PW51 (pw51-pw) Xfoil prediction polar at RE=5,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: PW51 (pw51-pw) Reynolds number: 5,000,000 Max Cl/Cd: 119.9 at α=5.75° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-pw51-pw-5000000.txt Download as CSV file: xf-pw51-pw-5000000.csv |
XFOIL Version 6.96
Calculated polar for: PW51
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 5.000 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-16.750 -1.4758 0.04517 0.04332 -0.0182 1.0000 0.0020
-16.500 -1.4989 0.03904 0.03703 -0.0222 1.0000 0.0020
-16.250 -1.5164 0.03531 0.03315 -0.0219 1.0000 0.0020
-16.000 -1.5246 0.03307 0.03080 -0.0195 1.0000 0.0020
-15.750 -1.5189 0.03144 0.02909 -0.0181 1.0000 0.0020
-15.500 -1.5080 0.03004 0.02762 -0.0170 1.0000 0.0021
-15.250 -1.4964 0.02856 0.02604 -0.0159 1.0000 0.0021
-15.000 -1.4813 0.02736 0.02478 -0.0150 1.0000 0.0021
-14.750 -1.4639 0.02637 0.02373 -0.0143 1.0000 0.0022
-14.500 -1.4463 0.02532 0.02262 -0.0135 1.0000 0.0022
-14.250 -1.4268 0.02444 0.02169 -0.0128 1.0000 0.0022
-14.000 -1.4062 0.02368 0.02089 -0.0123 1.0000 0.0023
-13.750 -1.3854 0.02287 0.02003 -0.0117 1.0000 0.0023
-13.500 -1.3636 0.02218 0.01930 -0.0112 1.0000 0.0023
-13.250 -1.3414 0.02151 0.01859 -0.0107 1.0000 0.0023
-13.000 -1.3187 0.02086 0.01791 -0.0103 1.0000 0.0024
-12.750 -1.2956 0.02025 0.01726 -0.0098 1.0000 0.0024
-12.500 -1.2719 0.01970 0.01667 -0.0095 1.0000 0.0024
-12.250 -1.2480 0.01915 0.01609 -0.0091 1.0000 0.0024
-12.000 -1.2238 0.01861 0.01552 -0.0088 1.0000 0.0024
-11.750 -1.1992 0.01813 0.01501 -0.0085 1.0000 0.0024
-11.500 -1.1744 0.01763 0.01449 -0.0082 1.0000 0.0024
-11.250 -1.1494 0.01717 0.01400 -0.0079 1.0000 0.0024
-11.000 -1.1243 0.01669 0.01348 -0.0077 1.0000 0.0025
-10.750 -1.0988 0.01625 0.01302 -0.0074 1.0000 0.0025
-10.500 -1.0803 0.01414 0.01060 -0.0065 1.0000 0.0026
-10.250 -1.0562 0.01325 0.00959 -0.0061 1.0000 0.0027
-10.000 -1.0310 0.01258 0.00885 -0.0058 1.0000 0.0028
-9.750 -1.0051 0.01202 0.00823 -0.0055 1.0000 0.0029
-9.500 -0.9790 0.01152 0.00768 -0.0053 1.0000 0.0030
-9.250 -0.9525 0.01108 0.00721 -0.0051 1.0000 0.0030
-9.000 -0.9257 0.01068 0.00676 -0.0050 1.0000 0.0031
-8.750 -0.8988 0.01029 0.00634 -0.0048 1.0000 0.0032
-8.500 -0.8717 0.00992 0.00594 -0.0047 1.0000 0.0032
-8.250 -0.8445 0.00958 0.00558 -0.0046 1.0000 0.0033
-8.000 -0.8155 0.00926 0.00523 -0.0049 0.9818 0.0033
-7.750 -0.7917 0.00902 0.00493 -0.0039 0.9609 0.0034
-7.500 -0.7671 0.00878 0.00462 -0.0031 0.9416 0.0035
-7.250 -0.7410 0.00854 0.00432 -0.0026 0.9228 0.0035
-7.000 -0.7143 0.00832 0.00403 -0.0023 0.9032 0.0036
-6.750 -0.6872 0.00812 0.00374 -0.0020 0.8833 0.0037
-6.500 -0.6598 0.00792 0.00348 -0.0019 0.8628 0.0038
-6.250 -0.6321 0.00775 0.00324 -0.0017 0.8413 0.0039
-6.000 -0.6043 0.00760 0.00302 -0.0016 0.8197 0.0040
-5.750 -0.5763 0.00748 0.00283 -0.0016 0.7971 0.0041
-5.500 -0.5481 0.00737 0.00267 -0.0016 0.7759 0.0042
-5.250 -0.5203 0.00713 0.00235 -0.0015 0.7551 0.0053
-5.000 -0.4922 0.00701 0.00217 -0.0015 0.7350 0.0058
-4.750 -0.4639 0.00690 0.00202 -0.0015 0.7152 0.0062
-4.500 -0.4356 0.00683 0.00189 -0.0015 0.6950 0.0064
-4.250 -0.4073 0.00669 0.00171 -0.0015 0.6757 0.0082
-4.000 -0.3790 0.00659 0.00157 -0.0015 0.6565 0.0094
-3.750 -0.3507 0.00648 0.00144 -0.0015 0.6378 0.0126
-3.500 -0.3223 0.00639 0.00132 -0.0015 0.6202 0.0163
-3.250 -0.2938 0.00630 0.00121 -0.0016 0.6038 0.0202
-3.000 -0.2653 0.00622 0.00111 -0.0016 0.5880 0.0243
-2.750 -0.2369 0.00613 0.00102 -0.0017 0.5725 0.0315
-2.500 -0.2084 0.00604 0.00093 -0.0017 0.5569 0.0414
-2.250 -0.1799 0.00595 0.00085 -0.0018 0.5414 0.0546
-2.000 -0.1515 0.00585 0.00078 -0.0018 0.5255 0.0735
-1.750 -0.1231 0.00575 0.00071 -0.0019 0.5094 0.0976
-1.500 -0.0947 0.00564 0.00065 -0.0020 0.4925 0.1265
-1.250 -0.0661 0.00557 0.00060 -0.0021 0.4762 0.1505
-1.000 -0.0377 0.00546 0.00056 -0.0022 0.4612 0.1871
-0.750 -0.0094 0.00535 0.00052 -0.0023 0.4467 0.2294
-0.500 0.0190 0.00523 0.00049 -0.0024 0.4320 0.2752
-0.250 0.0474 0.00513 0.00047 -0.0025 0.4171 0.3241
0.000 0.0757 0.00500 0.00046 -0.0026 0.4020 0.3810
0.250 0.1040 0.00490 0.00045 -0.0027 0.3873 0.4333
0.500 0.1323 0.00480 0.00045 -0.0028 0.3713 0.4924
0.750 0.1605 0.00469 0.00046 -0.0029 0.3560 0.5542
1.000 0.1887 0.00460 0.00047 -0.0030 0.3401 0.6123
1.250 0.2170 0.00454 0.00050 -0.0031 0.3250 0.6638
1.500 0.2451 0.00445 0.00052 -0.0032 0.3117 0.7230
1.750 0.2733 0.00443 0.00056 -0.0032 0.2972 0.7640
2.000 0.3014 0.00439 0.00060 -0.0032 0.2835 0.8094
2.250 0.3293 0.00438 0.00065 -0.0032 0.2698 0.8497
2.500 0.3572 0.00440 0.00071 -0.0031 0.2561 0.8805
2.750 0.3847 0.00440 0.00076 -0.0029 0.2469 0.9098
3.000 0.4118 0.00444 0.00083 -0.0027 0.2345 0.9338
3.250 0.4383 0.00451 0.00090 -0.0023 0.2223 0.9549
3.500 0.4647 0.00459 0.00097 -0.0018 0.2102 0.9721
3.750 0.4924 0.00471 0.00104 -0.0017 0.1962 0.9844
4.000 0.5236 0.00484 0.00112 -0.0024 0.1823 0.9908
4.250 0.5550 0.00499 0.00121 -0.0032 0.1687 0.9954
4.500 0.5886 0.00516 0.00131 -0.0046 0.1538 0.9981
4.750 0.6214 0.00536 0.00143 -0.0058 0.1361 0.9999
5.000 0.6487 0.00554 0.00155 -0.0057 0.1230 1.0000
5.250 0.6757 0.00570 0.00166 -0.0055 0.1124 1.0000
5.500 0.7029 0.00589 0.00179 -0.0054 0.1005 1.0000
5.750 0.7302 0.00609 0.00194 -0.0054 0.0883 1.0000
6.000 0.7575 0.00632 0.00210 -0.0053 0.0753 1.0000
6.250 0.7849 0.00655 0.00227 -0.0053 0.0644 1.0000
6.500 0.8122 0.00681 0.00246 -0.0053 0.0527 1.0000
6.750 0.8395 0.00707 0.00267 -0.0053 0.0431 1.0000
7.000 0.8669 0.00732 0.00287 -0.0054 0.0366 1.0000
7.250 0.8943 0.00754 0.00306 -0.0054 0.0309 1.0000
7.500 0.9214 0.00782 0.00330 -0.0054 0.0245 1.0000
7.750 0.9487 0.00806 0.00352 -0.0054 0.0214 1.0000
8.000 0.9759 0.00832 0.00375 -0.0054 0.0176 1.0000
8.250 1.0032 0.00855 0.00396 -0.0054 0.0163 1.0000
8.500 1.0301 0.00883 0.00423 -0.0054 0.0139 1.0000
8.750 1.0573 0.00906 0.00446 -0.0054 0.0126 1.0000
9.000 1.0842 0.00931 0.00470 -0.0055 0.0116 1.0000
9.250 1.1108 0.00964 0.00501 -0.0054 0.0094 1.0000
9.500 1.1375 0.00991 0.00528 -0.0054 0.0085 1.0000
9.750 1.1639 0.01025 0.00561 -0.0054 0.0071 1.0000
10.000 1.1902 0.01056 0.00593 -0.0053 0.0061 1.0000
10.250 1.2163 0.01092 0.00628 -0.0053 0.0051 1.0000
10.500 1.2421 0.01130 0.00666 -0.0052 0.0040 1.0000
10.750 1.2673 0.01178 0.00714 -0.0051 0.0025 1.0000
11.000 1.2923 0.01227 0.00764 -0.0049 0.0018 1.0000
11.250 1.3173 0.01274 0.00814 -0.0047 0.0014 1.0000
11.500 1.3424 0.01314 0.00857 -0.0046 0.0013 1.0000
11.750 1.3673 0.01356 0.00902 -0.0045 0.0013 1.0000
12.000 1.3919 0.01401 0.00949 -0.0043 0.0013 1.0000
12.250 1.4162 0.01448 0.00999 -0.0041 0.0012 1.0000
12.500 1.4401 0.01497 0.01052 -0.0038 0.0012 1.0000
12.750 1.4636 0.01549 0.01108 -0.0036 0.0012 1.0000
13.000 1.4867 0.01604 0.01167 -0.0032 0.0012 1.0000
13.250 1.5093 0.01662 0.01229 -0.0029 0.0012 1.0000
13.500 1.5314 0.01722 0.01292 -0.0025 0.0011 1.0000
13.750 1.5530 0.01784 0.01359 -0.0021 0.0011 1.0000
14.000 1.5738 0.01851 0.01430 -0.0016 0.0011 1.0000
14.250 1.5938 0.01923 0.01507 -0.0011 0.0011 1.0000
14.500 1.6130 0.01999 0.01588 -0.0005 0.0011 1.0000
14.750 1.6310 0.02080 0.01675 0.0002 0.0011 1.0000
15.000 1.6478 0.02167 0.01768 0.0010 0.0011 1.0000
15.250 1.6629 0.02262 0.01870 0.0019 0.0010 1.0000
15.500 1.6756 0.02365 0.01979 0.0030 0.0010 1.0000
15.750 1.6817 0.02482 0.02103 0.0049 0.0010 1.0000
16.000 1.6855 0.02627 0.02256 0.0063 0.0010 1.0000
16.250 1.6884 0.02807 0.02444 0.0070 0.0010 1.0000
16.500 1.6895 0.03033 0.02679 0.0072 0.0010 1.0000
16.750 1.6893 0.03305 0.02960 0.0067 0.0010 1.0000
17.000 1.6879 0.03619 0.03283 0.0056 0.0010 1.0000
17.250 1.6823 0.04009 0.03684 0.0039 0.0010 1.0000
17.500 1.6729 0.04472 0.04158 0.0017 0.0010 1.0000
17.750 1.6600 0.05000 0.04697 -0.0009 0.0010 1.0000
18.000 1.6412 0.05624 0.05333 -0.0040 0.0010 1.0000
18.250 1.6175 0.06335 0.06056 -0.0075 0.0010 1.0000
18.500 1.5873 0.07150 0.06885 -0.0115 0.0010 1.0000
18.750 1.5510 0.08088 0.07837 -0.0161 0.0010 1.0000
19.000 1.5121 0.09108 0.08870 -0.0211 0.0010 1.0000
19.250 1.4674 0.10250 0.10028 -0.0268 0.0010 1.0000
19.500 1.4255 0.11375 0.11166 -0.0324 0.0010 1.0000
19.750 1.3794 0.12622 0.12427 -0.0388 0.0010 1.0000
20.000 1.3322 0.13939 0.13759 -0.0459 0.0011 1.0000
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