LWK 80-080 (lwk80080-il) Xfoil prediction polar at RE=200,000 Ncrit=5
| Details | Polar file |
|---|---|
|
Airfoil: LWK 80-080 (lwk80080-il) Reynolds number: 200,000 Max Cl/Cd: 35.7 at α=4.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-lwk80080-il-200000-n5.txt Download as CSV file: xf-lwk80080-il-200000-n5.csv |
XFOIL Version 6.96
Calculated polar for: LWK 80-080
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.200 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-9.750 -0.6717 0.08298 0.07953 -0.0114 1.0000 0.0114
-9.500 -0.6847 0.07412 0.07069 -0.0195 1.0000 0.0113
-9.250 -0.7005 0.06780 0.06430 -0.0237 1.0000 0.0111
-9.000 -0.7160 0.06306 0.05946 -0.0243 1.0000 0.0110
-8.750 -0.7290 0.05807 0.05432 -0.0238 1.0000 0.0109
-8.500 -0.7381 0.05284 0.04886 -0.0227 1.0000 0.0109
-8.250 -0.7423 0.04793 0.04368 -0.0211 1.0000 0.0108
-8.000 -0.7443 0.04288 0.03826 -0.0190 1.0000 0.0106
-7.750 -0.7432 0.03791 0.03285 -0.0164 1.0000 0.0108
-7.500 -0.7371 0.03372 0.02818 -0.0139 1.0000 0.0109
-7.250 -0.7269 0.03011 0.02407 -0.0115 1.0000 0.0111
-7.000 -0.7127 0.02706 0.02051 -0.0093 1.0000 0.0119
-6.750 -0.6929 0.02584 0.01896 -0.0079 1.0000 0.0130
-6.500 -0.6768 0.02305 0.01581 -0.0061 1.0000 0.0138
-6.250 -0.6578 0.02140 0.01398 -0.0048 1.0000 0.0148
-6.000 -0.6378 0.01993 0.01233 -0.0033 1.0000 0.0155
-5.750 -0.6178 0.01869 0.01096 -0.0019 1.0000 0.0163
-5.500 -0.5987 0.01759 0.00970 -0.0003 1.0000 0.0174
-5.250 -0.5807 0.01664 0.00866 0.0015 1.0000 0.0186
-5.000 -0.5642 0.01585 0.00777 0.0035 1.0000 0.0201
-4.750 -0.5395 0.01486 0.00673 0.0037 0.9916 0.0249
-4.500 -0.5078 0.01433 0.00612 0.0026 0.9842 0.0318
-4.250 -0.4769 0.01366 0.00544 0.0015 0.9771 0.0424
-4.000 -0.4450 0.01310 0.00485 0.0003 0.9707 0.0573
-3.750 -0.4136 0.01251 0.00433 -0.0009 0.9646 0.0846
-3.500 -0.3826 0.01189 0.00390 -0.0021 0.9585 0.1310
-3.250 -0.3535 0.01108 0.00350 -0.0031 0.9525 0.2309
-3.000 -0.3310 0.00992 0.00312 -0.0028 0.9449 0.4147
-2.750 -0.3118 0.00896 0.00306 -0.0011 0.9379 0.6268
-2.500 -0.2844 0.00884 0.00313 -0.0007 0.9319 0.7091
-2.250 -0.2534 0.00884 0.00313 -0.0011 0.9275 0.7488
-2.000 -0.2264 0.00887 0.00314 -0.0007 0.9212 0.7758
-1.750 -0.1979 0.00892 0.00318 -0.0004 0.9160 0.8023
-1.500 -0.1694 0.00898 0.00324 -0.0001 0.9114 0.8253
-1.250 -0.1432 0.00902 0.00327 0.0005 0.9055 0.8422
-1.000 -0.1135 0.00904 0.00327 0.0003 0.9010 0.8540
-0.750 -0.0854 0.00904 0.00325 0.0004 0.8957 0.8622
-0.500 -0.0576 0.00904 0.00322 0.0004 0.8902 0.8693
-0.250 -0.0275 0.00903 0.00319 -0.0001 0.8860 0.8747
0.000 0.0000 0.00903 0.00319 0.0000 0.8801 0.8801
0.250 0.0275 0.00903 0.00319 0.0001 0.8747 0.8860
0.500 0.0577 0.00904 0.00322 -0.0004 0.8694 0.8902
0.750 0.0854 0.00904 0.00325 -0.0004 0.8621 0.8957
1.000 0.1134 0.00904 0.00327 -0.0003 0.8538 0.9009
1.250 0.1431 0.00902 0.00327 -0.0005 0.8419 0.9055
1.500 0.1694 0.00898 0.00324 0.0001 0.8253 0.9113
1.750 0.1979 0.00891 0.00318 0.0005 0.8015 0.9161
2.000 0.2263 0.00886 0.00314 0.0007 0.7748 0.9213
2.250 0.2534 0.00884 0.00313 0.0011 0.7486 0.9275
2.500 0.2846 0.00884 0.00315 0.0006 0.7118 0.9318
2.750 0.3122 0.00895 0.00311 0.0010 0.6329 0.9378
3.000 0.3304 0.00997 0.00313 0.0029 0.4063 0.9450
3.250 0.3529 0.01116 0.00351 0.0031 0.2179 0.9528
3.500 0.3826 0.01190 0.00390 0.0020 0.1293 0.9586
3.750 0.4137 0.01250 0.00433 0.0009 0.0853 0.9647
4.000 0.4451 0.01309 0.00486 -0.0003 0.0579 0.9707
4.250 0.4770 0.01363 0.00540 -0.0015 0.0407 0.9770
4.500 0.5080 0.01425 0.00604 -0.0026 0.0299 0.9840
4.750 0.5384 0.01508 0.00689 -0.0036 0.0218 0.9918
5.000 0.5641 0.01588 0.00781 -0.0035 0.0194 1.0000
5.250 0.5805 0.01669 0.00871 -0.0014 0.0181 1.0000
5.500 0.5985 0.01764 0.00975 0.0004 0.0165 1.0000
5.750 0.6177 0.01873 0.01100 0.0019 0.0160 1.0000
6.000 0.6375 0.01997 0.01236 0.0034 0.0150 1.0000
6.250 0.6576 0.02146 0.01403 0.0048 0.0146 1.0000
6.500 0.6765 0.02324 0.01601 0.0062 0.0138 1.0000
6.750 0.6938 0.02554 0.01867 0.0078 0.0127 1.0000
7.000 0.7121 0.02734 0.02082 0.0094 0.0119 1.0000
7.250 0.7265 0.03022 0.02418 0.0115 0.0113 1.0000
7.500 0.7368 0.03381 0.02827 0.0139 0.0110 1.0000
7.750 0.7436 0.03778 0.03270 0.0163 0.0111 1.0000
8.000 0.7465 0.04224 0.03757 0.0187 0.0110 1.0000
8.250 0.7442 0.04744 0.04315 0.0209 0.0110 1.0000
8.500 0.7375 0.05298 0.04901 0.0227 0.0109 1.0000
8.750 0.7308 0.05769 0.05392 0.0237 0.0111 1.0000
9.000 0.7188 0.06260 0.05899 0.0242 0.0111 1.0000
9.250 0.7026 0.06739 0.06388 0.0237 0.0113 1.0000
9.500 0.6866 0.07364 0.07021 0.0198 0.0115 1.0000
9.750 0.6755 0.08168 0.07825 0.0124 0.0117 1.0000
10.000 0.6664 0.08937 0.08589 0.0067 0.0117 1.0000
|
Polar data table (+)
Polar graphs
<< Back to LWK 80-080 (lwk80080-il)