Glenn Martin 2 (glennmartin2-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: Glenn Martin 2 (glennmartin2-il) Reynolds number: 1,000,000 Max Cl/Cd: 101.34 at α=6.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-glennmartin2-il-1000000-n5.txt Download as CSV file: xf-glennmartin2-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: Glenn Martin 2
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
------ -------- --------- --------- -------- -------- --------
-13.750 -0.3510 0.08424 0.08230 -0.0881 0.9759 0.0082
-13.500 -0.6516 0.02606 0.02286 -0.1339 0.9379 0.0070
-13.250 -0.6314 0.02310 0.01965 -0.1355 0.9324 0.0073
-13.000 -0.6106 0.02145 0.01782 -0.1357 0.9258 0.0075
-12.750 -0.5859 0.02011 0.01632 -0.1363 0.9203 0.0078
-12.500 -0.5661 0.01912 0.01518 -0.1354 0.9134 0.0080
-12.250 -0.5434 0.01821 0.01413 -0.1350 0.9061 0.0082
-12.000 -0.5232 0.01744 0.01321 -0.1338 0.8967 0.0084
-11.750 -0.5015 0.01676 0.01238 -0.1329 0.8874 0.0086
-11.500 -0.4820 0.01620 0.01170 -0.1314 0.8790 0.0088
-11.250 -0.4618 0.01557 0.01094 -0.1300 0.8716 0.0091
-11.000 -0.4428 0.01495 0.01024 -0.1284 0.8646 0.0096
-10.750 -0.4219 0.01443 0.00961 -0.1270 0.8572 0.0100
-10.500 -0.4013 0.01402 0.00911 -0.1255 0.8473 0.0105
-10.250 -0.3803 0.01363 0.00861 -0.1240 0.8371 0.0110
-10.000 -0.3589 0.01327 0.00815 -0.1226 0.8275 0.0114
-9.750 -0.3377 0.01288 0.00766 -0.1211 0.8174 0.0120
-9.500 -0.3164 0.01254 0.00724 -0.1196 0.8057 0.0127
-9.250 -0.2953 0.01225 0.00687 -0.1181 0.7923 0.0137
-9.000 -0.2747 0.01202 0.00652 -0.1164 0.7731 0.0144
-8.750 -0.2570 0.01188 0.00622 -0.1140 0.7401 0.0151
-8.500 -0.2417 0.01181 0.00595 -0.1112 0.6969 0.0161
-8.250 -0.2248 0.01179 0.00577 -0.1087 0.6622 0.0173
-8.000 -0.2042 0.01168 0.00554 -0.1070 0.6443 0.0183
-7.750 -0.1821 0.01157 0.00534 -0.1056 0.6319 0.0194
-7.500 -0.1592 0.01140 0.00513 -0.1045 0.6238 0.0205
-7.250 -0.1354 0.01127 0.00495 -0.1034 0.6173 0.0217
-7.000 -0.1115 0.01113 0.00475 -0.1024 0.6108 0.0226
-6.750 -0.0881 0.01103 0.00458 -0.1013 0.6040 0.0234
-6.500 -0.0639 0.01090 0.00440 -0.1003 0.5967 0.0242
-6.250 -0.0409 0.01072 0.00416 -0.0991 0.5897 0.0254
-6.000 -0.0166 0.01057 0.00399 -0.0982 0.5833 0.0266
-5.750 0.0074 0.01047 0.00385 -0.0973 0.5762 0.0279
-5.500 0.0312 0.01036 0.00368 -0.0962 0.5685 0.0287
-5.250 0.0545 0.01027 0.00352 -0.0951 0.5577 0.0293
-5.000 0.0780 0.01020 0.00339 -0.0940 0.5452 0.0300
-4.750 0.0993 0.01010 0.00320 -0.0924 0.5244 0.0318
-4.500 0.1097 0.01043 0.00317 -0.0888 0.4379 0.0328
-4.250 0.1283 0.01054 0.00312 -0.0868 0.4057 0.0339
-4.000 0.1495 0.01057 0.00305 -0.0852 0.3878 0.0351
-3.750 0.1715 0.01056 0.00297 -0.0839 0.3752 0.0364
-3.500 0.1936 0.01056 0.00290 -0.0826 0.3647 0.0377
-3.250 0.2161 0.01050 0.00282 -0.0813 0.3572 0.0414
-3.000 0.2382 0.01048 0.00276 -0.0800 0.3500 0.0449
-2.750 0.2609 0.01043 0.00273 -0.0788 0.3451 0.0517
-2.500 0.2827 0.01041 0.00270 -0.0775 0.3399 0.0580
-2.000 0.3256 0.01041 0.00266 -0.0746 0.3314 0.0666
-1.750 0.3469 0.01038 0.00262 -0.0731 0.3282 0.0702
-1.500 0.3682 0.01037 0.00260 -0.0716 0.3249 0.0737
-1.250 0.3895 0.01038 0.00259 -0.0702 0.3214 0.0768
-0.750 0.4330 0.01043 0.00259 -0.0675 0.3159 0.0801
-0.500 0.4548 0.01043 0.00258 -0.0662 0.3139 0.0835
-0.250 0.4764 0.01043 0.00259 -0.0649 0.3118 0.0878
0.000 0.4980 0.01045 0.00262 -0.0636 0.3097 0.0926
0.500 0.5407 0.01052 0.00269 -0.0609 0.3049 0.1070
0.750 0.5610 0.01054 0.00275 -0.0593 0.3023 0.1266
1.000 0.5798 0.01049 0.00286 -0.0576 0.3003 0.1924
1.250 0.6018 0.01053 0.00294 -0.0564 0.2993 0.2093
1.500 0.6239 0.01059 0.00302 -0.0553 0.2979 0.2205
1.750 0.6460 0.01065 0.00311 -0.0542 0.2965 0.2297
2.000 0.6681 0.01073 0.00319 -0.0531 0.2950 0.2369
2.250 0.6896 0.01081 0.00328 -0.0519 0.2934 0.2432
2.500 0.7112 0.01090 0.00338 -0.0507 0.2919 0.2487
3.000 0.7537 0.01111 0.00360 -0.0484 0.2887 0.2606
3.250 0.7748 0.01123 0.00372 -0.0472 0.2870 0.2669
3.500 0.7953 0.01136 0.00385 -0.0459 0.2847 0.2720
3.750 0.8173 0.01143 0.00396 -0.0449 0.2834 0.2793
4.000 0.8389 0.01153 0.00408 -0.0439 0.2819 0.2872
4.250 0.8603 0.01162 0.00421 -0.0428 0.2806 0.2980
4.500 0.8814 0.01172 0.00435 -0.0417 0.2788 0.3120
4.750 0.9019 0.01182 0.00450 -0.0406 0.2775 0.3297
5.250 1.1180 0.01147 0.00563 -0.0779 0.2687 0.9952
5.500 1.1567 0.01164 0.00579 -0.0808 0.2657 0.9977
5.750 1.1977 0.01183 0.00597 -0.0843 0.2617 0.9995
6.000 1.2215 0.01207 0.00616 -0.0840 0.2561 1.0000
6.250 1.2394 0.01223 0.00632 -0.0824 0.2509 1.0000
6.500 1.2568 0.01242 0.00651 -0.0807 0.2469 1.0000
6.750 1.2724 0.01268 0.00674 -0.0787 0.2403 1.0000
7.000 1.2870 0.01301 0.00699 -0.0766 0.2277 1.0000
7.250 1.3017 0.01335 0.00728 -0.0746 0.2159 1.0000
7.500 1.3049 0.01420 0.00791 -0.0707 0.1822 1.0000
7.750 1.3035 0.01533 0.00882 -0.0661 0.1491 1.0000
8.000 1.3130 0.01600 0.00942 -0.0635 0.1351 1.0000
8.250 1.3120 0.01723 0.01044 -0.0593 0.1037 1.0000
8.500 1.2891 0.01969 0.01255 -0.0521 0.0381 1.0000
8.750 1.2920 0.02085 0.01368 -0.0490 0.0146 1.0000
9.000 1.3051 0.02148 0.01433 -0.0473 0.0132 1.0000
9.250 1.3173 0.02216 0.01505 -0.0456 0.0121 1.0000
9.500 1.3290 0.02291 0.01583 -0.0440 0.0112 1.0000
9.750 1.3403 0.02370 0.01666 -0.0423 0.0102 1.0000
10.000 1.3515 0.02452 0.01752 -0.0407 0.0098 1.0000
10.250 1.3623 0.02540 0.01843 -0.0392 0.0092 1.0000
10.500 1.3721 0.02636 0.01943 -0.0376 0.0087 1.0000
10.750 1.3810 0.02741 0.02053 -0.0361 0.0083 1.0000
11.000 1.3883 0.02862 0.02179 -0.0345 0.0078 1.0000
11.250 1.3968 0.02979 0.02301 -0.0331 0.0075 1.0000
11.500 1.4045 0.03105 0.02432 -0.0317 0.0071 1.0000
11.750 1.4113 0.03244 0.02575 -0.0305 0.0067 1.0000
12.000 1.4173 0.03394 0.02731 -0.0292 0.0065 1.0000
12.250 1.4224 0.03560 0.02902 -0.0281 0.0063 1.0000
12.500 1.4245 0.03760 0.03108 -0.0270 0.0059 1.0000
12.750 1.4273 0.03961 0.03316 -0.0260 0.0058 1.0000
13.000 1.4304 0.04169 0.03531 -0.0253 0.0056 1.0000
13.250 1.4301 0.04421 0.03792 -0.0246 0.0056 1.0000
13.500 1.4318 0.04659 0.04037 -0.0241 0.0053 1.0000
13.750 1.4319 0.04917 0.04303 -0.0237 0.0052 1.0000
14.000 1.4293 0.05213 0.04607 -0.0233 0.0050 1.0000
14.250 1.4282 0.05496 0.04896 -0.0231 0.0048 1.0000
14.500 1.4236 0.05828 0.05237 -0.0230 0.0048 1.0000
14.750 1.4178 0.06182 0.05599 -0.0230 0.0046 1.0000
15.000 1.4096 0.06575 0.06002 -0.0232 0.0045 1.0000
15.250 1.3976 0.07036 0.06473 -0.0236 0.0043 1.0000
15.500 1.3876 0.07484 0.06933 -0.0242 0.0044 1.0000
15.750 1.3727 0.08009 0.07470 -0.0250 0.0043 1.0000
16.000 1.3588 0.08533 0.08004 -0.0259 0.0042 1.0000
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Polar data table (+)
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