P-51D ROOT (BL17.5) AIRFOIL (p51droot-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: P-51D ROOT (BL17.5) AIRFOIL (p51droot-il) Reynolds number: 500,000 Max Cl/Cd: 81.34 at α=6.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-p51droot-il-500000.txt Download as CSV file: xf-p51droot-il-500000.csv |
XFOIL Version 6.96
Calculated polar for: P-51D ROOT (BL17.5) AIRFOIL
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.500 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-18.750 -0.8658 0.11555 0.11257 -0.0372 1.0000 0.0273
-18.500 -0.9261 0.09945 0.09615 -0.0475 1.0000 0.0272
-18.250 -0.9603 0.08948 0.08595 -0.0536 1.0000 0.0272
-18.000 -0.9843 0.08181 0.07807 -0.0582 1.0000 0.0273
-17.750 -1.0030 0.07550 0.07156 -0.0619 1.0000 0.0275
-17.500 -1.0177 0.07016 0.06604 -0.0647 1.0000 0.0276
-17.250 -1.0340 0.06490 0.06061 -0.0667 1.0000 0.0279
-17.000 -1.0382 0.06139 0.05700 -0.0678 1.0000 0.0282
-16.750 -1.0370 0.05868 0.05425 -0.0686 1.0000 0.0285
-16.500 -1.0352 0.05616 0.05168 -0.0694 1.0000 0.0288
-16.250 -1.0338 0.05368 0.04913 -0.0701 1.0000 0.0291
-16.000 -1.0328 0.05123 0.04661 -0.0707 1.0000 0.0295
-15.750 -1.0321 0.04886 0.04414 -0.0711 1.0000 0.0298
-15.500 -1.0303 0.04674 0.04194 -0.0715 1.0000 0.0304
-15.250 -1.0278 0.04458 0.03966 -0.0716 1.0000 0.0308
-15.000 -1.0254 0.04257 0.03753 -0.0716 1.0000 0.0313
-14.750 -1.0220 0.04060 0.03543 -0.0715 1.0000 0.0317
-14.500 -1.0177 0.03882 0.03352 -0.0713 1.0000 0.0321
-14.250 -1.0123 0.03719 0.03176 -0.0710 1.0000 0.0323
-14.000 -1.0007 0.03541 0.02995 -0.0702 1.0000 0.0331
-13.750 -0.9896 0.03418 0.02870 -0.0698 1.0000 0.0336
-13.500 -0.9789 0.03300 0.02750 -0.0693 1.0000 0.0341
-13.250 -0.9690 0.03191 0.02637 -0.0687 1.0000 0.0347
-13.000 -0.9594 0.03084 0.02524 -0.0679 1.0000 0.0353
-12.750 -0.9514 0.02986 0.02420 -0.0667 1.0000 0.0360
-12.500 -0.9468 0.02900 0.02327 -0.0647 1.0000 0.0364
-12.250 -0.9281 0.02792 0.02210 -0.0651 0.9920 0.0371
-12.000 -0.9039 0.02693 0.02098 -0.0666 0.9878 0.0376
-11.750 -0.8785 0.02557 0.01964 -0.0674 0.9852 0.0389
-11.500 -0.8517 0.02464 0.01871 -0.0691 0.9822 0.0398
-11.250 -0.8249 0.02378 0.01781 -0.0706 0.9789 0.0409
-11.000 -0.7973 0.02291 0.01688 -0.0721 0.9751 0.0419
-10.750 -0.7690 0.02211 0.01600 -0.0737 0.9715 0.0430
-10.500 -0.7418 0.02142 0.01522 -0.0749 0.9675 0.0438
-10.250 -0.7247 0.02029 0.01412 -0.0744 0.9621 0.0453
-10.000 -0.7053 0.01965 0.01346 -0.0742 0.9570 0.0465
-9.750 -0.6891 0.01908 0.01286 -0.0732 0.9519 0.0476
-9.500 -0.6753 0.01855 0.01228 -0.0716 0.9463 0.0487
-9.000 -0.6496 0.01775 0.01134 -0.0675 0.9344 0.0507
-8.750 -0.6470 0.01702 0.01059 -0.0637 0.9276 0.0521
-8.500 -0.6375 0.01658 0.01014 -0.0609 0.9225 0.0536
-8.250 -0.6223 0.01619 0.00974 -0.0590 0.9173 0.0554
-8.000 -0.6060 0.01584 0.00934 -0.0572 0.9126 0.0571
-7.750 -0.5873 0.01556 0.00900 -0.0557 0.9082 0.0587
-7.500 -0.5740 0.01491 0.00835 -0.0536 0.9024 0.0613
-7.250 -0.5562 0.01449 0.00792 -0.0519 0.8974 0.0639
-7.000 -0.5361 0.01416 0.00755 -0.0506 0.8927 0.0666
-6.750 -0.5165 0.01371 0.00709 -0.0493 0.8865 0.0702
-6.500 -0.4967 0.01327 0.00665 -0.0480 0.8809 0.0748
-6.250 -0.4752 0.01289 0.00626 -0.0469 0.8748 0.0801
-6.000 -0.4539 0.01244 0.00585 -0.0458 0.8676 0.0896
-5.750 -0.4335 0.01189 0.00542 -0.0446 0.8613 0.1120
-5.500 -0.4119 0.01136 0.00505 -0.0437 0.8522 0.1458
-5.250 -0.3898 0.01085 0.00465 -0.0427 0.8436 0.1758
-5.000 -0.3683 0.01025 0.00421 -0.0418 0.8310 0.2134
-4.750 -0.3514 0.00922 0.00363 -0.0404 0.8139 0.3202
-4.500 -0.3332 0.00834 0.00312 -0.0389 0.7852 0.4167
-4.250 -0.3128 0.00799 0.00288 -0.0374 0.7412 0.4957
-4.000 -0.2884 0.00810 0.00283 -0.0366 0.7044 0.5277
-3.750 -0.2625 0.00825 0.00285 -0.0362 0.6816 0.5461
-3.500 -0.2354 0.00840 0.00287 -0.0359 0.6658 0.5605
-3.250 -0.2080 0.00854 0.00294 -0.0358 0.6538 0.5722
-3.000 -0.1806 0.00868 0.00299 -0.0356 0.6440 0.5812
-2.750 -0.1525 0.00882 0.00305 -0.0356 0.6359 0.5902
-2.500 -0.1247 0.00895 0.00311 -0.0355 0.6290 0.5976
-2.250 -0.0964 0.00906 0.00320 -0.0355 0.6231 0.6045
-2.000 -0.0681 0.00919 0.00324 -0.0355 0.6174 0.6111
-1.750 -0.0400 0.00925 0.00329 -0.0355 0.6124 0.6161
-1.500 -0.0116 0.00936 0.00337 -0.0356 0.6080 0.6212
-1.250 0.0171 0.00942 0.00339 -0.0357 0.6038 0.6257
-1.000 0.0457 0.00947 0.00338 -0.0359 0.5998 0.6290
-0.750 0.0741 0.00949 0.00340 -0.0360 0.5960 0.6328
-0.500 0.1024 0.00964 0.00351 -0.0360 0.5921 0.6381
-0.250 0.1310 0.00972 0.00359 -0.0361 0.5885 0.6437
0.000 0.1595 0.00973 0.00358 -0.0362 0.5845 0.6474
0.250 0.1879 0.00973 0.00359 -0.0364 0.5807 0.6503
0.500 0.2165 0.00978 0.00362 -0.0365 0.5775 0.6531
0.750 0.2453 0.00988 0.00367 -0.0368 0.5742 0.6554
1.000 0.2739 0.00985 0.00367 -0.0369 0.5704 0.6576
1.250 0.3023 0.00986 0.00367 -0.0371 0.5657 0.6599
1.500 0.3310 0.00991 0.00368 -0.0373 0.5622 0.6621
1.750 0.3597 0.00996 0.00370 -0.0375 0.5592 0.6641
2.000 0.3882 0.00999 0.00373 -0.0377 0.5558 0.6661
2.250 0.4164 0.00995 0.00375 -0.0378 0.5517 0.6681
2.500 0.4447 0.00996 0.00379 -0.0379 0.5477 0.6703
2.750 0.4731 0.01000 0.00384 -0.0381 0.5445 0.6728
3.000 0.5016 0.01007 0.00390 -0.0382 0.5411 0.6754
3.250 0.5301 0.01015 0.00398 -0.0384 0.5377 0.6777
3.500 0.5581 0.01016 0.00403 -0.0385 0.5335 0.6798
3.750 0.5860 0.01014 0.00405 -0.0385 0.5289 0.6821
4.000 0.6138 0.01016 0.00408 -0.0386 0.5244 0.6845
4.250 0.6416 0.01021 0.00417 -0.0386 0.5200 0.6869
4.500 0.6690 0.01020 0.00424 -0.0385 0.5149 0.6897
4.750 0.6964 0.01022 0.00429 -0.0385 0.5096 0.6927
5.000 0.7232 0.01027 0.00434 -0.0383 0.5022 0.6956
5.250 0.7493 0.01024 0.00435 -0.0380 0.4917 0.6982
5.500 0.7749 0.01021 0.00438 -0.0376 0.4794 0.7012
5.750 0.8001 0.01022 0.00442 -0.0371 0.4653 0.7043
6.000 0.8249 0.01028 0.00449 -0.0366 0.4467 0.7076
6.250 0.8476 0.01042 0.00458 -0.0357 0.4154 0.7112
6.500 0.8561 0.01129 0.00494 -0.0327 0.3158 0.7147
6.750 0.8669 0.01214 0.00553 -0.0301 0.2654 0.7188
7.000 0.8835 0.01264 0.00596 -0.0284 0.2388 0.7233
7.250 0.8996 0.01314 0.00636 -0.0267 0.2109 0.7282
7.500 0.9150 0.01364 0.00674 -0.0248 0.1847 0.7331
7.750 0.9278 0.01404 0.00711 -0.0224 0.1690 0.7387
8.000 0.9408 0.01443 0.00751 -0.0200 0.1582 0.7455
8.250 0.9529 0.01491 0.00799 -0.0175 0.1489 0.7533
8.500 0.9670 0.01530 0.00844 -0.0155 0.1407 0.7634
8.750 0.9795 0.01575 0.00896 -0.0132 0.1325 0.7771
9.000 0.9919 0.01618 0.00947 -0.0110 0.1233 0.7993
9.500 1.0121 0.01697 0.01056 -0.0056 0.1023 0.9003
9.750 1.0459 0.01791 0.01145 -0.0086 0.0821 1.0000
10.250 1.0653 0.01968 0.01312 -0.0047 0.0662 1.0000
10.500 1.0738 0.02068 0.01410 -0.0028 0.0617 1.0000
10.750 1.0844 0.02161 0.01504 -0.0011 0.0583 1.0000
11.000 1.0902 0.02285 0.01627 0.0008 0.0551 1.0000
11.250 1.1002 0.02390 0.01736 0.0023 0.0530 1.0000
11.500 1.1105 0.02497 0.01847 0.0036 0.0509 1.0000
11.750 1.1185 0.02624 0.01975 0.0050 0.0491 1.0000
12.000 1.1205 0.02800 0.02151 0.0066 0.0472 1.0000
12.250 1.1313 0.02920 0.02278 0.0075 0.0460 1.0000
12.500 1.1410 0.03052 0.02416 0.0084 0.0448 1.0000
12.750 1.1500 0.03195 0.02563 0.0092 0.0436 1.0000
13.000 1.1576 0.03353 0.02724 0.0099 0.0424 1.0000
13.250 1.1619 0.03543 0.02916 0.0107 0.0412 1.0000
13.500 1.1651 0.03748 0.03125 0.0115 0.0403 1.0000
13.750 1.1759 0.03894 0.03279 0.0118 0.0394 1.0000
14.000 1.1850 0.04056 0.03448 0.0121 0.0385 1.0000
14.250 1.1938 0.04226 0.03623 0.0124 0.0374 1.0000
14.500 1.2008 0.04411 0.03813 0.0127 0.0368 1.0000
14.750 1.2071 0.04606 0.04011 0.0129 0.0360 1.0000
15.000 1.2099 0.04834 0.04240 0.0132 0.0351 1.0000
15.250 1.2150 0.05042 0.04453 0.0135 0.0344 1.0000
15.500 1.2224 0.05239 0.04660 0.0135 0.0339 1.0000
15.750 1.2292 0.05443 0.04873 0.0134 0.0332 1.0000
16.000 1.2353 0.05659 0.05096 0.0133 0.0326 1.0000
16.250 1.2411 0.05882 0.05324 0.0130 0.0318 1.0000
16.500 1.2459 0.06119 0.05565 0.0127 0.0311 1.0000
16.750 1.2501 0.06359 0.05810 0.0124 0.0306 1.0000
17.000 1.2522 0.06613 0.06064 0.0124 0.0298 1.0000
17.250 1.2559 0.06870 0.06330 0.0120 0.0294 1.0000
17.500 1.2588 0.07149 0.06621 0.0114 0.0290 1.0000
17.750 1.2610 0.07443 0.06926 0.0106 0.0285 1.0000
18.000 1.2626 0.07749 0.07242 0.0096 0.0279 1.0000
18.250 1.2638 0.08063 0.07564 0.0087 0.0274 1.0000
18.500 1.2653 0.08378 0.07886 0.0076 0.0269 1.0000
18.750 1.2659 0.08709 0.08223 0.0065 0.0265 1.0000
19.000 1.2669 0.09033 0.08552 0.0053 0.0260 1.0000
19.250 1.2670 0.09363 0.08886 0.0042 0.0256 1.0000
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