DORNIER A-5 AIRFOIL (doa5-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: DORNIER A-5 AIRFOIL (doa5-il) Reynolds number: 1,000,000 Max Cl/Cd: 68.73 at α=6.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-doa5-il-1000000-n5.txt Download as CSV file: xf-doa5-il-1000000-n5.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 = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -1.0826 0.08017 0.07696 -0.0819 1.0000 0.0172
-19.500 -1.0957 0.07489 0.07156 -0.0844 0.9999 0.0173
-19.250 -1.1007 0.07035 0.06691 -0.0872 0.9996 0.0174
-19.000 -1.1004 0.06667 0.06315 -0.0894 0.9993 0.0176
-18.750 -1.1020 0.06288 0.05926 -0.0916 0.9990 0.0177
-18.500 -1.1031 0.05924 0.05551 -0.0936 0.9985 0.0178
-18.250 -1.0986 0.05637 0.05256 -0.0953 0.9980 0.0180
-18.000 -1.0943 0.05357 0.04967 -0.0968 0.9974 0.0182
-17.750 -1.0879 0.05107 0.04709 -0.0982 0.9967 0.0184
-17.500 -1.0796 0.04881 0.04474 -0.0994 0.9960 0.0186
-17.250 -1.0709 0.04664 0.04248 -0.1006 0.9952 0.0187
-17.000 -1.0610 0.04463 0.04039 -0.1017 0.9945 0.0189
-16.500 -1.0401 0.04096 0.03655 -0.1032 0.9927 0.0191
-16.250 -1.0290 0.03935 0.03487 -0.1036 0.9915 0.0192
-16.000 -1.0187 0.03762 0.03306 -0.1042 0.9900 0.0193
-15.750 -1.0106 0.03571 0.03109 -0.1046 0.9886 0.0197
-15.500 -0.9980 0.03420 0.02952 -0.1052 0.9872 0.0198
-15.250 -0.9825 0.03291 0.02820 -0.1059 0.9859 0.0201
-15.000 -0.9671 0.03162 0.02686 -0.1066 0.9848 0.0202
-14.750 -0.9484 0.03058 0.02578 -0.1074 0.9839 0.0204
-14.500 -0.9319 0.02955 0.02470 -0.1077 0.9825 0.0207
-14.250 -0.9188 0.02861 0.02373 -0.1071 0.9800 0.0209
-14.000 -0.9031 0.02757 0.02263 -0.1072 0.9781 0.0210
-13.750 -0.8842 0.02666 0.02168 -0.1076 0.9765 0.0213
-13.500 -0.8644 0.02575 0.02072 -0.1082 0.9752 0.0215
-13.250 -0.8437 0.02486 0.01978 -0.1088 0.9741 0.0217
-13.000 -0.8210 0.02410 0.01898 -0.1096 0.9731 0.0221
-12.750 -0.7985 0.02326 0.01809 -0.1104 0.9723 0.0223
-12.500 -0.7820 0.02252 0.01730 -0.1099 0.9694 0.0224
-12.250 -0.7611 0.02180 0.01654 -0.1101 0.9672 0.0226
-12.000 -0.7383 0.02106 0.01575 -0.1107 0.9652 0.0227
-11.750 -0.7117 0.02039 0.01504 -0.1119 0.9636 0.0229
-11.500 -0.6857 0.01954 0.01416 -0.1134 0.9621 0.0232
-11.000 -0.6458 0.01816 0.01273 -0.1133 0.9544 0.0239
-10.750 -0.6224 0.01755 0.01209 -0.1138 0.9508 0.0241
-10.500 -0.5940 0.01695 0.01147 -0.1153 0.9485 0.0244
-10.250 -0.5816 0.01649 0.01098 -0.1133 0.9404 0.0247
-10.000 -0.5542 0.01594 0.01041 -0.1144 0.9359 0.0250
-9.750 -0.5294 0.01543 0.00987 -0.1150 0.9308 0.0253
-9.500 -0.4984 0.01491 0.00932 -0.1167 0.9263 0.0256
-9.250 -0.4623 0.01442 0.00878 -0.1195 0.9228 0.0260
-9.000 -0.4338 0.01395 0.00828 -0.1208 0.9177 0.0262
-8.750 -0.4053 0.01352 0.00781 -0.1219 0.9123 0.0267
-8.500 -0.3752 0.01312 0.00736 -0.1233 0.9077 0.0270
-8.250 -0.3623 0.01263 0.00684 -0.1215 0.9001 0.0274
-8.000 -0.3444 0.01221 0.00637 -0.1205 0.8932 0.0279
-7.750 -0.3287 0.01187 0.00601 -0.1189 0.8858 0.0282
-7.500 -0.3095 0.01156 0.00568 -0.1177 0.8772 0.0288
-7.250 -0.2906 0.01130 0.00539 -0.1164 0.8673 0.0293
-7.000 -0.2693 0.01106 0.00510 -0.1156 0.8571 0.0299
-6.500 -0.2255 0.01066 0.00458 -0.1139 0.8390 0.0311
-6.250 -0.2030 0.01049 0.00435 -0.1131 0.8308 0.0318
-6.000 -0.1807 0.01029 0.00412 -0.1123 0.8242 0.0331
-5.750 -0.1577 0.01013 0.00393 -0.1116 0.8170 0.0343
-5.500 -0.1332 0.00998 0.00376 -0.1112 0.8125 0.0358
-5.250 -0.1094 0.00981 0.00359 -0.1106 0.8082 0.0377
-5.000 -0.0855 0.00963 0.00341 -0.1100 0.8038 0.0406
-4.750 -0.0607 0.00948 0.00326 -0.1096 0.7997 0.0435
-4.500 -0.0356 0.00932 0.00311 -0.1093 0.7966 0.0485
-4.250 -0.0102 0.00916 0.00299 -0.1090 0.7934 0.0571
-4.000 0.0149 0.00901 0.00288 -0.1086 0.7899 0.0646
-3.750 0.0391 0.00888 0.00275 -0.1080 0.7833 0.0695
-3.500 0.0635 0.00879 0.00264 -0.1074 0.7758 0.0741
-3.250 0.0880 0.00868 0.00253 -0.1068 0.7683 0.0782
-3.000 0.1118 0.00855 0.00241 -0.1061 0.7594 0.0847
-2.750 0.1354 0.00836 0.00229 -0.1054 0.7504 0.1049
-2.500 0.1570 0.00815 0.00216 -0.1043 0.7381 0.1401
-2.250 0.1798 0.00803 0.00206 -0.1034 0.7262 0.1652
-2.000 0.2006 0.00777 0.00192 -0.1022 0.7133 0.2138
-1.750 0.2115 0.00651 0.00147 -0.0998 0.6992 0.4750
-1.500 0.2309 0.00643 0.00143 -0.0981 0.6757 0.5172
-1.250 0.2506 0.00646 0.00142 -0.0964 0.6556 0.5352
-1.000 0.2718 0.00649 0.00143 -0.0950 0.6392 0.5515
-0.750 0.2923 0.00656 0.00145 -0.0935 0.6194 0.5619
-0.500 0.3108 0.00670 0.00148 -0.0915 0.5917 0.5691
-0.250 0.3282 0.00687 0.00153 -0.0893 0.5627 0.5751
0.000 0.3478 0.00702 0.00160 -0.0876 0.5399 0.5832
0.250 0.3634 0.00731 0.00170 -0.0851 0.4919 0.5915
0.500 0.3761 0.00772 0.00187 -0.0820 0.4230 0.5996
0.750 0.3934 0.00804 0.00202 -0.0800 0.3905 0.6060
1.000 0.4140 0.00823 0.00214 -0.0785 0.3688 0.6130
1.250 0.4348 0.00843 0.00226 -0.0771 0.3464 0.6188
1.500 0.4569 0.00861 0.00235 -0.0760 0.3321 0.6232
1.750 0.4791 0.00875 0.00246 -0.0749 0.3201 0.6274
2.000 0.5017 0.00889 0.00257 -0.0739 0.3081 0.6341
2.250 0.5241 0.00904 0.00268 -0.0729 0.2971 0.6400
2.500 0.5452 0.00923 0.00282 -0.0716 0.2807 0.6456
2.750 0.5677 0.00936 0.00295 -0.0705 0.2699 0.6523
3.000 0.5872 0.00962 0.00310 -0.0690 0.2450 0.6568
3.250 0.6016 0.01008 0.00335 -0.0665 0.1994 0.6609
3.500 0.6199 0.01040 0.00358 -0.0647 0.1762 0.6657
3.750 0.6400 0.01065 0.00377 -0.0633 0.1635 0.6705
4.000 0.6616 0.01085 0.00393 -0.0622 0.1577 0.6740
4.250 0.6833 0.01103 0.00411 -0.0611 0.1538 0.6775
4.500 0.7049 0.01121 0.00429 -0.0600 0.1496 0.6811
4.750 0.7270 0.01138 0.00447 -0.0590 0.1468 0.6859
5.000 0.7493 0.01155 0.00464 -0.0580 0.1447 0.6886
5.250 0.7711 0.01173 0.00484 -0.0570 0.1422 0.6933
5.500 0.7926 0.01193 0.00505 -0.0559 0.1395 0.6970
5.750 0.8134 0.01217 0.00528 -0.0547 0.1357 0.7004
6.000 0.8347 0.01237 0.00549 -0.0536 0.1331 0.7036
6.250 0.8566 0.01256 0.00569 -0.0526 0.1304 0.7064
6.500 0.8773 0.01280 0.00593 -0.0515 0.1240 0.7091
6.750 0.8976 0.01306 0.00618 -0.0502 0.1178 0.7116
7.000 0.9167 0.01338 0.00645 -0.0489 0.1073 0.7142
7.250 0.9359 0.01369 0.00673 -0.0475 0.1025 0.7169
7.500 0.9553 0.01400 0.00702 -0.0462 0.0983 0.7194
7.750 0.9751 0.01430 0.00731 -0.0450 0.0953 0.7217
8.000 0.9942 0.01462 0.00763 -0.0437 0.0929 0.7241
8.250 1.0120 0.01500 0.00801 -0.0422 0.0895 0.7263
8.500 1.0305 0.01535 0.00839 -0.0408 0.0869 0.7287
8.750 1.0501 0.01565 0.00872 -0.0396 0.0856 0.7312
9.000 1.0695 0.01597 0.00907 -0.0384 0.0837 0.7336
9.250 1.0885 0.01631 0.00944 -0.0372 0.0816 0.7361
9.500 1.1065 0.01671 0.00984 -0.0359 0.0785 0.7381
9.750 1.1239 0.01713 0.01025 -0.0345 0.0758 0.7396
10.000 1.1420 0.01752 0.01066 -0.0332 0.0727 0.7410
10.250 1.1596 0.01793 0.01110 -0.0319 0.0704 0.7424
10.500 1.1759 0.01842 0.01157 -0.0304 0.0669 0.7438
10.750 1.1927 0.01888 0.01205 -0.0290 0.0651 0.7452
11.000 1.2093 0.01936 0.01256 -0.0277 0.0633 0.7467
11.250 1.2248 0.01992 0.01311 -0.0262 0.0609 0.7483
11.500 1.2400 0.02050 0.01371 -0.0247 0.0588 0.7499
11.750 1.2565 0.02101 0.01425 -0.0235 0.0578 0.7514
12.000 1.2720 0.02157 0.01485 -0.0221 0.0564 0.7527
12.250 1.2865 0.02222 0.01551 -0.0207 0.0542 0.7540
12.500 1.3000 0.02293 0.01623 -0.0192 0.0522 0.7553
12.750 1.3141 0.02362 0.01695 -0.0178 0.0507 0.7567
13.000 1.3293 0.02423 0.01761 -0.0166 0.0496 0.7584
13.250 1.3432 0.02492 0.01836 -0.0153 0.0480 0.7600
13.500 1.3562 0.02571 0.01916 -0.0139 0.0454 0.7614
13.750 1.3681 0.02657 0.02004 -0.0125 0.0439 0.7626
14.000 1.3811 0.02738 0.02088 -0.0113 0.0417 0.7639
14.250 1.3932 0.02827 0.02180 -0.0100 0.0399 0.7652
14.500 1.4034 0.02929 0.02285 -0.0086 0.0379 0.7664
14.750 1.4147 0.03028 0.02386 -0.0074 0.0360 0.7674
15.000 1.4245 0.03138 0.02499 -0.0061 0.0346 0.7684
15.250 1.4337 0.03256 0.02620 -0.0048 0.0330 0.7693
15.500 1.4430 0.03375 0.02743 -0.0036 0.0320 0.7703
15.750 1.4524 0.03497 0.02870 -0.0025 0.0308 0.7712
16.000 1.4602 0.03634 0.03011 -0.0014 0.0297 0.7719
16.250 1.4673 0.03780 0.03161 -0.0004 0.0285 0.7729
16.500 1.4737 0.03935 0.03323 0.0006 0.0274 0.7738
16.750 1.4816 0.04083 0.03477 0.0014 0.0267 0.7748
17.000 1.4878 0.04250 0.03650 0.0022 0.0259 0.7757
17.250 1.4925 0.04433 0.03839 0.0030 0.0248 0.7765
17.500 1.4956 0.04638 0.04049 0.0036 0.0239 0.7773
17.750 1.5003 0.04834 0.04253 0.0041 0.0232 0.7782
18.000 1.5039 0.05047 0.04473 0.0045 0.0224 0.7789
18.250 1.5068 0.05273 0.04706 0.0048 0.0217 0.7798
18.500 1.5076 0.05527 0.04966 0.0050 0.0208 0.7805
18.750 1.5069 0.05806 0.05252 0.0050 0.0200 0.7812
19.000 1.5072 0.06082 0.05537 0.0048 0.0192 0.7819
19.250 1.5059 0.06386 0.05849 0.0044 0.0184 0.7826
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