AG45c -03f (ag45c03-il)
AG45c -03f - Drela AG45c -03f airfoil
| Details | Dat file | Parser | |
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(ag45c03-il) AG45c -03f Drela AG45c -03f airfoil Max thickness 6.9% at 23.5% chord. Max camber 2% at 31.7% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Selig format |
AG45c -03f
1.000086 0.015922
0.994138 0.016317
0.982099 0.017150
0.968507 0.018092
0.954615 0.019018
0.940684 0.019941
0.926751 0.020852
0.912817 0.021756
0.898884 0.022651
0.884954 0.023532
0.871023 0.024397
0.857096 0.025245
0.843173 0.026073
0.829250 0.026883
0.815328 0.027672
0.801405 0.028440
0.787486 0.029188
0.773565 0.029917
0.759646 0.030627
0.745726 0.031316
0.731807 0.031988
0.717884 0.032644
0.707074 0.033141
0.703460 0.033311
0.701652 0.033395
0.698206 0.033724
0.691314 0.034394
0.677446 0.035733
0.663581 0.037053
0.656762 0.037694
0.646541 0.038646
0.635857 0.039627
0.621994 0.040879
0.605869 0.042302
0.594295 0.043299
0.580476 0.044462
0.566659 0.045596
0.555673 0.046476
0.546779 0.047173
0.538810 0.047786
0.524991 0.048822
0.511176 0.049822
0.497336 0.050788
0.483480 0.051715
0.469633 0.052602
0.455797 0.053447
0.441954 0.054250
0.428114 0.055008
0.414279 0.055721
0.400440 0.056378
0.386604 0.056967
0.372772 0.057484
0.358942 0.057929
0.345111 0.058298
0.331287 0.058589
0.317470 0.058797
0.303656 0.058914
0.289853 0.058939
0.276060 0.058864
0.262271 0.058683
0.248498 0.058389
0.234746 0.057976
0.221005 0.057435
0.207291 0.056758
0.193607 0.055937
0.179951 0.054959
0.166346 0.053814
0.152785 0.052485
0.139290 0.050958
0.125875 0.049215
0.112549 0.047231
0.099355 0.044984
0.086310 0.042435
0.073476 0.039546
0.060899 0.036264
0.048706 0.032533
0.037085 0.028314
0.026424 0.023642
0.017422 0.018794
0.010776 0.014325
0.006402 0.010622
0.003629 0.007640
0.001877 0.005178
0.000830 0.003085
0.000323 0.001304
0.000250 -0.000178
0.000581 -0.001543
0.001479 -0.002917
0.003095 -0.004214
0.005482 -0.005487
0.008963 -0.006839
0.014198 -0.008345
0.022017 -0.009970
0.032333 -0.011478
0.044204 -0.012670
0.056845 -0.013515
0.069853 -0.014071
0.083076 -0.014399
0.096446 -0.014558
0.109914 -0.014581
0.123457 -0.014492
0.137057 -0.014307
0.150705 -0.014041
0.164384 -0.013707
0.178099 -0.013314
0.191835 -0.012872
0.205592 -0.012389
0.219378 -0.011885
0.233198 -0.011374
0.247042 -0.010859
0.260919 -0.010338
0.274829 -0.009811
0.288770 -0.009279
0.302739 -0.008743
0.316729 -0.008203
0.330733 -0.007659
0.344757 -0.007112
0.358791 -0.006561
0.372833 -0.006009
0.386891 -0.005453
0.400968 -0.004895
0.415056 -0.004335
0.429138 -0.003775
0.443210 -0.003214
0.457270 -0.002653
0.471326 -0.002091
0.485372 -0.001531
0.499404 -0.000971
0.513429 -0.000412
0.527448 0.000146
0.541461 0.000703
0.549029 0.001003
0.558642 0.001383
0.568957 0.001791
0.582414 0.002321
0.595587 0.002837
0.609478 0.003380
0.623073 0.003908
0.636668 0.004433
0.646250 0.004801
0.655266 0.005147
0.663866 0.005474
0.677534 0.005992
0.691197 0.006506
0.697089 0.006727
0.700090 0.006839
0.706464 0.007075
0.718992 0.007539
0.732862 0.008047
0.746721 0.008549
0.760568 0.009047
0.774417 0.009538
0.788265 0.010023
0.802117 0.010503
0.815974 0.010977
0.829832 0.011440
0.843692 0.011882
0.857561 0.012306
0.871428 0.012708
0.885297 0.013084
0.899175 0.013445
0.913051 0.013773
0.926933 0.014076
0.940816 0.014342
0.954703 0.014571
0.968566 0.014761
0.982184 0.014890
0.994208 0.014978
1.000152 0.015029
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Polars for AG45c -03f (ag45c03-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| ag45c03-il | 50,000 | 9 | 29.7 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ag45c03-il | 50,000 | 5 | 34.9 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ag45c03-il | 100,000 | 9 | 46 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ag45c03-il | 100,000 | 5 | 47.9 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ag45c03-il | 200,000 | 9 | 62.4 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ag45c03-il | 200,000 | 5 | 61 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ag45c03-il | 500,000 | 9 | 83 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ag45c03-il | 500,000 | 5 | 78.1 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ag45c03-il | 1,000,000 | 9 | 97.4 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ag45c03-il | 1,000,000 | 5 | 91.2 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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