LWK 80-100 (lwk80100-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: LWK 80-100 (lwk80100-il) Reynolds number: 1,000,000 Max Cl/Cd: 61.39 at α=7.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-lwk80100-il-1000000-n5.txt Download as CSV file: xf-lwk80100-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: LWK 80-100
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
------ -------- --------- --------- -------- -------- --------
-15.750 -1.1445 0.07063 0.06842 -0.0154 1.0000 0.0036
-15.500 -1.1827 0.05895 0.05648 -0.0236 1.0000 0.0035
-15.250 -1.2088 0.05157 0.04889 -0.0275 1.0000 0.0034
-15.000 -1.2379 0.04498 0.04203 -0.0294 1.0000 0.0034
-14.750 -1.2291 0.04335 0.04036 -0.0296 1.0000 0.0035
-14.500 -1.2334 0.04035 0.03723 -0.0296 1.0000 0.0036
-14.250 -1.2432 0.03700 0.03369 -0.0290 1.0000 0.0036
-14.000 -1.2389 0.03519 0.03176 -0.0283 1.0000 0.0037
-13.750 -1.2386 0.03306 0.02949 -0.0271 1.0000 0.0037
-13.500 -1.2294 0.03183 0.02817 -0.0262 1.0000 0.0039
-13.250 -1.2304 0.02972 0.02588 -0.0243 1.0000 0.0039
-13.000 -1.2191 0.02875 0.02483 -0.0231 1.0000 0.0040
-12.750 -1.2160 0.02710 0.02301 -0.0208 1.0000 0.0040
-12.500 -1.2017 0.02640 0.02224 -0.0194 1.0000 0.0043
-12.250 -1.1931 0.02517 0.02087 -0.0173 1.0000 0.0043
-12.000 -1.1795 0.02408 0.01966 -0.0158 1.0000 0.0044
-11.750 -1.1637 0.02315 0.01862 -0.0146 1.0000 0.0045
-11.500 -1.1477 0.02219 0.01754 -0.0133 1.0000 0.0045
-11.250 -1.1302 0.02136 0.01659 -0.0122 1.0000 0.0045
-10.750 -1.0953 0.01952 0.01452 -0.0098 1.0000 0.0047
-10.250 -1.0663 0.01763 0.01244 -0.0058 0.9924 0.0052
-10.000 -1.0259 0.01674 0.01144 -0.0095 0.9633 0.0054
-9.750 -0.9815 0.01592 0.01053 -0.0140 0.9515 0.0058
-9.500 -0.9379 0.01526 0.00976 -0.0182 0.9388 0.0061
-9.250 -0.8983 0.01464 0.00904 -0.0215 0.9244 0.0064
-9.000 -0.8660 0.01419 0.00847 -0.0230 0.9091 0.0070
-8.750 -0.8393 0.01378 0.00796 -0.0232 0.8959 0.0072
-8.250 -0.7935 0.01284 0.00682 -0.0219 0.8764 0.0077
-8.000 -0.7708 0.01245 0.00637 -0.0212 0.8691 0.0086
-7.750 -0.7477 0.01210 0.00597 -0.0205 0.8628 0.0092
-7.500 -0.7242 0.01182 0.00563 -0.0198 0.8572 0.0099
-7.250 -0.7005 0.01153 0.00528 -0.0192 0.8525 0.0104
-7.000 -0.6774 0.01119 0.00493 -0.0184 0.8475 0.0124
-6.750 -0.6537 0.01092 0.00463 -0.0178 0.8429 0.0145
-6.500 -0.6295 0.01069 0.00436 -0.0172 0.8388 0.0159
-6.250 -0.6058 0.01040 0.00408 -0.0165 0.8347 0.0193
-6.000 -0.5813 0.01019 0.00384 -0.0160 0.8310 0.0214
-5.500 -0.5323 0.00974 0.00338 -0.0149 0.8240 0.0282
-5.250 -0.5072 0.00955 0.00317 -0.0144 0.8203 0.0309
-5.000 -0.4828 0.00932 0.00297 -0.0139 0.8169 0.0382
-4.750 -0.4577 0.00915 0.00278 -0.0134 0.8139 0.0438
-4.500 -0.4328 0.00894 0.00261 -0.0129 0.8110 0.0517
-4.250 -0.4078 0.00873 0.00243 -0.0124 0.8076 0.0623
-4.000 -0.3826 0.00856 0.00228 -0.0120 0.8043 0.0719
-3.750 -0.3574 0.00838 0.00213 -0.0115 0.8013 0.0842
-3.500 -0.3328 0.00817 0.00198 -0.0110 0.7985 0.1053
-3.250 -0.3080 0.00794 0.00184 -0.0105 0.7955 0.1287
-3.000 -0.2839 0.00766 0.00170 -0.0098 0.7924 0.1653
-2.750 -0.2604 0.00736 0.00156 -0.0091 0.7893 0.2113
-2.500 -0.2373 0.00703 0.00142 -0.0083 0.7863 0.2666
-2.250 -0.2151 0.00666 0.00127 -0.0073 0.7835 0.3359
-2.000 -0.1921 0.00633 0.00116 -0.0065 0.7804 0.3970
-1.750 -0.1713 0.00587 0.00102 -0.0052 0.7772 0.4856
-1.500 -0.1518 0.00541 0.00091 -0.0036 0.7739 0.5838
-1.250 -0.1286 0.00521 0.00087 -0.0026 0.7708 0.6368
-1.000 -0.1034 0.00512 0.00086 -0.0020 0.7675 0.6688
-0.750 -0.0783 0.00504 0.00088 -0.0013 0.7627 0.6993
-0.500 -0.0524 0.00502 0.00087 -0.0009 0.7565 0.7151
-0.250 -0.0262 0.00500 0.00087 -0.0004 0.7479 0.7287
0.000 -0.0001 0.00501 0.00086 0.0000 0.7384 0.7396
0.250 0.0260 0.00500 0.00087 0.0005 0.7274 0.7482
0.500 0.0526 0.00502 0.00087 0.0008 0.7159 0.7560
0.750 0.0783 0.00504 0.00087 0.0014 0.6981 0.7623
1.000 0.1034 0.00512 0.00086 0.0020 0.6681 0.7675
1.250 0.1285 0.00522 0.00087 0.0026 0.6344 0.7707
1.500 0.1518 0.00542 0.00091 0.0036 0.5823 0.7739
1.750 0.1700 0.00596 0.00104 0.0055 0.4680 0.7773
2.000 0.1917 0.00636 0.00117 0.0066 0.3905 0.7806
2.250 0.2150 0.00667 0.00128 0.0074 0.3336 0.7835
2.500 0.2382 0.00698 0.00141 0.0082 0.2780 0.7863
2.750 0.2607 0.00734 0.00155 0.0091 0.2157 0.7893
3.000 0.2834 0.00770 0.00170 0.0099 0.1576 0.7924
3.250 0.3081 0.00794 0.00183 0.0105 0.1292 0.7955
3.750 0.3575 0.00838 0.00213 0.0115 0.0846 0.8013
4.000 0.3826 0.00855 0.00228 0.0120 0.0723 0.8043
4.250 0.4080 0.00873 0.00243 0.0124 0.0635 0.8077
4.500 0.4329 0.00894 0.00261 0.0129 0.0528 0.8110
4.750 0.4577 0.00915 0.00278 0.0134 0.0431 0.8139
5.000 0.4827 0.00933 0.00296 0.0139 0.0369 0.8169
5.250 0.5072 0.00955 0.00316 0.0144 0.0304 0.8204
5.500 0.5323 0.00974 0.00337 0.0149 0.0278 0.8241
6.000 0.5813 0.01018 0.00384 0.0160 0.0211 0.8309
6.250 0.6056 0.01042 0.00408 0.0166 0.0181 0.8347
6.500 0.6294 0.01069 0.00436 0.0172 0.0150 0.8388
6.750 0.6534 0.01095 0.00464 0.0178 0.0129 0.8429
7.000 0.6767 0.01126 0.00498 0.0186 0.0107 0.8475
7.250 0.7005 0.01153 0.00529 0.0192 0.0102 0.8524
7.500 0.7240 0.01184 0.00564 0.0199 0.0091 0.8573
7.750 0.7471 0.01217 0.00602 0.0206 0.0085 0.8628
8.000 0.7698 0.01255 0.00645 0.0214 0.0079 0.8691
8.250 0.7920 0.01301 0.00701 0.0222 0.0073 0.8765
8.750 0.8393 0.01379 0.00797 0.0233 0.0069 0.8961
9.000 0.8659 0.01420 0.00848 0.0231 0.0066 0.9092
9.250 0.8977 0.01476 0.00917 0.0216 0.0064 0.9248
9.500 0.9377 0.01539 0.00991 0.0182 0.0059 0.9394
9.750 0.9816 0.01607 0.01070 0.0139 0.0057 0.9522
10.000 1.0263 0.01686 0.01157 0.0094 0.0053 0.9641
10.250 1.0583 0.01781 0.01262 0.0076 0.0051 1.0000
10.500 1.0761 0.01876 0.01368 0.0088 0.0049 1.0000
10.750 1.0926 0.01985 0.01490 0.0102 0.0047 1.0000
11.000 1.1090 0.02089 0.01606 0.0115 0.0046 1.0000
11.250 1.1273 0.02167 0.01695 0.0126 0.0046 1.0000
11.500 1.1443 0.02259 0.01799 0.0138 0.0045 1.0000
11.750 1.1594 0.02363 0.01915 0.0151 0.0045 1.0000
12.000 1.1763 0.02443 0.02004 0.0162 0.0044 1.0000
12.250 1.1921 0.02524 0.02095 0.0174 0.0043 1.0000
12.500 1.1987 0.02665 0.02251 0.0198 0.0042 1.0000
12.750 1.2078 0.02779 0.02378 0.0217 0.0041 1.0000
13.000 1.2158 0.02904 0.02515 0.0234 0.0041 1.0000
13.250 1.2212 0.03055 0.02679 0.0251 0.0039 1.0000
13.500 1.2164 0.03302 0.02947 0.0270 0.0040 1.0000
13.750 1.2360 0.03332 0.02976 0.0273 0.0038 1.0000
14.000 1.2345 0.03563 0.03224 0.0284 0.0037 1.0000
14.250 1.2316 0.03820 0.03498 0.0292 0.0037 1.0000
14.500 1.2202 0.04183 0.03881 0.0296 0.0036 1.0000
14.750 1.2211 0.04431 0.04139 0.0294 0.0036 1.0000
15.000 1.2021 0.04948 0.04676 0.0281 0.0036 1.0000
15.250 1.1865 0.05487 0.05232 0.0257 0.0036 1.0000
15.500 1.1279 0.06976 0.06756 0.0157 0.0037 1.0000
15.750 1.1382 0.07235 0.07017 0.0140 0.0036 1.0000
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