LWK 80-150/K25 (lwk80150k25-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: LWK 80-150/K25 (lwk80150k25-il) Reynolds number: 1,000,000 Max Cl/Cd: 59.43 at α=3.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-lwk80150k25-il-1000000.txt Download as CSV file: xf-lwk80150k25-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: LWK 80-150/K25
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
------ -------- --------- --------- -------- -------- --------
-19.750 -1.2116 0.10498 0.10179 -0.0108 1.0000 0.0142
-19.500 -1.2300 0.09794 0.09462 -0.0144 1.0000 0.0143
-19.250 -1.2469 0.09130 0.08787 -0.0177 1.0000 0.0144
-19.000 -1.2602 0.08539 0.08184 -0.0206 1.0000 0.0144
-18.750 -1.2726 0.07971 0.07606 -0.0233 1.0000 0.0146
-18.500 -1.2839 0.07438 0.07062 -0.0256 1.0000 0.0147
-18.250 -1.2903 0.06992 0.06606 -0.0275 1.0000 0.0148
-18.000 -1.2983 0.06541 0.06144 -0.0291 1.0000 0.0148
-17.750 -1.2998 0.06186 0.05782 -0.0304 1.0000 0.0151
-17.500 -1.3053 0.05798 0.05382 -0.0314 1.0000 0.0150
-17.250 -1.3080 0.05460 0.05035 -0.0321 1.0000 0.0151
-17.000 -1.3062 0.05184 0.04751 -0.0326 1.0000 0.0153
-16.750 -1.3026 0.04936 0.04495 -0.0329 1.0000 0.0156
-16.500 -1.2989 0.04698 0.04249 -0.0331 1.0000 0.0158
-16.250 -1.2965 0.04456 0.03999 -0.0330 1.0000 0.0159
-16.000 -1.2902 0.04260 0.03796 -0.0329 1.0000 0.0161
-15.750 -1.2882 0.04028 0.03554 -0.0325 1.0000 0.0163
-15.500 -1.2800 0.03862 0.03380 -0.0322 1.0000 0.0165
-15.250 -1.2726 0.03693 0.03204 -0.0318 1.0000 0.0167
-15.000 -1.2659 0.03520 0.03024 -0.0312 1.0000 0.0167
-14.750 -1.2451 0.03380 0.02876 -0.0323 0.9543 0.0170
-14.500 -1.2311 0.03129 0.02608 -0.0345 0.9259 0.0176
-14.250 -1.2142 0.02977 0.02443 -0.0355 0.9102 0.0179
-14.000 -1.1967 0.02851 0.02308 -0.0362 0.9000 0.0183
-13.750 -1.1763 0.02740 0.02189 -0.0371 0.8927 0.0186
-13.500 -1.1542 0.02648 0.02089 -0.0381 0.8863 0.0192
-13.250 -1.1312 0.02538 0.01970 -0.0394 0.8808 0.0195
-13.000 -1.1084 0.02456 0.01879 -0.0402 0.8760 0.0201
-12.750 -1.0892 0.02355 0.01770 -0.0406 0.8713 0.0203
-12.500 -1.0711 0.02235 0.01644 -0.0410 0.8669 0.0212
-12.250 -1.0480 0.02144 0.01545 -0.0420 0.8630 0.0214
-12.000 -1.0264 0.02072 0.01471 -0.0423 0.8595 0.0223
-11.750 -1.0049 0.02005 0.01400 -0.0424 0.8559 0.0231
-11.500 -0.9812 0.01949 0.01338 -0.0428 0.8525 0.0239
-11.250 -0.9589 0.01877 0.01259 -0.0432 0.8491 0.0248
-11.000 -0.9354 0.01803 0.01181 -0.0438 0.8453 0.0260
-10.750 -0.9152 0.01746 0.01123 -0.0434 0.8425 0.0270
-10.500 -0.8936 0.01695 0.01069 -0.0432 0.8394 0.0280
-10.250 -0.8724 0.01642 0.01011 -0.0429 0.8364 0.0291
-10.000 -0.8517 0.01584 0.00952 -0.0426 0.8335 0.0308
-9.750 -0.8285 0.01543 0.00908 -0.0426 0.8306 0.0328
-9.500 -0.8064 0.01499 0.00860 -0.0423 0.8278 0.0344
-9.250 -0.7880 0.01448 0.00811 -0.0413 0.8253 0.0368
-9.000 -0.7669 0.01414 0.00775 -0.0406 0.8227 0.0393
-8.750 -0.7489 0.01366 0.00728 -0.0394 0.8197 0.0426
-8.500 -0.7289 0.01331 0.00692 -0.0385 0.8171 0.0456
-8.250 -0.7106 0.01290 0.00652 -0.0372 0.8144 0.0499
-8.000 -0.6898 0.01263 0.00622 -0.0363 0.8115 0.0536
-7.750 -0.6734 0.01224 0.00587 -0.0345 0.8096 0.0592
-7.500 -0.6552 0.01195 0.00559 -0.0330 0.8073 0.0639
-7.250 -0.6384 0.01163 0.00530 -0.0311 0.8049 0.0704
-7.000 -0.6211 0.01135 0.00505 -0.0293 0.8023 0.0772
-6.500 -0.5878 0.01088 0.00463 -0.0253 0.7976 0.0938
-6.250 -0.5689 0.01064 0.00442 -0.0237 0.7950 0.1056
-6.000 -0.5498 0.01038 0.00423 -0.0222 0.7932 0.1189
-5.750 -0.5309 0.01009 0.00402 -0.0207 0.7913 0.1361
-5.500 -0.5116 0.00980 0.00381 -0.0192 0.7891 0.1563
-5.250 -0.4932 0.00946 0.00360 -0.0176 0.7868 0.1837
-5.000 -0.4749 0.00910 0.00339 -0.0159 0.7846 0.2172
-4.750 -0.4575 0.00870 0.00316 -0.0141 0.7826 0.2598
-4.500 -0.4402 0.00827 0.00294 -0.0122 0.7806 0.3094
-4.250 -0.4235 0.00784 0.00273 -0.0103 0.7783 0.3673
-4.000 -0.4085 0.00732 0.00250 -0.0080 0.7761 0.4378
-3.750 -0.3939 0.00677 0.00227 -0.0055 0.7742 0.5130
-3.500 -0.3779 0.00633 0.00212 -0.0032 0.7722 0.5855
-3.250 -0.3551 0.00617 0.00207 -0.0022 0.7702 0.6242
-3.000 -0.3302 0.00609 0.00206 -0.0015 0.7681 0.6486
-2.750 -0.3037 0.00606 0.00204 -0.0012 0.7661 0.6644
-2.500 -0.2764 0.00606 0.00202 -0.0011 0.7644 0.6761
-2.250 -0.2491 0.00605 0.00203 -0.0009 0.7626 0.6848
-2.000 -0.2213 0.00610 0.00203 -0.0009 0.7604 0.6927
-1.750 -0.1939 0.00611 0.00208 -0.0007 0.7585 0.7000
-1.500 -0.1665 0.00613 0.00208 -0.0006 0.7567 0.7066
-1.250 -0.1389 0.00613 0.00211 -0.0005 0.7547 0.7133
-1.000 -0.1112 0.00616 0.00215 -0.0004 0.7525 0.7193
-0.750 -0.0836 0.00620 0.00216 -0.0003 0.7500 0.7246
-0.500 -0.0554 0.00618 0.00216 -0.0003 0.7471 0.7299
-0.250 -0.0272 0.00623 0.00219 -0.0002 0.7432 0.7347
0.000 0.0001 0.00623 0.00220 0.0000 0.7392 0.7390
0.250 0.0273 0.00623 0.00219 0.0002 0.7347 0.7431
0.500 0.0554 0.00618 0.00215 0.0003 0.7297 0.7472
0.750 0.0836 0.00620 0.00216 0.0003 0.7244 0.7501
1.000 0.1113 0.00617 0.00215 0.0004 0.7195 0.7524
1.250 0.1390 0.00613 0.00211 0.0005 0.7133 0.7546
1.500 0.1665 0.00614 0.00209 0.0006 0.7067 0.7568
1.750 0.1939 0.00611 0.00208 0.0007 0.6999 0.7585
2.000 0.2212 0.00610 0.00203 0.0009 0.6921 0.7603
2.250 0.2491 0.00605 0.00203 0.0009 0.6847 0.7625
2.500 0.2764 0.00605 0.00202 0.0011 0.6762 0.7644
2.750 0.3037 0.00606 0.00204 0.0012 0.6644 0.7662
3.000 0.3302 0.00609 0.00206 0.0015 0.6486 0.7682
3.250 0.3550 0.00617 0.00207 0.0022 0.6235 0.7702
3.500 0.3774 0.00635 0.00212 0.0033 0.5823 0.7722
3.750 0.3939 0.00678 0.00227 0.0055 0.5128 0.7741
4.000 0.4087 0.00731 0.00250 0.0080 0.4394 0.7760
4.250 0.4241 0.00781 0.00272 0.0102 0.3717 0.7783
4.500 0.4409 0.00824 0.00293 0.0121 0.3134 0.7806
4.750 0.4578 0.00868 0.00316 0.0140 0.2614 0.7826
5.000 0.4750 0.00910 0.00339 0.0159 0.2182 0.7846
5.250 0.4936 0.00945 0.00360 0.0175 0.1862 0.7868
5.500 0.5122 0.00978 0.00381 0.0191 0.1583 0.7891
5.750 0.5305 0.01011 0.00402 0.0208 0.1339 0.7913
6.000 0.5497 0.01039 0.00423 0.0223 0.1182 0.7931
6.250 0.5686 0.01065 0.00443 0.0238 0.1042 0.7951
6.500 0.5878 0.01088 0.00463 0.0253 0.0936 0.7976
6.750 0.6039 0.01114 0.00484 0.0274 0.0836 0.7999
7.000 0.6213 0.01135 0.00505 0.0293 0.0775 0.8024
7.250 0.6385 0.01162 0.00530 0.0311 0.0707 0.8049
7.500 0.6556 0.01194 0.00558 0.0329 0.0642 0.8073
7.750 0.6737 0.01224 0.00587 0.0345 0.0592 0.8096
8.000 0.6900 0.01263 0.00622 0.0363 0.0540 0.8115
8.250 0.7109 0.01290 0.00652 0.0372 0.0502 0.8144
8.500 0.7292 0.01331 0.00692 0.0384 0.0459 0.8171
8.750 0.7496 0.01364 0.00727 0.0393 0.0430 0.8197
9.000 0.7677 0.01412 0.00773 0.0405 0.0392 0.8226
9.250 0.7885 0.01447 0.00810 0.0412 0.0369 0.8253
9.500 0.8073 0.01496 0.00857 0.0422 0.0344 0.8278
9.750 0.8292 0.01542 0.00907 0.0424 0.0328 0.8306
10.000 0.8522 0.01586 0.00953 0.0425 0.0309 0.8335
10.250 0.8730 0.01643 0.01012 0.0428 0.0291 0.8364
10.500 0.8944 0.01696 0.01069 0.0431 0.0278 0.8394
10.750 0.9163 0.01744 0.01120 0.0433 0.0266 0.8425
11.000 0.9367 0.01801 0.01177 0.0436 0.0254 0.8453
11.250 0.9590 0.01885 0.01266 0.0431 0.0242 0.8490
11.500 0.9832 0.01943 0.01332 0.0426 0.0237 0.8524
11.750 1.0052 0.02014 0.01409 0.0423 0.0230 0.8559
12.000 1.0273 0.02077 0.01476 0.0420 0.0224 0.8594
12.250 1.0489 0.02149 0.01551 0.0417 0.0216 0.8628
12.500 1.0697 0.02261 0.01669 0.0409 0.0206 0.8670
12.750 1.0889 0.02372 0.01788 0.0404 0.0203 0.8713
13.000 1.1120 0.02441 0.01865 0.0397 0.0199 0.8758
13.250 1.1334 0.02535 0.01967 0.0390 0.0195 0.8806
13.500 1.1578 0.02633 0.02073 0.0376 0.0190 0.8860
13.750 1.1777 0.02744 0.02193 0.0368 0.0186 0.8924
14.000 1.1964 0.02867 0.02326 0.0360 0.0183 0.9000
14.250 1.2156 0.02979 0.02445 0.0352 0.0179 0.9100
14.500 1.2308 0.03145 0.02623 0.0343 0.0174 0.9260
14.750 1.2460 0.03386 0.02882 0.0320 0.0170 0.9545
15.000 1.2631 0.03557 0.03062 0.0312 0.0167 1.0000
15.250 1.2716 0.03715 0.03227 0.0317 0.0166 1.0000
15.500 1.2816 0.03861 0.03381 0.0320 0.0163 1.0000
15.750 1.2886 0.04039 0.03566 0.0323 0.0162 1.0000
16.000 1.2953 0.04225 0.03759 0.0325 0.0160 1.0000
16.250 1.2979 0.04459 0.04002 0.0328 0.0158 1.0000
16.500 1.3017 0.04687 0.04238 0.0328 0.0157 1.0000
16.750 1.3049 0.04929 0.04488 0.0326 0.0155 1.0000
17.000 1.3075 0.05190 0.04757 0.0323 0.0153 1.0000
17.250 1.3064 0.05499 0.05075 0.0317 0.0152 1.0000
17.500 1.3034 0.05843 0.05429 0.0310 0.0151 1.0000
17.750 1.2989 0.06220 0.05816 0.0299 0.0150 1.0000
18.000 1.2979 0.06571 0.06175 0.0287 0.0149 1.0000
18.250 1.2921 0.06997 0.06610 0.0270 0.0147 1.0000
18.500 1.2847 0.07457 0.07080 0.0251 0.0146 1.0000
18.750 1.2739 0.07988 0.07620 0.0227 0.0144 1.0000
19.000 1.2612 0.08560 0.08204 0.0200 0.0143 1.0000
19.250 1.2505 0.09111 0.08768 0.0173 0.0144 1.0000
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