Glenn Martin 2 (glennmartin2-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: Glenn Martin 2 (glennmartin2-il) Reynolds number: 500,000 Max Cl/Cd: 78.56 at α=6.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-glennmartin2-il-500000-n5.txt Download as CSV file: xf-glennmartin2-il-500000-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 = 0.500 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-12.500 -0.1524 0.10987 0.10750 -0.0722 0.9690 0.0098
-12.000 -0.5111 0.03197 0.02868 -0.1236 0.9355 0.0111
-11.750 -0.5075 0.02653 0.02282 -0.1243 0.9276 0.0112
-11.500 -0.4873 0.02411 0.02007 -0.1251 0.9230 0.0116
-11.250 -0.4640 0.02224 0.01799 -0.1257 0.9189 0.0120
-11.000 -0.4463 0.02111 0.01672 -0.1245 0.9118 0.0125
-10.750 -0.4187 0.02003 0.01547 -0.1251 0.9058 0.0130
-10.500 -0.3973 0.01913 0.01441 -0.1243 0.8975 0.0135
-10.250 -0.3721 0.01827 0.01337 -0.1241 0.8901 0.0141
-10.000 -0.3512 0.01755 0.01247 -0.1229 0.8833 0.0148
-9.750 -0.3282 0.01687 0.01166 -0.1220 0.8751 0.0155
-9.500 -0.3050 0.01641 0.01113 -0.1211 0.8675 0.0163
-9.250 -0.2807 0.01602 0.01065 -0.1204 0.8595 0.0174
-9.000 -0.2580 0.01558 0.01007 -0.1192 0.8511 0.0184
-8.750 -0.2347 0.01511 0.00946 -0.1183 0.8425 0.0192
-8.500 -0.2124 0.01474 0.00904 -0.1171 0.8339 0.0202
-8.250 -0.1879 0.01445 0.00865 -0.1162 0.8246 0.0213
-8.000 -0.1654 0.01414 0.00823 -0.1150 0.8129 0.0224
-7.750 -0.1420 0.01390 0.00785 -0.1139 0.8000 0.0236
-7.500 -0.1205 0.01353 0.00737 -0.1124 0.7840 0.0247
-7.250 -0.0990 0.01333 0.00705 -0.1109 0.7626 0.0260
-7.000 -0.0785 0.01315 0.00672 -0.1092 0.7353 0.0271
-6.750 -0.0598 0.01304 0.00641 -0.1071 0.7042 0.0283
-6.500 -0.0413 0.01297 0.00614 -0.1049 0.6781 0.0294
-6.250 -0.0224 0.01281 0.00581 -0.1028 0.6586 0.0303
-6.000 -0.0023 0.01259 0.00549 -0.1011 0.6453 0.0318
-5.750 0.0194 0.01245 0.00526 -0.0997 0.6349 0.0332
-5.500 0.0418 0.01231 0.00504 -0.0984 0.6255 0.0346
-5.250 0.0642 0.01219 0.00482 -0.0971 0.6161 0.0360
-5.000 0.0864 0.01208 0.00460 -0.0958 0.6065 0.0370
-4.750 0.1089 0.01186 0.00433 -0.0945 0.5977 0.0387
-4.500 0.1311 0.01174 0.00416 -0.0932 0.5889 0.0406
-4.250 0.1541 0.01161 0.00398 -0.0920 0.5786 0.0427
-4.000 0.1763 0.01152 0.00382 -0.0907 0.5675 0.0446
-3.750 0.1978 0.01142 0.00367 -0.0892 0.5530 0.0475
-3.500 0.2178 0.01138 0.00356 -0.0875 0.5298 0.0514
-3.250 0.2326 0.01149 0.00348 -0.0846 0.4839 0.0556
-3.000 0.2435 0.01176 0.00351 -0.0811 0.4317 0.0606
-2.750 0.2612 0.01192 0.00353 -0.0789 0.4074 0.0655
-2.500 0.2803 0.01198 0.00350 -0.0771 0.3927 0.0696
-2.250 0.2995 0.01202 0.00348 -0.0752 0.3818 0.0738
-2.000 0.3195 0.01206 0.00346 -0.0735 0.3725 0.0776
-1.750 0.3394 0.01212 0.00343 -0.0718 0.3651 0.0800
-1.500 0.3597 0.01211 0.00339 -0.0701 0.3591 0.0833
-1.250 0.3795 0.01211 0.00336 -0.0684 0.3533 0.0877
-1.000 0.3998 0.01213 0.00335 -0.0668 0.3490 0.0917
-0.750 0.4209 0.01215 0.00335 -0.0654 0.3449 0.0959
-0.500 0.4411 0.01216 0.00335 -0.0638 0.3409 0.1030
-0.250 0.4613 0.01219 0.00337 -0.0622 0.3372 0.1103
0.000 0.4807 0.01221 0.00341 -0.0605 0.3340 0.1267
0.250 0.5002 0.01215 0.00352 -0.0589 0.3314 0.1844
0.500 0.5214 0.01220 0.00362 -0.0576 0.3290 0.2093
0.750 0.5426 0.01228 0.00372 -0.0562 0.3263 0.2258
1.000 0.5638 0.01238 0.00381 -0.0549 0.3236 0.2375
1.250 0.5845 0.01249 0.00391 -0.0536 0.3213 0.2457
1.500 0.6048 0.01263 0.00402 -0.0521 0.3185 0.2521
1.750 0.6254 0.01275 0.00413 -0.0508 0.3165 0.2593
2.000 0.6473 0.01283 0.00423 -0.0497 0.3146 0.2663
2.250 0.6687 0.01293 0.00434 -0.0485 0.3127 0.2720
2.500 0.6899 0.01303 0.00446 -0.0473 0.3110 0.2781
2.750 0.7110 0.01316 0.00458 -0.0461 0.3092 0.2853
3.000 0.7313 0.01327 0.00472 -0.0448 0.3074 0.2965
3.250 0.7516 0.01339 0.00487 -0.0435 0.3057 0.3055
3.500 0.7717 0.01352 0.00502 -0.0422 0.3042 0.3188
3.750 0.7911 0.01364 0.00520 -0.0408 0.3026 0.3427
4.000 0.7897 0.01276 0.00543 -0.0351 0.3012 0.7870
4.500 1.0598 0.01365 0.00668 -0.0835 0.2929 1.0000
4.750 1.0768 0.01383 0.00685 -0.0815 0.2912 1.0000
5.000 1.0934 0.01403 0.00704 -0.0796 0.2892 1.0000
5.250 1.1099 0.01425 0.00725 -0.0777 0.2873 1.0000
5.500 1.1260 0.01451 0.00749 -0.0758 0.2852 1.0000
5.750 1.1446 0.01468 0.00769 -0.0743 0.2836 1.0000
6.000 1.1632 0.01485 0.00790 -0.0728 0.2817 1.0000
6.250 1.1816 0.01504 0.00811 -0.0714 0.2789 1.0000
6.500 1.1989 0.01526 0.00833 -0.0698 0.2750 1.0000
6.750 1.2148 0.01554 0.00859 -0.0680 0.2712 1.0000
7.000 1.2331 0.01575 0.00882 -0.0666 0.2662 1.0000
7.250 1.2511 0.01599 0.00908 -0.0652 0.2617 1.0000
7.500 1.2667 0.01632 0.00938 -0.0635 0.2560 1.0000
7.750 1.2847 0.01659 0.00968 -0.0622 0.2504 1.0000
8.000 1.3007 0.01694 0.01001 -0.0606 0.2427 1.0000
8.250 1.3161 0.01734 0.01039 -0.0590 0.2313 1.0000
8.500 1.3275 0.01794 0.01090 -0.0569 0.2123 1.0000
8.750 1.3280 0.01917 0.01186 -0.0533 0.1750 1.0000
9.000 1.3290 0.02046 0.01299 -0.0500 0.1501 1.0000
9.250 1.3260 0.02205 0.01439 -0.0463 0.1209 1.0000
9.500 1.3048 0.02483 0.01682 -0.0407 0.0664 1.0000
9.750 1.2881 0.02753 0.01938 -0.0361 0.0212 1.0000
10.000 1.2935 0.02885 0.02075 -0.0342 0.0160 1.0000
10.250 1.3008 0.03009 0.02205 -0.0325 0.0143 1.0000
10.500 1.3088 0.03131 0.02335 -0.0311 0.0133 1.0000
10.750 1.3165 0.03260 0.02471 -0.0298 0.0125 1.0000
11.000 1.3225 0.03409 0.02628 -0.0284 0.0118 1.0000
11.250 1.3272 0.03575 0.02802 -0.0271 0.0112 1.0000
11.500 1.3290 0.03775 0.03013 -0.0258 0.0106 1.0000
11.750 1.3330 0.03963 0.03210 -0.0248 0.0102 1.0000
12.000 1.3362 0.04167 0.03423 -0.0240 0.0099 1.0000
12.250 1.3383 0.04391 0.03656 -0.0233 0.0096 1.0000
12.500 1.3397 0.04630 0.03904 -0.0227 0.0090 1.0000
12.750 1.3380 0.04911 0.04196 -0.0222 0.0088 1.0000
13.000 1.3361 0.05200 0.04495 -0.0218 0.0084 1.0000
13.250 1.3305 0.05541 0.04846 -0.0215 0.0083 1.0000
13.500 1.3216 0.05933 0.05250 -0.0214 0.0081 1.0000
13.750 1.3139 0.06319 0.05647 -0.0215 0.0080 1.0000
14.000 1.3008 0.06793 0.06135 -0.0218 0.0078 1.0000
14.250 1.2930 0.07213 0.06568 -0.0223 0.0077 1.0000
14.500 1.2815 0.07699 0.07066 -0.0230 0.0077 1.0000
14.750 1.2697 0.08199 0.07578 -0.0239 0.0076 1.0000
15.000 1.2587 0.08694 0.08085 -0.0249 0.0075 1.0000
15.250 1.2475 0.09195 0.08597 -0.0259 0.0072 1.0000
15.500 1.2339 0.09732 0.09146 -0.0270 0.0073 1.0000
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