 1.4990 0.05329 0.04794 0.0058 0.0260 0.8152
18.500 1.5005 0.05580 0.05053 0.0059 0.0253 0.8166
18.750 1.4994 0.05868 0.05348 0.0058 0.0246 0.8178
19.000 1.4951 0.06205 0.05692 0.0055 0.0238 0.8187
19.250 1.4887 0.06580 0.06076 0.0049 0.0232 0.8195
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