P-51D ROOT (BL17.5) AIRFOIL (p51droot-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: P-51D ROOT (BL17.5) AIRFOIL (p51droot-il) Reynolds number: 1,000,000 Max Cl/Cd: 92.53 at α=5.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-p51droot-il-1000000.txt Download as CSV file: xf-p51droot-il-1000000.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 = 1.000 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.500 -1.1370 0.08211 0.07858 -0.0519 1.0000 0.0198
-19.250 -1.1486 0.07705 0.07342 -0.0543 1.0000 0.0201
-19.000 -1.1622 0.07191 0.06819 -0.0565 1.0000 0.0205
-18.750 -1.1664 0.06807 0.06429 -0.0582 1.0000 0.0207
-18.500 -1.1695 0.06442 0.06058 -0.0597 1.0000 0.0209
-18.250 -1.1705 0.06115 0.05723 -0.0610 1.0000 0.0211
-18.000 -1.1691 0.05826 0.05428 -0.0621 1.0000 0.0214
-17.750 -1.1674 0.05547 0.05143 -0.0631 1.0000 0.0217
-17.500 -1.1640 0.05294 0.04883 -0.0639 1.0000 0.0219
-17.250 -1.1612 0.05041 0.04623 -0.0645 1.0000 0.0223
-17.000 -1.1573 0.04809 0.04384 -0.0651 1.0000 0.0225
-16.750 -1.1519 0.04597 0.04165 -0.0655 1.0000 0.0227
-16.500 -1.1444 0.04409 0.03970 -0.0659 1.0000 0.0231
-16.250 -1.1361 0.04235 0.03788 -0.0662 1.0000 0.0233
-16.000 -1.1281 0.04064 0.03610 -0.0664 1.0000 0.0236
-15.750 -1.1298 0.03819 0.03358 -0.0662 1.0000 0.0239
-15.500 -1.1276 0.03613 0.03148 -0.0660 1.0000 0.0243
-15.250 -1.1190 0.03463 0.02995 -0.0659 1.0000 0.0248
-15.000 -1.1090 0.03325 0.02855 -0.0658 1.0000 0.0252
-14.750 -1.0991 0.03191 0.02717 -0.0656 1.0000 0.0255
-14.500 -1.0768 0.03048 0.02569 -0.0677 0.9758 0.0260
-14.250 -1.0486 0.02923 0.02437 -0.0707 0.9692 0.0266
-14.000 -1.0219 0.02805 0.02311 -0.0732 0.9643 0.0272
-13.750 -0.9973 0.02695 0.02193 -0.0751 0.9583 0.0275
-13.500 -0.9826 0.02565 0.02053 -0.0756 0.9512 0.0279
-13.250 -0.9753 0.02425 0.01908 -0.0749 0.9452 0.0286
-13.000 -0.9636 0.02325 0.01802 -0.0742 0.9403 0.0291
-12.750 -0.9506 0.02244 0.01719 -0.0734 0.9368 0.0296
-12.500 -0.9376 0.02166 0.01638 -0.0724 0.9330 0.0302
-12.250 -0.9255 0.02089 0.01555 -0.0713 0.9291 0.0307
-12.000 -0.9120 0.02022 0.01482 -0.0702 0.9252 0.0312
-11.750 -0.8988 0.01954 0.01410 -0.0690 0.9222 0.0317
-11.500 -0.8845 0.01895 0.01346 -0.0678 0.9191 0.0321
-11.250 -0.8749 0.01817 0.01262 -0.0660 0.9158 0.0327
-11.000 -0.8685 0.01734 0.01174 -0.0637 0.9123 0.0335
-10.750 -0.8576 0.01676 0.01114 -0.0618 0.9090 0.0342
-10.500 -0.8450 0.01626 0.01063 -0.0599 0.9058 0.0349
-10.250 -0.8328 0.01581 0.01015 -0.0577 0.9021 0.0356
-10.000 -0.8200 0.01545 0.00974 -0.0555 0.8986 0.0363
-9.750 -0.8057 0.01517 0.00941 -0.0534 0.8954 0.0369
-9.500 -0.7865 0.01487 0.00908 -0.0521 0.8925 0.0375
-9.250 -0.7719 0.01430 0.00848 -0.0503 0.8889 0.0388
-9.000 -0.7529 0.01390 0.00808 -0.0490 0.8854 0.0401
-8.750 -0.7319 0.01359 0.00774 -0.0481 0.8821 0.0412
-8.500 -0.7101 0.01332 0.00744 -0.0472 0.8789 0.0424
-8.250 -0.6866 0.01305 0.00715 -0.0466 0.8759 0.0434
-8.000 -0.6655 0.01263 0.00671 -0.0456 0.8721 0.0449
-7.750 -0.6435 0.01225 0.00633 -0.0448 0.8679 0.0468
-7.500 -0.6199 0.01198 0.00603 -0.0442 0.8639 0.0486
-7.250 -0.5950 0.01174 0.00577 -0.0438 0.8596 0.0502
-7.000 -0.5712 0.01140 0.00542 -0.0432 0.8544 0.0523
-6.750 -0.5475 0.01105 0.00508 -0.0426 0.8489 0.0551
-6.500 -0.5223 0.01080 0.00480 -0.0422 0.8430 0.0575
-6.250 -0.4968 0.01053 0.00452 -0.0419 0.8346 0.0601
-6.000 -0.4722 0.01021 0.00421 -0.0414 0.8248 0.0649
-5.750 -0.4469 0.00995 0.00393 -0.0410 0.8082 0.0698
-5.500 -0.4235 0.00969 0.00359 -0.0402 0.7693 0.0792
-5.250 -0.4029 0.00953 0.00331 -0.0390 0.7067 0.1020
-5.000 -0.3802 0.00935 0.00311 -0.0383 0.6727 0.1315
-4.750 -0.3558 0.00916 0.00294 -0.0378 0.6515 0.1555
-4.500 -0.3304 0.00898 0.00278 -0.0376 0.6363 0.1770
-4.250 -0.3057 0.00870 0.00257 -0.0372 0.6245 0.2094
-4.000 -0.2848 0.00798 0.00224 -0.0365 0.6149 0.3120
-3.750 -0.2617 0.00746 0.00198 -0.0360 0.6071 0.3878
-3.500 -0.2381 0.00696 0.00181 -0.0355 0.6004 0.4774
-3.250 -0.2113 0.00687 0.00179 -0.0354 0.5940 0.5151
-3.000 -0.1830 0.00686 0.00179 -0.0354 0.5889 0.5343
-2.750 -0.1543 0.00687 0.00179 -0.0356 0.5840 0.5469
-2.500 -0.1256 0.00692 0.00180 -0.0357 0.5793 0.5576
-2.250 -0.0974 0.00697 0.00182 -0.0358 0.5744 0.5657
-2.000 -0.0681 0.00700 0.00184 -0.0360 0.5713 0.5727
-1.750 -0.0391 0.00703 0.00184 -0.0362 0.5679 0.5786
-1.500 -0.0104 0.00706 0.00188 -0.0364 0.5642 0.5843
-1.250 0.0183 0.00714 0.00190 -0.0365 0.5599 0.5893
-1.000 0.0471 0.00723 0.00194 -0.0367 0.5556 0.5935
-0.750 0.0760 0.00720 0.00193 -0.0369 0.5525 0.5975
-0.500 0.1050 0.00721 0.00195 -0.0371 0.5496 0.6006
-0.250 0.1339 0.00726 0.00198 -0.0372 0.5469 0.6040
0.000 0.1626 0.00734 0.00203 -0.0374 0.5435 0.6084
0.250 0.1909 0.00743 0.00207 -0.0375 0.5389 0.6129
0.500 0.2199 0.00741 0.00209 -0.0377 0.5357 0.6168
0.750 0.2489 0.00742 0.00212 -0.0379 0.5327 0.6193
1.000 0.2778 0.00746 0.00215 -0.0381 0.5298 0.6218
1.250 0.3065 0.00751 0.00218 -0.0383 0.5266 0.6243
1.500 0.3349 0.00759 0.00222 -0.0384 0.5228 0.6263
1.750 0.3639 0.00762 0.00225 -0.0386 0.5200 0.6278
2.000 0.3928 0.00761 0.00226 -0.0388 0.5173 0.6297
2.250 0.4216 0.00759 0.00228 -0.0390 0.5145 0.6319
2.500 0.4502 0.00761 0.00231 -0.0392 0.5114 0.6338
2.750 0.4785 0.00766 0.00236 -0.0393 0.5078 0.6358
3.000 0.5067 0.00772 0.00241 -0.0394 0.5035 0.6378
3.250 0.5356 0.00772 0.00245 -0.0396 0.4995 0.6399
3.500 0.5642 0.00775 0.00250 -0.0398 0.4960 0.6418
3.750 0.5925 0.00781 0.00255 -0.0399 0.4917 0.6436
4.000 0.6203 0.00790 0.00262 -0.0399 0.4872 0.6452
4.250 0.6490 0.00788 0.00266 -0.0401 0.4819 0.6472
4.500 0.6763 0.00792 0.00269 -0.0400 0.4723 0.6497
4.750 0.7042 0.00794 0.00275 -0.0401 0.4623 0.6520
5.000 0.7311 0.00803 0.00281 -0.0399 0.4468 0.6544
5.250 0.7569 0.00818 0.00289 -0.0396 0.4231 0.6568
5.500 0.7750 0.00882 0.00316 -0.0382 0.3407 0.6592
5.750 0.7900 0.00970 0.00367 -0.0363 0.2678 0.6613
6.000 0.8122 0.01011 0.00395 -0.0354 0.2434 0.6632
6.250 0.8342 0.01044 0.00421 -0.0346 0.2169 0.6662
6.500 0.8539 0.01089 0.00451 -0.0334 0.1830 0.6690
6.750 0.8743 0.01127 0.00480 -0.0323 0.1630 0.6718
7.000 0.8955 0.01159 0.00508 -0.0313 0.1514 0.6747
7.250 0.9178 0.01185 0.00533 -0.0304 0.1436 0.6776
7.500 0.9380 0.01218 0.00562 -0.0292 0.1348 0.6804
7.750 0.9597 0.01238 0.00585 -0.0283 0.1288 0.6844
8.000 0.9778 0.01269 0.00615 -0.0267 0.1204 0.6883
8.250 0.9959 0.01290 0.00638 -0.0251 0.1135 0.6923
8.500 1.0107 0.01323 0.00668 -0.0230 0.1044 0.6962
8.750 1.0237 0.01366 0.00706 -0.0206 0.0919 0.7008
9.000 1.0347 0.01416 0.00753 -0.0180 0.0786 0.7063
9.250 1.0455 0.01472 0.00805 -0.0155 0.0681 0.7123
9.500 1.0569 0.01528 0.00860 -0.0132 0.0607 0.7193
9.750 1.0677 0.01587 0.00920 -0.0109 0.0551 0.7289
10.000 1.0815 0.01634 0.00974 -0.0090 0.0517 0.7422
10.250 1.0914 0.01694 0.01041 -0.0066 0.0479 0.7656
10.500 1.1015 0.01733 0.01104 -0.0041 0.0459 0.8276
10.750 1.1103 0.01768 0.01165 -0.0012 0.0438 0.9098
11.000 1.1473 0.01863 0.01268 -0.0050 0.0403 1.0000
11.250 1.1626 0.01924 0.01333 -0.0038 0.0393 1.0000
11.500 1.1762 0.01996 0.01407 -0.0024 0.0379 1.0000
11.750 1.1884 0.02079 0.01491 -0.0010 0.0366 1.0000
12.000 1.1971 0.02186 0.01599 0.0007 0.0351 1.0000
12.250 1.2086 0.02280 0.01697 0.0020 0.0343 1.0000
12.500 1.2221 0.02365 0.01786 0.0031 0.0336 1.0000
12.750 1.2340 0.02463 0.01888 0.0042 0.0328 1.0000
13.000 1.2452 0.02570 0.01997 0.0052 0.0318 1.0000
13.250 1.2540 0.02698 0.02128 0.0063 0.0310 1.0000
13.500 1.2590 0.02863 0.02296 0.0074 0.0299 1.0000
13.750 1.2675 0.03008 0.02446 0.0082 0.0295 1.0000
14.000 1.2776 0.03143 0.02587 0.0089 0.0291 1.0000
14.250 1.2885 0.03277 0.02726 0.0093 0.0285 1.0000
14.500 1.2992 0.03417 0.02871 0.0097 0.0278 1.0000
14.750 1.3081 0.03576 0.03035 0.0101 0.0273 1.0000
15.000 1.3156 0.03752 0.03214 0.0105 0.0267 1.0000
15.250 1.3209 0.03951 0.03417 0.0108 0.0261 1.0000
15.500 1.3211 0.04205 0.03676 0.0111 0.0254 1.0000
15.750 1.3267 0.04411 0.03888 0.0112 0.0251 1.0000
16.000 1.3358 0.04582 0.04066 0.0113 0.0247 1.0000
16.250 1.3432 0.04771 0.04261 0.0113 0.0243 1.0000
16.500 1.3490 0.04982 0.04478 0.0113 0.0238 1.0000
16.750 1.3553 0.05189 0.04690 0.0112 0.0234 1.0000
17.000 1.3602 0.05413 0.04919 0.0110 0.0229 1.0000
17.250 1.3629 0.05663 0.05174 0.0108 0.0226 1.0000
17.500 1.3635 0.05940 0.05457 0.0105 0.0222 1.0000
17.750 1.3611 0.06259 0.05782 0.0101 0.0218 1.0000
18.000 1.3542 0.06636 0.06167 0.0095 0.0213 1.0000
18.250 1.3586 0.06887 0.06425 0.0089 0.0211 1.0000
18.500 1.3634 0.07137 0.06682 0.0084 0.0208 1.0000
18.750 1.3639 0.07448 0.07002 0.0076 0.0205 1.0000
19.000 1.3646 0.07757 0.07318 0.0068 0.0202 1.0000
19.250 1.3660 0.08063 0.07631 0.0058 0.0198 1.0000
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