LA2573A (la2573a-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: LA2573A (la2573a-il) Reynolds number: 500,000 Max Cl/Cd: 95.29 at α=8.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-la2573a-il-500000-n5.txt Download as CSV file: xf-la2573a-il-500000-n5.csv |
XFOIL Version 6.96
Calculated polar for: LA2573A
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.500 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-10.000 -0.5349 0.09845 0.09425 0.0170 0.4519 0.0233
-9.750 -0.8878 0.03464 0.02898 -0.0043 0.4658 0.0253
-9.500 -0.8900 0.03002 0.02370 -0.0018 0.4643 0.0256
-9.250 -0.8728 0.02855 0.02208 -0.0006 0.4623 0.0258
-9.000 -0.8525 0.02755 0.02097 0.0004 0.4601 0.0259
-8.750 -0.8312 0.02663 0.01995 0.0013 0.4578 0.0261
-8.500 -0.8094 0.02576 0.01897 0.0021 0.4555 0.0263
-8.250 -0.7869 0.02493 0.01801 0.0029 0.4533 0.0264
-8.000 -0.7641 0.02409 0.01704 0.0037 0.4512 0.0266
-7.750 -0.7409 0.02326 0.01608 0.0044 0.4491 0.0269
-7.500 -0.7173 0.02244 0.01510 0.0052 0.4470 0.0271
-7.250 -0.6933 0.02162 0.01413 0.0059 0.4451 0.0274
-7.000 -0.6688 0.02081 0.01319 0.0065 0.4435 0.0278
-6.750 -0.6438 0.02005 0.01230 0.0071 0.4417 0.0281
-6.500 -0.6184 0.01937 0.01148 0.0077 0.4398 0.0286
-6.250 -0.5926 0.01877 0.01074 0.0083 0.4381 0.0289
-6.000 -0.5665 0.01821 0.01005 0.0088 0.4364 0.0292
-5.750 -0.5407 0.01758 0.00938 0.0093 0.4348 0.0295
-5.500 -0.5143 0.01712 0.00889 0.0097 0.4331 0.0298
-5.250 -0.4877 0.01673 0.00845 0.0102 0.4315 0.0301
-5.000 -0.4609 0.01636 0.00804 0.0106 0.4299 0.0304
-4.750 -0.4341 0.01601 0.00763 0.0110 0.4280 0.0308
-4.500 -0.4072 0.01566 0.00723 0.0114 0.4262 0.0312
-4.250 -0.3801 0.01529 0.00683 0.0118 0.4250 0.0316
-4.000 -0.3530 0.01494 0.00644 0.0122 0.4238 0.0321
-3.750 -0.3258 0.01462 0.00608 0.0126 0.4224 0.0326
-3.500 -0.2985 0.01433 0.00575 0.0129 0.4211 0.0330
-3.250 -0.2716 0.01399 0.00542 0.0133 0.4197 0.0336
-3.000 -0.2442 0.01375 0.00519 0.0137 0.4182 0.0342
-2.750 -0.2168 0.01352 0.00496 0.0140 0.4166 0.0348
-2.500 -0.1894 0.01330 0.00472 0.0143 0.4150 0.0355
-2.250 -0.1619 0.01309 0.00449 0.0147 0.4134 0.0362
-2.000 -0.1344 0.01290 0.00426 0.0150 0.4120 0.0369
-1.750 -0.1070 0.01270 0.00405 0.0153 0.4107 0.0376
-1.500 -0.0795 0.01254 0.00389 0.0156 0.4092 0.0385
-1.250 -0.0518 0.01241 0.00376 0.0159 0.4078 0.0395
-1.000 -0.0239 0.01226 0.00363 0.0162 0.4067 0.0408
-0.750 0.0040 0.01212 0.00351 0.0164 0.4053 0.0421
-0.500 0.0319 0.01198 0.00340 0.0167 0.4039 0.0437
-0.250 0.0599 0.01187 0.00331 0.0169 0.4025 0.0455
0.000 0.0879 0.01177 0.00322 0.0171 0.4012 0.0474
0.250 0.1160 0.01167 0.00315 0.0173 0.3997 0.0500
0.500 0.1441 0.01158 0.00307 0.0175 0.3981 0.0535
0.750 0.1721 0.01149 0.00300 0.0177 0.3965 0.0590
1.000 0.2001 0.01140 0.00296 0.0179 0.3950 0.0677
1.250 0.2280 0.01132 0.00294 0.0181 0.3937 0.0833
1.500 0.2554 0.01118 0.00293 0.0183 0.3923 0.1211
1.750 0.2813 0.01088 0.00293 0.0187 0.3907 0.2247
2.000 0.2837 0.00879 0.00300 0.0237 0.3898 0.8511
2.250 0.3094 0.00884 0.00313 0.0247 0.3883 0.8882
2.500 0.3356 0.00892 0.00324 0.0256 0.3868 0.9091
2.750 0.3616 0.00901 0.00335 0.0265 0.3853 0.9250
3.000 0.3872 0.00911 0.00348 0.0276 0.3836 0.9413
3.250 0.4173 0.00925 0.00363 0.0279 0.3818 0.9574
3.500 0.4519 0.00934 0.00369 0.0268 0.3799 0.9611
3.750 0.4821 0.00940 0.00372 0.0265 0.3783 0.9625
4.000 0.5118 0.00946 0.00375 0.0262 0.3766 0.9638
4.250 0.5411 0.00955 0.00380 0.0260 0.3747 0.9653
4.500 0.5701 0.00961 0.00387 0.0259 0.3731 0.9670
4.750 0.5984 0.00966 0.00395 0.0259 0.3712 0.9688
5.000 0.6279 0.00972 0.00403 0.0257 0.3690 0.9703
5.250 0.6593 0.00979 0.00411 0.0250 0.3667 0.9711
5.500 0.6907 0.00985 0.00418 0.0244 0.3644 0.9720
5.750 0.7219 0.00992 0.00424 0.0238 0.3620 0.9731
6.000 0.7529 0.01001 0.00431 0.0232 0.3598 0.9742
6.250 0.7838 0.01010 0.00443 0.0226 0.3574 0.9755
6.500 0.8146 0.01019 0.00457 0.0220 0.3546 0.9768
6.750 0.8451 0.01027 0.00469 0.0215 0.3514 0.9784
7.000 0.8752 0.01035 0.00478 0.0210 0.3481 0.9802
7.250 0.9045 0.01044 0.00487 0.0207 0.3449 0.9823
7.500 0.9369 0.01053 0.00500 0.0198 0.3403 0.9832
7.750 0.9688 0.01057 0.00501 0.0188 0.3285 0.9842
8.000 1.0002 0.01071 0.00511 0.0180 0.3125 0.9853
8.250 1.0310 0.01092 0.00530 0.0171 0.3006 0.9867
8.500 1.0615 0.01114 0.00553 0.0164 0.2901 0.9883
8.750 1.0911 0.01145 0.00581 0.0156 0.2773 0.9903
9.000 1.1198 0.01184 0.00616 0.0150 0.2621 0.9925
9.250 1.1484 0.01240 0.00664 0.0142 0.2425 0.9947
9.500 1.1764 0.01313 0.00728 0.0131 0.2179 0.9975
9.750 1.2029 0.01407 0.00810 0.0121 0.1912 1.0000
10.000 1.2156 0.01497 0.00892 0.0138 0.1697 1.0000
10.250 1.2271 0.01604 0.00988 0.0154 0.1480 1.0000
10.500 1.2380 0.01721 0.01096 0.0168 0.1271 1.0000
10.750 1.2473 0.01851 0.01219 0.0181 0.1096 1.0000
11.000 1.2544 0.01998 0.01361 0.0192 0.0954 1.0000
11.250 1.2559 0.02190 0.01554 0.0201 0.0848 1.0000
11.500 1.2413 0.02585 0.01960 0.0190 0.0808 1.0000
11.750 1.2290 0.02973 0.02353 0.0182 0.0762 1.0000
12.000 1.2183 0.03328 0.02712 0.0179 0.0723 1.0000
12.250 1.2080 0.03673 0.03061 0.0176 0.0684 1.0000
12.500 1.2003 0.03992 0.03382 0.0174 0.0653 1.0000
12.750 1.1938 0.04299 0.03692 0.0171 0.0618 1.0000
13.000 1.1877 0.04607 0.04003 0.0168 0.0590 1.0000
13.250 1.1837 0.04895 0.04294 0.0165 0.0561 1.0000
13.750 1.1795 0.05465 0.04869 0.0156 0.0510 1.0000
14.000 1.1784 0.05755 0.05162 0.0151 0.0487 1.0000
14.250 1.1790 0.06028 0.05437 0.0146 0.0466 1.0000
14.500 1.1796 0.06311 0.05724 0.0140 0.0447 1.0000
14.750 1.1805 0.06591 0.06006 0.0134 0.0432 1.0000
15.000 1.1814 0.06874 0.06292 0.0128 0.0416 1.0000
15.250 1.1831 0.07153 0.06575 0.0121 0.0403 1.0000
15.500 1.1848 0.07434 0.06859 0.0115 0.0390 1.0000
15.750 1.1850 0.07736 0.07165 0.0107 0.0380 1.0000
16.000 1.1857 0.08037 0.07470 0.0099 0.0372 1.0000
16.250 1.1886 0.08312 0.07750 0.0092 0.0363 1.0000
16.500 1.1900 0.08610 0.08053 0.0083 0.0355 1.0000
16.750 1.1911 0.08914 0.08361 0.0074 0.0347 1.0000
17.000 1.1921 0.09223 0.08674 0.0065 0.0340 1.0000
17.250 1.1917 0.09559 0.09013 0.0054 0.0334 1.0000
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