TRAINER60 (trainer60-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
|---|---|
|
Airfoil: TRAINER60 (trainer60-il) Reynolds number: 1,000,000 Max Cl/Cd: 79.28 at α=8.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-trainer60-il-1000000-n5.txt Download as CSV file: xf-trainer60-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: TRAINER60
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
------ -------- --------- --------- -------- -------- --------
-19.000 -1.4056 0.10278 0.09842 0.0236 0.9985 0.0204
-18.750 -1.4191 0.09664 0.09218 0.0206 0.9981 0.0206
-18.500 -1.4317 0.09085 0.08628 0.0180 0.9976 0.0207
-18.250 -1.4433 0.08528 0.08062 0.0155 0.9972 0.0209
-18.000 -1.4542 0.07993 0.07517 0.0132 0.9968 0.0212
-17.750 -1.4621 0.07508 0.07023 0.0112 0.9964 0.0214
-17.500 -1.4687 0.07045 0.06551 0.0092 0.9960 0.0216
-17.250 -1.4743 0.06597 0.06094 0.0073 0.9955 0.0218
-17.000 -1.4779 0.06182 0.05671 0.0055 0.9951 0.0221
-16.750 -1.4819 0.05787 0.05267 0.0042 0.9946 0.0223
-16.250 -1.5169 0.05135 0.04602 0.0092 0.9598 0.0226
-16.000 -1.5103 0.04795 0.04252 0.0067 0.9494 0.0230
-15.500 -1.4978 0.04200 0.03638 0.0035 0.9414 0.0236
-15.250 -1.4912 0.03906 0.03337 0.0019 0.9386 0.0242
-15.000 -1.4807 0.03639 0.03062 0.0001 0.9361 0.0247
-14.750 -1.4642 0.03390 0.02806 -0.0025 0.9350 0.0253
-14.500 -1.4320 0.03152 0.02561 -0.0077 0.9359 0.0260
-14.250 -1.4005 0.02950 0.02353 -0.0122 0.9352 0.0268
-14.000 -1.3759 0.02781 0.02177 -0.0150 0.9324 0.0274
-13.750 -1.3592 0.02617 0.02007 -0.0162 0.9298 0.0282
-13.500 -1.3416 0.02475 0.01861 -0.0171 0.9270 0.0291
-13.250 -1.3211 0.02353 0.01733 -0.0182 0.9241 0.0300
-13.000 -1.2975 0.02247 0.01621 -0.0196 0.9217 0.0311
-12.750 -1.2802 0.02144 0.01515 -0.0196 0.9182 0.0320
-12.500 -1.2609 0.02052 0.01420 -0.0197 0.9145 0.0334
-12.250 -1.2387 0.01976 0.01340 -0.0200 0.9112 0.0348
-12.000 -1.2209 0.01910 0.01271 -0.0191 0.9083 0.0361
-11.750 -1.2061 0.01846 0.01206 -0.0175 0.9048 0.0379
-11.500 -1.1891 0.01792 0.01150 -0.0160 0.9008 0.0398
-11.250 -1.1705 0.01738 0.01094 -0.0149 0.8971 0.0422
-11.000 -1.1539 0.01689 0.01045 -0.0131 0.8926 0.0448
-10.750 -1.1365 0.01637 0.00994 -0.0115 0.8867 0.0483
-10.500 -1.1172 0.01591 0.00948 -0.0102 0.8809 0.0518
-10.000 -1.0815 0.01494 0.00854 -0.0068 0.8619 0.0630
-9.750 -1.0645 0.01443 0.00805 -0.0049 0.8453 0.0710
-9.500 -1.0477 0.01391 0.00750 -0.0028 0.8086 0.0825
-9.250 -1.0244 0.01336 0.00690 -0.0024 0.7665 0.0995
-9.000 -0.9989 0.01290 0.00646 -0.0022 0.7388 0.1157
-8.750 -0.9726 0.01258 0.00613 -0.0021 0.7200 0.1268
-8.500 -0.9461 0.01231 0.00585 -0.0019 0.7036 0.1356
-8.250 -0.9197 0.01207 0.00559 -0.0016 0.6916 0.1428
-8.000 -0.8928 0.01187 0.00537 -0.0014 0.6799 0.1493
-7.750 -0.8659 0.01168 0.00516 -0.0012 0.6708 0.1538
-7.500 -0.8392 0.01149 0.00496 -0.0009 0.6613 0.1591
-7.250 -0.8119 0.01135 0.00478 -0.0007 0.6523 0.1641
-7.000 -0.7852 0.01115 0.00459 -0.0004 0.6463 0.1692
-6.750 -0.7586 0.01096 0.00441 0.0000 0.6397 0.1760
-6.500 -0.7316 0.01080 0.00424 0.0003 0.6328 0.1826
-6.250 -0.7054 0.01059 0.00405 0.0007 0.6264 0.1916
-6.000 -0.6779 0.01045 0.00391 0.0009 0.6201 0.1969
-5.750 -0.6512 0.01027 0.00374 0.0013 0.6125 0.2032
-5.500 -0.6239 0.01015 0.00359 0.0016 0.6045 0.2084
-5.250 -0.5961 0.01003 0.00346 0.0018 0.5989 0.2129
-5.000 -0.5691 0.00987 0.00331 0.0021 0.5918 0.2202
-4.750 -0.5417 0.00975 0.00318 0.0024 0.5840 0.2269
-4.500 -0.5144 0.00960 0.00305 0.0027 0.5772 0.2354
-4.250 -0.4873 0.00945 0.00292 0.0030 0.5683 0.2477
-4.000 -0.4604 0.00930 0.00279 0.0034 0.5583 0.2613
-3.750 -0.4332 0.00913 0.00267 0.0037 0.5492 0.2763
-3.500 -0.4058 0.00901 0.00257 0.0040 0.5389 0.2907
-3.250 -0.3780 0.00891 0.00249 0.0042 0.5304 0.3045
-3.000 -0.3502 0.00881 0.00241 0.0044 0.5205 0.3179
-2.750 -0.3221 0.00874 0.00234 0.0046 0.5113 0.3291
-2.500 -0.2937 0.00867 0.00229 0.0047 0.5026 0.3404
-2.250 -0.2654 0.00864 0.00224 0.0048 0.4924 0.3488
-2.000 -0.2368 0.00859 0.00220 0.0049 0.4832 0.3573
-1.500 -0.1797 0.00858 0.00213 0.0051 0.4589 0.3709
-1.250 -0.1514 0.00859 0.00211 0.0052 0.4467 0.3781
-1.000 -0.1223 0.00858 0.00209 0.0052 0.4390 0.3839
-0.750 -0.0936 0.00857 0.00207 0.0052 0.4293 0.3917
-0.500 -0.0648 0.00857 0.00206 0.0052 0.4203 0.3999
-0.250 -0.0358 0.00859 0.00206 0.0052 0.4111 0.4056
0.000 -0.0069 0.00859 0.00206 0.0052 0.4037 0.4127
0.250 0.0226 0.00857 0.00206 0.0051 0.3987 0.4204
0.750 0.0811 0.00858 0.00209 0.0050 0.3833 0.4412
1.000 0.1109 0.00857 0.00211 0.0048 0.3786 0.4517
1.250 0.1409 0.00856 0.00214 0.0045 0.3723 0.4658
1.500 0.1705 0.00858 0.00218 0.0044 0.3641 0.4781
1.750 0.2005 0.00860 0.00223 0.0041 0.3575 0.4923
2.000 0.2308 0.00862 0.00228 0.0038 0.3497 0.5047
2.250 0.2603 0.00869 0.00234 0.0036 0.3413 0.5141
2.500 0.2907 0.00872 0.00240 0.0033 0.3341 0.5224
2.750 0.3203 0.00881 0.00247 0.0031 0.3231 0.5298
3.000 0.3499 0.00891 0.00253 0.0029 0.3111 0.5351
3.250 0.3793 0.00904 0.00262 0.0027 0.2949 0.5410
3.500 0.4087 0.00919 0.00273 0.0025 0.2777 0.5479
3.750 0.4376 0.00938 0.00285 0.0024 0.2595 0.5540
4.000 0.4662 0.00958 0.00299 0.0023 0.2438 0.5586
4.250 0.4959 0.00975 0.00313 0.0020 0.2308 0.5639
4.500 0.5262 0.00990 0.00326 0.0015 0.2213 0.5693
4.750 0.5561 0.01008 0.00342 0.0012 0.2121 0.5745
5.000 0.5864 0.01021 0.00355 0.0008 0.2062 0.5791
5.250 0.6159 0.01042 0.00372 0.0005 0.1969 0.5836
5.500 0.6479 0.01056 0.00387 -0.0003 0.1899 0.5895
5.750 0.6801 0.01074 0.00404 -0.0013 0.1821 0.5959
6.000 0.7122 0.01091 0.00421 -0.0022 0.1769 0.6011
6.250 0.7439 0.01105 0.00436 -0.0029 0.1726 0.6055
6.500 0.7767 0.01126 0.00455 -0.0040 0.1654 0.6117
6.750 0.8098 0.01141 0.00474 -0.0052 0.1606 0.6187
7.000 0.8418 0.01160 0.00493 -0.0061 0.1547 0.6264
7.250 0.8743 0.01183 0.00516 -0.0071 0.1480 0.6351
7.500 0.9072 0.01203 0.00538 -0.0083 0.1414 0.6447
7.750 0.9400 0.01227 0.00564 -0.0094 0.1350 0.6568
8.000 0.9741 0.01252 0.00591 -0.0109 0.1273 0.6723
8.250 1.0092 0.01280 0.00622 -0.0127 0.1189 0.6935
8.500 1.0473 0.01321 0.00666 -0.0152 0.1049 0.7258
8.750 1.0776 0.01380 0.00720 -0.0162 0.0856 0.7551
9.000 1.1033 0.01451 0.00787 -0.0163 0.0665 0.7798
9.250 1.1282 0.01511 0.00847 -0.0162 0.0557 0.8016
9.500 1.1526 0.01559 0.00899 -0.0158 0.0500 0.8222
9.750 1.1749 0.01605 0.00949 -0.0149 0.0460 0.8424
10.000 1.1962 0.01650 0.00997 -0.0138 0.0434 0.8582
10.250 1.2184 0.01697 0.01045 -0.0129 0.0412 0.8690
10.500 1.2391 0.01747 0.01096 -0.0119 0.0393 0.8764
10.750 1.2614 0.01794 0.01144 -0.0111 0.0378 0.8829
11.000 1.2823 0.01846 0.01198 -0.0102 0.0364 0.8876
11.250 1.3020 0.01906 0.01258 -0.0091 0.0349 0.8927
11.500 1.3223 0.01960 0.01314 -0.0081 0.0340 0.8977
11.750 1.3422 0.02019 0.01376 -0.0072 0.0330 0.9006
12.000 1.3609 0.02083 0.01443 -0.0062 0.0322 0.9038
12.250 1.3767 0.02156 0.01517 -0.0048 0.0314 0.9071
12.500 1.3851 0.02238 0.01603 -0.0023 0.0307 0.9103
12.750 1.3968 0.02325 0.01695 -0.0008 0.0303 0.9127
13.000 1.4081 0.02428 0.01805 0.0004 0.0299 0.9160
13.250 1.4186 0.02545 0.01926 0.0014 0.0294 0.9193
13.500 1.4291 0.02677 0.02063 0.0021 0.0289 0.9218
13.750 1.4408 0.02822 0.02214 0.0023 0.0285 0.9247
14.000 1.4505 0.02988 0.02386 0.0024 0.0280 0.9278
14.250 1.4586 0.03177 0.02580 0.0024 0.0276 0.9300
14.500 1.4657 0.03390 0.02799 0.0022 0.0272 0.9315
14.750 1.4720 0.03629 0.03044 0.0015 0.0267 0.9330
15.000 1.4791 0.03857 0.03280 0.0010 0.0265 0.9352
15.250 1.4840 0.04106 0.03537 0.0004 0.0263 0.9381
15.500 1.4880 0.04362 0.03801 -0.0001 0.0260 0.9408
15.750 1.4923 0.04641 0.04088 -0.0011 0.0257 0.9433
16.000 1.4934 0.04950 0.04405 -0.0021 0.0253 0.9454
16.250 1.4924 0.05282 0.04746 -0.0030 0.0251 0.9470
16.500 1.4895 0.05642 0.05114 -0.0041 0.0248 0.9484
17.000 1.4811 0.06437 0.05927 -0.0070 0.0245 0.9510
17.250 1.4762 0.06872 0.06372 -0.0088 0.0243 0.9525
17.500 1.4700 0.07355 0.06865 -0.0111 0.0240 0.9543
17.750 1.4621 0.07864 0.07385 -0.0135 0.0238 0.9557
18.000 1.4530 0.08393 0.07925 -0.0160 0.0236 0.9566
18.500 1.4311 0.09551 0.09104 -0.0219 0.0233 0.9604
18.750 1.4190 0.10195 0.09759 -0.0256 0.0231 0.9629
19.000 1.3771 0.10456 0.10021 -0.0174 0.0232 0.9941
|
Polar data table (+)
Polar graphs
<< Back to TRAINER60 (trainer60-il)