LWK 79-100 (lwk79100-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: LWK 79-100 (lwk79100-il) Reynolds number: 500,000 Max Cl/Cd: 59.49 at α=5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-lwk79100-il-500000.txt Download as CSV file: xf-lwk79100-il-500000.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 = 0.500 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-14.250 -0.5905 0.15400 0.15190 0.0378 1.0000 0.0264
-14.000 -0.5914 0.15034 0.14824 0.0355 1.0000 0.0273
-13.750 -1.0424 0.06379 0.06046 -0.0148 1.0000 0.0134
-12.750 -1.1154 0.04172 0.03758 -0.0255 1.0000 0.0136
-12.500 -1.1271 0.03812 0.03378 -0.0256 1.0000 0.0137
-12.250 -1.1350 0.03538 0.03086 -0.0244 1.0000 0.0139
-12.000 -1.1387 0.03333 0.02868 -0.0221 1.0000 0.0141
-11.750 -1.1351 0.03171 0.02694 -0.0202 1.0000 0.0144
-11.500 -1.1249 0.03040 0.02554 -0.0188 1.0000 0.0147
-11.250 -1.1127 0.02908 0.02410 -0.0176 1.0000 0.0151
-11.000 -1.0991 0.02774 0.02263 -0.0164 1.0000 0.0156
-10.750 -1.0839 0.02642 0.02116 -0.0153 1.0000 0.0162
-10.500 -1.0663 0.02536 0.01997 -0.0143 1.0000 0.0168
-10.250 -1.0472 0.02444 0.01890 -0.0134 1.0000 0.0174
-10.000 -1.0328 0.02252 0.01682 -0.0122 1.0000 0.0183
-9.750 -1.0142 0.02138 0.01562 -0.0113 1.0000 0.0193
-9.500 -0.9929 0.02062 0.01482 -0.0106 1.0000 0.0203
-9.250 -0.9712 0.01984 0.01395 -0.0098 1.0000 0.0214
-9.000 -0.9487 0.01914 0.01315 -0.0091 1.0000 0.0225
-8.750 -0.9294 0.01787 0.01177 -0.0081 1.0000 0.0240
-8.500 -0.9077 0.01703 0.01091 -0.0074 1.0000 0.0257
-8.250 -0.8836 0.01657 0.01042 -0.0069 1.0000 0.0277
-8.000 -0.8590 0.01615 0.00992 -0.0064 1.0000 0.0294
-7.750 -0.8380 0.01510 0.00881 -0.0055 1.0000 0.0317
-7.500 -0.8144 0.01449 0.00818 -0.0049 1.0000 0.0340
-7.250 -0.7897 0.01403 0.00768 -0.0044 1.0000 0.0364
-7.000 -0.7641 0.01373 0.00732 -0.0040 1.0000 0.0384
-6.750 -0.7419 0.01285 0.00644 -0.0032 1.0000 0.0427
-6.500 -0.7168 0.01245 0.00601 -0.0027 1.0000 0.0463
-6.250 -0.6921 0.01195 0.00546 -0.0021 1.0000 0.0503
-6.000 -0.6675 0.01146 0.00500 -0.0016 1.0000 0.0570
-5.750 -0.6428 0.01096 0.00454 -0.0010 1.0000 0.0666
-5.500 -0.6181 0.01049 0.00414 -0.0004 1.0000 0.0823
-5.250 -0.5935 0.01000 0.00377 0.0001 1.0000 0.1068
-5.000 -0.5688 0.00956 0.00347 0.0006 1.0000 0.1356
-4.750 -0.5440 0.00916 0.00321 0.0011 1.0000 0.1659
-4.250 -0.4945 0.00838 0.00273 0.0021 1.0000 0.2341
-4.000 -0.4702 0.00797 0.00252 0.0027 1.0000 0.2781
-3.750 -0.4339 0.00755 0.00233 0.0006 0.9835 0.3357
-3.500 -0.3822 0.00719 0.00214 -0.0046 0.9151 0.3987
-3.250 -0.3540 0.00717 0.00201 -0.0043 0.8359 0.4419
-3.000 -0.3291 0.00715 0.00195 -0.0035 0.8011 0.4786
-2.750 -0.3029 0.00715 0.00190 -0.0030 0.7794 0.5069
-2.500 -0.2762 0.00714 0.00188 -0.0026 0.7631 0.5301
-2.250 -0.2489 0.00716 0.00185 -0.0022 0.7497 0.5498
-2.000 -0.2214 0.00717 0.00183 -0.0020 0.7381 0.5664
-1.750 -0.1940 0.00720 0.00182 -0.0017 0.7279 0.5814
-1.500 -0.1663 0.00721 0.00180 -0.0014 0.7180 0.5946
-1.250 -0.1386 0.00721 0.00180 -0.0012 0.7088 0.6064
-1.000 -0.1110 0.00724 0.00179 -0.0009 0.7002 0.6180
-0.750 -0.0831 0.00724 0.00179 -0.0007 0.6907 0.6294
-0.500 -0.0553 0.00726 0.00178 -0.0005 0.6803 0.6398
-0.250 -0.0279 0.00727 0.00178 -0.0002 0.6697 0.6492
0.000 0.0000 0.00725 0.00177 0.0000 0.6594 0.6594
0.250 0.0279 0.00727 0.00178 0.0002 0.6493 0.6697
0.500 0.0553 0.00726 0.00178 0.0005 0.6398 0.6803
0.750 0.0831 0.00724 0.00179 0.0007 0.6293 0.6907
1.250 0.1386 0.00721 0.00180 0.0012 0.6065 0.7088
1.500 0.1663 0.00721 0.00180 0.0014 0.5946 0.7180
1.750 0.1939 0.00720 0.00181 0.0017 0.5813 0.7279
2.000 0.2215 0.00717 0.00183 0.0020 0.5664 0.7382
2.250 0.2489 0.00716 0.00185 0.0022 0.5498 0.7497
2.500 0.2762 0.00714 0.00188 0.0026 0.5301 0.7631
2.750 0.3029 0.00715 0.00190 0.0030 0.5069 0.7793
3.000 0.3291 0.00715 0.00195 0.0035 0.4786 0.8011
3.250 0.3540 0.00717 0.00201 0.0043 0.4419 0.8357
3.500 0.3821 0.00719 0.00214 0.0046 0.3987 0.9148
3.750 0.4340 0.00755 0.00233 -0.0006 0.3354 0.9836
4.000 0.4701 0.00797 0.00252 -0.0027 0.2780 1.0000
4.250 0.4944 0.00838 0.00273 -0.0021 0.2339 1.0000
4.750 0.5439 0.00916 0.00321 -0.0011 0.1659 1.0000
5.000 0.5687 0.00956 0.00347 -0.0006 0.1357 1.0000
5.250 0.5935 0.01000 0.00377 -0.0001 0.1068 1.0000
5.500 0.6180 0.01048 0.00414 0.0005 0.0823 1.0000
5.750 0.6428 0.01096 0.00454 0.0010 0.0666 1.0000
6.000 0.6675 0.01145 0.00500 0.0016 0.0569 1.0000
6.250 0.6921 0.01195 0.00547 0.0021 0.0503 1.0000
6.500 0.7168 0.01245 0.00601 0.0027 0.0463 1.0000
6.750 0.7419 0.01285 0.00644 0.0032 0.0427 1.0000
7.000 0.7641 0.01374 0.00734 0.0040 0.0383 1.0000
7.250 0.7897 0.01405 0.00769 0.0044 0.0365 1.0000
7.500 0.8145 0.01449 0.00818 0.0049 0.0340 1.0000
7.750 0.8380 0.01510 0.00881 0.0055 0.0316 1.0000
8.000 0.8590 0.01616 0.00993 0.0064 0.0294 1.0000
8.250 0.8838 0.01656 0.01040 0.0069 0.0276 1.0000
8.500 0.9079 0.01703 0.01091 0.0074 0.0257 1.0000
8.750 0.9294 0.01790 0.01180 0.0081 0.0239 1.0000
9.000 0.9488 0.01917 0.01318 0.0091 0.0225 1.0000
9.250 0.9714 0.01986 0.01397 0.0098 0.0214 1.0000
9.500 0.9933 0.02060 0.01479 0.0105 0.0202 1.0000
9.750 1.0144 0.02138 0.01562 0.0112 0.0193 1.0000
10.000 1.0333 0.02248 0.01678 0.0121 0.0184 1.0000
10.250 1.0473 0.02450 0.01897 0.0134 0.0174 1.0000
10.500 1.0673 0.02524 0.01985 0.0142 0.0168 1.0000
10.750 1.0845 0.02639 0.02113 0.0152 0.0161 1.0000
11.000 1.0997 0.02771 0.02260 0.0163 0.0156 1.0000
11.250 1.1135 0.02905 0.02407 0.0175 0.0151 1.0000
11.500 1.1259 0.03034 0.02547 0.0187 0.0147 1.0000
11.750 1.1360 0.03169 0.02691 0.0200 0.0143 1.0000
12.000 1.1399 0.03330 0.02865 0.0220 0.0141 1.0000
12.250 1.1348 0.03552 0.03099 0.0242 0.0138 1.0000
12.500 1.1280 0.03815 0.03380 0.0254 0.0137 1.0000
12.750 1.1131 0.04215 0.03802 0.0253 0.0136 1.0000
13.000 1.0987 0.04652 0.04260 0.0241 0.0135 1.0000
13.750 0.6181 0.14041 0.13829 -0.0305 0.0206 1.0000
14.000 0.6094 0.14477 0.14266 -0.0330 0.0220 1.0000
14.250 1.0163 0.07629 0.07325 0.0061 0.0135 1.0000
14.500 0.9903 0.08568 0.08282 -0.0004 0.0135 1.0000
14.750 0.9727 0.09409 0.09136 -0.0061 0.0136 1.0000
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