NASA/LANGLEY LS(1)-0013 AIRFOIL (ls013-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: NASA/LANGLEY LS(1)-0013 AIRFOIL (ls013-il) Reynolds number: 500,000 Max Cl/Cd: 57.2 at α=8.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-ls013-il-500000-n5.txt Download as CSV file: xf-ls013-il-500000-n5.csv |
XFOIL Version 6.96
Calculated polar for: NASA/LANGLEY LS(1)-0013 AIRFOIL
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.500 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-18.500 -1.1961 0.11869 0.11561 0.0196 1.0000 0.0154
-18.250 -1.2313 0.10736 0.10410 0.0132 1.0000 0.0154
-18.000 -1.2609 0.09746 0.09402 0.0077 1.0000 0.0154
-17.750 -1.2851 0.08875 0.08514 0.0028 1.0000 0.0154
-17.500 -1.3043 0.08118 0.07740 -0.0013 1.0000 0.0155
-17.250 -1.3193 0.07466 0.07073 -0.0048 1.0000 0.0156
-17.000 -1.3311 0.06895 0.06486 -0.0076 1.0000 0.0158
-16.750 -1.3401 0.06401 0.05978 -0.0097 1.0000 0.0160
-16.500 -1.3475 0.05963 0.05526 -0.0113 1.0000 0.0161
-16.250 -1.3530 0.05575 0.05124 -0.0125 1.0000 0.0163
-16.000 -1.3566 0.05228 0.04764 -0.0132 1.0000 0.0165
-15.750 -1.3584 0.04915 0.04437 -0.0137 1.0000 0.0168
-15.500 -1.3584 0.04634 0.04142 -0.0139 1.0000 0.0170
-15.250 -1.3568 0.04380 0.03875 -0.0138 1.0000 0.0172
-15.000 -1.3533 0.04152 0.03633 -0.0136 1.0000 0.0174
-14.750 -1.3505 0.03923 0.03393 -0.0133 1.0000 0.0177
-14.500 -1.3473 0.03706 0.03168 -0.0128 1.0000 0.0180
-14.250 -1.3409 0.03525 0.02980 -0.0122 1.0000 0.0184
-14.000 -1.3324 0.03367 0.02815 -0.0116 1.0000 0.0187
-13.750 -1.3225 0.03224 0.02663 -0.0109 1.0000 0.0191
-13.500 -1.3119 0.03090 0.02521 -0.0102 1.0000 0.0195
-13.250 -1.3006 0.02962 0.02385 -0.0094 1.0000 0.0199
-13.000 -1.2888 0.02842 0.02254 -0.0085 1.0000 0.0203
-12.750 -1.2760 0.02732 0.02135 -0.0075 1.0000 0.0207
-12.500 -1.2622 0.02632 0.02025 -0.0066 1.0000 0.0211
-12.250 -1.2494 0.02527 0.01913 -0.0054 1.0000 0.0216
-12.000 -1.2372 0.02428 0.01809 -0.0041 1.0000 0.0221
-11.750 -1.2221 0.02349 0.01726 -0.0028 1.0000 0.0226
-11.500 -1.2039 0.02275 0.01647 -0.0020 1.0000 0.0232
-11.250 -1.1841 0.02206 0.01573 -0.0014 1.0000 0.0238
-11.000 -1.1625 0.02148 0.01505 -0.0011 0.9491 0.0246
-10.750 -1.1440 0.02096 0.01442 0.0001 0.9297 0.0252
-10.500 -1.1246 0.02042 0.01377 0.0012 0.9168 0.0259
-10.250 -1.1055 0.01977 0.01307 0.0022 0.9066 0.0267
-10.000 -1.0843 0.01926 0.01250 0.0030 0.8980 0.0275
-9.750 -1.0620 0.01878 0.01196 0.0036 0.8908 0.0285
-9.500 -1.0392 0.01832 0.01143 0.0041 0.8835 0.0295
-9.250 -1.0159 0.01790 0.01091 0.0046 0.8773 0.0306
-9.000 -0.9925 0.01739 0.01036 0.0050 0.8710 0.0318
-8.750 -0.9687 0.01694 0.00988 0.0054 0.8655 0.0331
-8.500 -0.9440 0.01655 0.00943 0.0057 0.8606 0.0345
-8.250 -0.9188 0.01617 0.00899 0.0059 0.8552 0.0359
-8.000 -0.8934 0.01583 0.00858 0.0061 0.8500 0.0371
-7.750 -0.8687 0.01536 0.00810 0.0064 0.8454 0.0389
-7.500 -0.8428 0.01499 0.00771 0.0064 0.8407 0.0409
-7.250 -0.8165 0.01468 0.00735 0.0065 0.8362 0.0428
-7.000 -0.7901 0.01440 0.00700 0.0066 0.8320 0.0444
-6.750 -0.7639 0.01400 0.00661 0.0066 0.8277 0.0469
-6.500 -0.7371 0.01368 0.00628 0.0066 0.8231 0.0493
-6.250 -0.7100 0.01341 0.00597 0.0065 0.8189 0.0518
-6.000 -0.6831 0.01312 0.00565 0.0065 0.8154 0.0550
-5.750 -0.6557 0.01282 0.00537 0.0064 0.8114 0.0590
-5.500 -0.6279 0.01258 0.00511 0.0062 0.8072 0.0630
-5.250 -0.6005 0.01227 0.00483 0.0061 0.8031 0.0695
-5.000 -0.5729 0.01202 0.00457 0.0060 0.7996 0.0766
-4.750 -0.5449 0.01176 0.00434 0.0058 0.7961 0.0857
-4.500 -0.5169 0.01147 0.00411 0.0056 0.7923 0.0980
-4.000 -0.4611 0.01088 0.00366 0.0051 0.7849 0.1356
-3.750 -0.4332 0.01058 0.00344 0.0049 0.7817 0.1618
-3.500 -0.4051 0.01018 0.00323 0.0045 0.7781 0.2008
-3.250 -0.3772 0.00974 0.00301 0.0041 0.7746 0.2552
-3.000 -0.3492 0.00930 0.00281 0.0037 0.7711 0.3141
-2.500 -0.2926 0.00851 0.00242 0.0030 0.7647 0.4248
-2.250 -0.2648 0.00786 0.00226 0.0025 0.7613 0.5388
-2.000 -0.2361 0.00761 0.00225 0.0022 0.7578 0.6042
-1.750 -0.2068 0.00753 0.00224 0.0019 0.7544 0.6308
-1.500 -0.1775 0.00749 0.00224 0.0017 0.7512 0.6543
-1.250 -0.1482 0.00748 0.00227 0.0015 0.7483 0.6755
-1.000 -0.1185 0.00746 0.00230 0.0012 0.7438 0.6909
-0.750 -0.0887 0.00746 0.00228 0.0008 0.7384 0.7006
-0.500 -0.0595 0.00746 0.00226 0.0006 0.7334 0.7068
-0.250 -0.0295 0.00746 0.00227 0.0003 0.7279 0.7150
0.000 0.0000 0.00745 0.00228 0.0000 0.7219 0.7218
0.250 0.0295 0.00746 0.00227 -0.0003 0.7151 0.7280
0.500 0.0595 0.00746 0.00226 -0.0006 0.7068 0.7335
0.750 0.0887 0.00746 0.00228 -0.0008 0.7006 0.7384
1.000 0.1185 0.00746 0.00230 -0.0012 0.6909 0.7437
1.250 0.1482 0.00748 0.00227 -0.0015 0.6753 0.7482
1.500 0.1775 0.00749 0.00224 -0.0017 0.6545 0.7512
1.750 0.2068 0.00753 0.00224 -0.0019 0.6310 0.7544
2.000 0.2361 0.00761 0.00225 -0.0022 0.6037 0.7578
2.250 0.2648 0.00786 0.00226 -0.0025 0.5396 0.7613
2.500 0.2926 0.00851 0.00242 -0.0029 0.4252 0.7647
2.750 0.3209 0.00893 0.00262 -0.0034 0.3659 0.7678
3.000 0.3492 0.00930 0.00281 -0.0037 0.3142 0.7711
3.250 0.3772 0.00974 0.00301 -0.0041 0.2548 0.7746
3.500 0.4051 0.01018 0.00323 -0.0045 0.2010 0.7781
3.750 0.4332 0.01057 0.00344 -0.0049 0.1619 0.7817
4.000 0.4611 0.01088 0.00366 -0.0051 0.1357 0.7849
4.500 0.5169 0.01147 0.00411 -0.0056 0.0979 0.7923
4.750 0.5450 0.01176 0.00434 -0.0058 0.0856 0.7961
5.000 0.5729 0.01202 0.00457 -0.0060 0.0766 0.7996
5.250 0.6006 0.01227 0.00483 -0.0061 0.0695 0.8031
5.500 0.6279 0.01258 0.00511 -0.0063 0.0630 0.8072
5.750 0.6557 0.01282 0.00537 -0.0064 0.0590 0.8114
6.000 0.6832 0.01312 0.00566 -0.0065 0.0550 0.8154
6.250 0.7101 0.01341 0.00597 -0.0066 0.0518 0.8189
6.500 0.7371 0.01368 0.00628 -0.0066 0.0493 0.8230
6.750 0.7640 0.01400 0.00661 -0.0066 0.0469 0.8277
7.000 0.7902 0.01440 0.00700 -0.0066 0.0444 0.8320
7.250 0.8166 0.01468 0.00735 -0.0065 0.0428 0.8362
7.500 0.8429 0.01499 0.00771 -0.0064 0.0408 0.8407
7.750 0.8688 0.01537 0.00810 -0.0064 0.0389 0.8454
8.000 0.8936 0.01583 0.00858 -0.0061 0.0371 0.8500
8.250 0.9190 0.01617 0.00899 -0.0059 0.0359 0.8552
8.500 0.9442 0.01655 0.00943 -0.0057 0.0345 0.8606
8.750 0.9689 0.01694 0.00988 -0.0055 0.0331 0.8655
9.000 0.9926 0.01739 0.01036 -0.0051 0.0318 0.8711
9.250 1.0161 0.01790 0.01091 -0.0047 0.0306 0.8773
9.500 1.0394 0.01832 0.01143 -0.0042 0.0295 0.8835
9.750 1.0622 0.01878 0.01196 -0.0036 0.0285 0.8908
10.000 1.0845 0.01926 0.01250 -0.0030 0.0275 0.8980
10.250 1.1058 0.01978 0.01307 -0.0023 0.0267 0.9065
10.500 1.1250 0.02042 0.01377 -0.0013 0.0259 0.9166
10.750 1.1443 0.02096 0.01442 -0.0002 0.0252 0.9295
11.000 1.1629 0.02148 0.01505 0.0010 0.0245 0.9487
11.250 1.1845 0.02207 0.01573 0.0014 0.0238 1.0000
11.500 1.2043 0.02275 0.01647 0.0020 0.0232 1.0000
11.750 1.2226 0.02349 0.01726 0.0027 0.0226 1.0000
12.000 1.2378 0.02428 0.01809 0.0039 0.0221 1.0000
12.250 1.2500 0.02528 0.01913 0.0053 0.0215 1.0000
12.500 1.2630 0.02630 0.02023 0.0065 0.0211 1.0000
12.750 1.2768 0.02731 0.02134 0.0074 0.0207 1.0000
13.000 1.2896 0.02841 0.02254 0.0083 0.0203 1.0000
13.250 1.3016 0.02961 0.02383 0.0092 0.0199 1.0000
13.500 1.3128 0.03089 0.02520 0.0100 0.0195 1.0000
13.750 1.3235 0.03223 0.02662 0.0108 0.0191 1.0000
14.000 1.3335 0.03366 0.02813 0.0114 0.0187 1.0000
14.250 1.3421 0.03523 0.02978 0.0120 0.0183 1.0000
14.500 1.3485 0.03705 0.03167 0.0126 0.0180 1.0000
14.750 1.3517 0.03922 0.03392 0.0131 0.0177 1.0000
15.000 1.3547 0.04149 0.03631 0.0134 0.0174 1.0000
15.250 1.3583 0.04376 0.03871 0.0136 0.0172 1.0000
15.500 1.3600 0.04630 0.04139 0.0136 0.0170 1.0000
15.750 1.3601 0.04911 0.04433 0.0134 0.0168 1.0000
16.000 1.3584 0.05223 0.04759 0.0130 0.0165 1.0000
16.250 1.3548 0.05569 0.05118 0.0122 0.0163 1.0000
16.500 1.3495 0.05956 0.05519 0.0111 0.0161 1.0000
16.750 1.3425 0.06390 0.05967 0.0095 0.0159 1.0000
17.000 1.3334 0.06885 0.06476 0.0073 0.0158 1.0000
17.250 1.3217 0.07454 0.07060 0.0045 0.0156 1.0000
17.500 1.3067 0.08107 0.07729 0.0010 0.0155 1.0000
17.750 1.2878 0.08860 0.08499 -0.0031 0.0154 1.0000
18.000 1.2633 0.09737 0.09393 -0.0080 0.0154 1.0000
18.250 1.2339 0.10723 0.10397 -0.0135 0.0154 1.0000
18.500 1.1979 0.11872 0.11565 -0.0199 0.0154 1.0000
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