LWK 79-100 (lwk79100-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: LWK 79-100 (lwk79100-il) Reynolds number: 1,000,000 Max Cl/Cd: 74.23 at α=8.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-lwk79100-il-1000000-n5.txt Download as CSV file: xf-lwk79100-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: LWK 79-100
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
------ -------- --------- --------- -------- -------- --------
-17.750 -1.1066 0.12069 0.11826 0.0214 1.0000 0.0055
-17.500 -1.1482 0.10757 0.10499 0.0138 1.0000 0.0054
-17.250 -1.1849 0.09596 0.09322 0.0071 1.0000 0.0053
-17.000 -1.2167 0.08562 0.08273 0.0011 1.0000 0.0052
-16.750 -1.2531 0.07483 0.07177 -0.0053 1.0000 0.0053
-16.500 -1.2808 0.06616 0.06293 -0.0104 1.0000 0.0052
-16.250 -1.2975 0.05972 0.05635 -0.0142 1.0000 0.0051
-16.000 -1.3173 0.05316 0.04963 -0.0180 1.0000 0.0051
-15.750 -1.3320 0.04773 0.04407 -0.0209 1.0000 0.0052
-15.500 -1.3427 0.04318 0.03939 -0.0230 1.0000 0.0052
-15.250 -1.3541 0.03882 0.03489 -0.0249 1.0000 0.0053
-15.000 -1.3578 0.03564 0.03159 -0.0259 1.0000 0.0054
-14.750 -1.3628 0.03259 0.02841 -0.0265 1.0000 0.0054
-14.500 -1.3656 0.03017 0.02588 -0.0264 1.0000 0.0055
-14.250 -1.3672 0.02831 0.02391 -0.0251 1.0000 0.0056
-14.000 -1.3651 0.02699 0.02251 -0.0231 1.0000 0.0058
-13.750 -1.3609 0.02592 0.02137 -0.0207 1.0000 0.0059
-13.500 -1.3524 0.02482 0.02017 -0.0188 1.0000 0.0060
-13.250 -1.3386 0.02391 0.01919 -0.0175 1.0000 0.0062
-13.000 -1.3238 0.02299 0.01819 -0.0163 1.0000 0.0064
-12.750 -1.3072 0.02216 0.01727 -0.0152 1.0000 0.0066
-12.500 -1.2897 0.02135 0.01637 -0.0142 1.0000 0.0068
-12.250 -1.2711 0.02058 0.01552 -0.0133 1.0000 0.0069
-12.000 -1.2516 0.01985 0.01472 -0.0124 1.0000 0.0071
-11.750 -1.2312 0.01918 0.01397 -0.0116 1.0000 0.0073
-11.500 -1.2109 0.01846 0.01317 -0.0108 1.0000 0.0075
-11.250 -1.1902 0.01773 0.01239 -0.0101 1.0000 0.0079
-11.000 -1.1684 0.01710 0.01171 -0.0094 1.0000 0.0083
-10.750 -1.1459 0.01653 0.01110 -0.0088 1.0000 0.0087
-10.500 -1.1230 0.01601 0.01053 -0.0082 1.0000 0.0091
-10.250 -1.0996 0.01551 0.00998 -0.0076 1.0000 0.0096
-10.000 -1.0758 0.01506 0.00947 -0.0071 1.0000 0.0100
-9.750 -1.0523 0.01454 0.00892 -0.0066 1.0000 0.0108
-9.500 -1.0283 0.01409 0.00845 -0.0061 1.0000 0.0118
-9.250 -1.0037 0.01368 0.00802 -0.0056 1.0000 0.0127
-9.000 -0.9789 0.01331 0.00760 -0.0052 1.0000 0.0133
-8.750 -0.9543 0.01289 0.00716 -0.0047 1.0000 0.0144
-8.500 -0.9293 0.01252 0.00678 -0.0043 1.0000 0.0156
-8.250 -0.9040 0.01218 0.00643 -0.0039 1.0000 0.0167
-8.000 -0.8785 0.01189 0.00609 -0.0035 1.0000 0.0175
-7.750 -0.8532 0.01153 0.00573 -0.0031 1.0000 0.0190
-7.500 -0.8278 0.01121 0.00541 -0.0027 1.0000 0.0206
-7.000 -0.7760 0.01068 0.00485 -0.0019 1.0000 0.0230
-6.750 -0.7505 0.01036 0.00453 -0.0015 1.0000 0.0253
-6.500 -0.7247 0.01008 0.00426 -0.0011 1.0000 0.0275
-6.250 -0.6909 0.00983 0.00400 -0.0024 0.9773 0.0296
-6.000 -0.6518 0.00986 0.00367 -0.0047 0.8177 0.0340
-5.500 -0.6008 0.00962 0.00321 -0.0037 0.7498 0.0424
-5.250 -0.5743 0.00946 0.00299 -0.0034 0.7313 0.0481
-5.000 -0.5477 0.00926 0.00278 -0.0031 0.7164 0.0569
-4.750 -0.5210 0.00906 0.00258 -0.0029 0.7038 0.0676
-4.500 -0.4942 0.00885 0.00239 -0.0027 0.6927 0.0818
-4.250 -0.4672 0.00865 0.00220 -0.0025 0.6825 0.0966
-3.750 -0.4130 0.00826 0.00188 -0.0021 0.6645 0.1307
-3.500 -0.3859 0.00806 0.00173 -0.0019 0.6567 0.1533
-3.250 -0.3586 0.00786 0.00160 -0.0018 0.6499 0.1743
-3.000 -0.3314 0.00765 0.00147 -0.0016 0.6429 0.2017
-2.750 -0.3042 0.00741 0.00134 -0.0015 0.6367 0.2363
-2.500 -0.2773 0.00714 0.00121 -0.0013 0.6300 0.2800
-2.250 -0.2501 0.00692 0.00111 -0.0011 0.6242 0.3185
-2.000 -0.2226 0.00674 0.00104 -0.0010 0.6178 0.3529
-1.750 -0.1951 0.00660 0.00096 -0.0009 0.6112 0.3826
-1.500 -0.1673 0.00647 0.00091 -0.0008 0.6046 0.4088
-1.250 -0.1396 0.00637 0.00086 -0.0006 0.5954 0.4348
-1.000 -0.1118 0.00628 0.00082 -0.0005 0.5832 0.4592
-0.750 -0.0839 0.00622 0.00079 -0.0004 0.5718 0.4806
-0.500 -0.0560 0.00617 0.00078 -0.0002 0.5604 0.5013
-0.250 -0.0281 0.00615 0.00077 -0.0001 0.5477 0.5205
0.000 0.0000 0.00614 0.00076 0.0000 0.5354 0.5356
0.250 0.0281 0.00615 0.00076 0.0001 0.5205 0.5476
0.500 0.0560 0.00617 0.00078 0.0002 0.5013 0.5602
0.750 0.0839 0.00622 0.00079 0.0004 0.4805 0.5718
1.000 0.1118 0.00629 0.00082 0.0005 0.4591 0.5832
1.250 0.1396 0.00637 0.00086 0.0006 0.4346 0.5955
1.500 0.1673 0.00647 0.00091 0.0008 0.4086 0.6046
1.750 0.1951 0.00660 0.00096 0.0009 0.3829 0.6112
2.000 0.2226 0.00674 0.00104 0.0010 0.3533 0.6178
2.250 0.2501 0.00692 0.00111 0.0011 0.3188 0.6242
2.500 0.2773 0.00714 0.00121 0.0013 0.2797 0.6301
2.750 0.3043 0.00741 0.00134 0.0015 0.2364 0.6368
3.000 0.3313 0.00766 0.00147 0.0016 0.2009 0.6429
3.250 0.3586 0.00786 0.00160 0.0018 0.1744 0.6498
3.500 0.3859 0.00806 0.00173 0.0019 0.1529 0.6567
3.750 0.4130 0.00826 0.00188 0.0021 0.1308 0.6646
4.000 0.4401 0.00847 0.00204 0.0023 0.1117 0.6727
4.250 0.4672 0.00866 0.00220 0.0025 0.0965 0.6824
4.500 0.4942 0.00885 0.00239 0.0027 0.0820 0.6927
4.750 0.5210 0.00906 0.00258 0.0029 0.0676 0.7039
5.000 0.5478 0.00926 0.00278 0.0031 0.0569 0.7164
5.250 0.5743 0.00946 0.00299 0.0034 0.0481 0.7314
5.500 0.6008 0.00962 0.00321 0.0037 0.0424 0.7499
6.000 0.6519 0.00987 0.00367 0.0047 0.0341 0.8169
6.250 0.6905 0.00983 0.00399 0.0025 0.0297 0.9761
6.500 0.7247 0.01008 0.00426 0.0011 0.0275 1.0000
6.750 0.7505 0.01036 0.00453 0.0015 0.0253 1.0000
7.000 0.7761 0.01068 0.00485 0.0019 0.0230 1.0000
7.250 0.8021 0.01093 0.00512 0.0023 0.0221 1.0000
7.500 0.8278 0.01121 0.00541 0.0027 0.0205 1.0000
7.750 0.8533 0.01153 0.00573 0.0031 0.0189 1.0000
8.000 0.8786 0.01189 0.00609 0.0035 0.0175 1.0000
8.250 0.9041 0.01218 0.00642 0.0039 0.0167 1.0000
8.500 0.9294 0.01252 0.00679 0.0043 0.0156 1.0000
8.750 0.9544 0.01289 0.00717 0.0047 0.0144 1.0000
9.000 0.9790 0.01332 0.00760 0.0052 0.0133 1.0000
9.250 1.0039 0.01369 0.00802 0.0056 0.0126 1.0000
9.500 1.0284 0.01409 0.00845 0.0060 0.0118 1.0000
9.750 1.0525 0.01454 0.00893 0.0065 0.0109 1.0000
10.000 1.0760 0.01507 0.00948 0.0071 0.0100 1.0000
10.250 1.0999 0.01552 0.00998 0.0076 0.0096 1.0000
10.500 1.1233 0.01601 0.01052 0.0081 0.0092 1.0000
10.750 1.1462 0.01654 0.01110 0.0087 0.0087 1.0000
11.000 1.1687 0.01710 0.01170 0.0093 0.0083 1.0000
11.250 1.1906 0.01772 0.01238 0.0100 0.0079 1.0000
11.500 1.2114 0.01844 0.01315 0.0107 0.0075 1.0000
11.750 1.2317 0.01918 0.01397 0.0116 0.0072 1.0000
12.000 1.2521 0.01985 0.01471 0.0123 0.0071 1.0000
12.250 1.2716 0.02057 0.01551 0.0132 0.0069 1.0000
12.500 1.2903 0.02133 0.01636 0.0141 0.0068 1.0000
12.750 1.3079 0.02215 0.01725 0.0151 0.0066 1.0000
13.000 1.3244 0.02300 0.01819 0.0162 0.0064 1.0000
13.250 1.3396 0.02388 0.01916 0.0174 0.0062 1.0000
13.500 1.3527 0.02485 0.02020 0.0187 0.0060 1.0000
13.750 1.3633 0.02584 0.02127 0.0204 0.0059 1.0000
14.000 1.3667 0.02696 0.02247 0.0229 0.0058 1.0000
14.250 1.3682 0.02830 0.02391 0.0250 0.0057 1.0000
14.500 1.3669 0.03014 0.02584 0.0262 0.0055 1.0000
14.750 1.3646 0.03251 0.02833 0.0264 0.0055 1.0000
15.000 1.3592 0.03560 0.03154 0.0258 0.0053 1.0000
15.250 1.3552 0.03883 0.03489 0.0247 0.0053 1.0000
15.500 1.3460 0.04291 0.03911 0.0230 0.0052 1.0000
15.750 1.3353 0.04746 0.04379 0.0208 0.0052 1.0000
16.000 1.3176 0.05333 0.04981 0.0176 0.0052 1.0000
16.250 1.3018 0.05928 0.05591 0.0142 0.0052 1.0000
16.500 1.2803 0.06652 0.06330 0.0099 0.0052 1.0000
16.750 1.2492 0.07585 0.07280 0.0044 0.0052 1.0000
17.000 1.2188 0.08555 0.08266 -0.0013 0.0052 1.0000
17.250 1.1904 0.09519 0.09245 -0.0069 0.0054 1.0000
17.500 1.1481 0.10794 0.10536 -0.0142 0.0054 1.0000
17.750 1.1067 0.12099 0.11858 -0.0218 0.0055 1.0000
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