Glenn Martin 3 (glennmartin3-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: Glenn Martin 3 (glennmartin3-il) Reynolds number: 1,000,000 Max Cl/Cd: 78.23 at α=7° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-glennmartin3-il-1000000-n5.txt Download as CSV file: xf-glennmartin3-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: Glenn Martin 3
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
------ -------- --------- --------- -------- -------- --------
-16.250 -0.9380 0.03800 0.03490 -0.1360 0.9735 0.0096
-16.000 -0.9515 0.03504 0.03177 -0.1345 0.9717 0.0099
-15.750 -0.9515 0.03311 0.02970 -0.1329 0.9706 0.0098
-15.500 -0.9470 0.03144 0.02789 -0.1313 0.9697 0.0101
-15.250 -0.9391 0.02994 0.02625 -0.1298 0.9691 0.0102
-15.000 -0.9514 0.02892 0.02514 -0.1232 0.9645 0.0103
-14.750 -0.9485 0.02777 0.02387 -0.1197 0.9625 0.0104
-14.500 -0.9394 0.02674 0.02272 -0.1171 0.9612 0.0105
-14.250 -0.9259 0.02588 0.02175 -0.1151 0.9602 0.0106
-14.000 -0.9123 0.02492 0.02070 -0.1130 0.9594 0.0109
-13.750 -0.9198 0.02425 0.01996 -0.1063 0.9545 0.0112
-13.500 -0.9100 0.02354 0.01917 -0.1031 0.9519 0.0112
-13.250 -0.8949 0.02282 0.01837 -0.1008 0.9504 0.0114
-13.000 -0.8775 0.02211 0.01758 -0.0989 0.9493 0.0115
-12.750 -0.8563 0.02156 0.01699 -0.0977 0.9486 0.0122
-12.500 -0.8641 0.02110 0.01645 -0.0903 0.9416 0.0121
-12.250 -0.8453 0.02050 0.01577 -0.0885 0.9398 0.0125
-12.000 -0.8246 0.01986 0.01505 -0.0870 0.9385 0.0126
-11.750 -0.8012 0.01933 0.01445 -0.0861 0.9375 0.0132
-11.500 -0.7956 0.01886 0.01390 -0.0813 0.9322 0.0132
-11.250 -0.7786 0.01837 0.01335 -0.0790 0.9289 0.0135
-11.000 -0.7565 0.01784 0.01277 -0.0776 0.9270 0.0138
-10.750 -0.7320 0.01740 0.01231 -0.0767 0.9257 0.0143
-10.500 -0.7065 0.01703 0.01192 -0.0761 0.9247 0.0149
-10.250 -0.6961 0.01682 0.01167 -0.0721 0.9186 0.0154
-10.000 -0.6763 0.01643 0.01122 -0.0701 0.9154 0.0157
-9.750 -0.6533 0.01603 0.01075 -0.0688 0.9133 0.0162
-9.500 -0.6292 0.01552 0.01020 -0.0678 0.9118 0.0165
-9.000 -0.5864 0.01495 0.00959 -0.0645 0.9039 0.0174
-8.750 -0.5601 0.01471 0.00933 -0.0639 0.9007 0.0179
-8.500 -0.5301 0.01427 0.00883 -0.0641 0.8979 0.0184
-8.250 -0.4957 0.01389 0.00841 -0.0652 0.8958 0.0190
-8.000 -0.4727 0.01351 0.00796 -0.0639 0.8895 0.0193
-7.750 -0.4433 0.01326 0.00768 -0.0639 0.8861 0.0199
-7.500 -0.4101 0.01281 0.00719 -0.0649 0.8825 0.0202
-7.250 -0.3717 0.01259 0.00697 -0.0669 0.8788 0.0210
-7.000 -0.3449 0.01234 0.00668 -0.0665 0.8724 0.0215
-6.750 -0.3116 0.01208 0.00638 -0.0674 0.8677 0.0220
-6.250 -0.2449 0.01148 0.00567 -0.0694 0.8560 0.0230
-6.000 -0.2132 0.01130 0.00543 -0.0700 0.8494 0.0234
-5.750 -0.1817 0.01100 0.00511 -0.0707 0.8428 0.0245
-5.500 -0.1559 0.01080 0.00487 -0.0701 0.8355 0.0248
-5.250 -0.1265 0.01062 0.00466 -0.0702 0.8300 0.0253
-5.000 -0.1006 0.01049 0.00449 -0.0696 0.8230 0.0259
-4.750 -0.0751 0.01038 0.00433 -0.0689 0.8132 0.0267
-4.500 -0.0519 0.01024 0.00412 -0.0676 0.8023 0.0270
-4.250 -0.0274 0.01012 0.00394 -0.0667 0.7925 0.0275
-4.000 -0.0074 0.01004 0.00381 -0.0647 0.7805 0.0276
-3.750 0.0134 0.00991 0.00361 -0.0630 0.7642 0.0285
-3.500 0.0293 0.00987 0.00349 -0.0601 0.7408 0.0292
-3.250 0.0341 0.01000 0.00342 -0.0548 0.6925 0.0294
-3.000 0.0371 0.01022 0.00342 -0.0492 0.6418 0.0297
-2.750 0.0520 0.01033 0.00339 -0.0462 0.6101 0.0301
-2.500 0.0631 0.01056 0.00339 -0.0425 0.5578 0.0307
-2.250 0.0774 0.01077 0.00340 -0.0395 0.5050 0.0316
-2.000 0.0927 0.01101 0.00342 -0.0369 0.4548 0.0322
-1.500 0.1375 0.01114 0.00336 -0.0345 0.4148 0.0337
-1.250 0.1625 0.01112 0.00332 -0.0338 0.4040 0.0355
-1.000 0.1858 0.01117 0.00331 -0.0328 0.3925 0.0357
-0.750 0.2105 0.01117 0.00328 -0.0322 0.3832 0.0386
-0.500 0.2345 0.01119 0.00328 -0.0313 0.3749 0.0407
-0.250 0.2583 0.01121 0.00329 -0.0305 0.3614 0.0484
0.000 0.2824 0.01123 0.00330 -0.0297 0.3517 0.0593
0.250 0.3065 0.01124 0.00332 -0.0290 0.3424 0.0757
0.500 0.3329 0.01117 0.00337 -0.0289 0.3281 0.1322
0.750 0.3560 0.01124 0.00342 -0.0280 0.3177 0.1450
1.000 0.3785 0.01133 0.00348 -0.0270 0.3041 0.1583
1.250 0.4004 0.01146 0.00355 -0.0259 0.2897 0.1664
1.500 0.4227 0.01157 0.00364 -0.0248 0.2738 0.1829
1.750 0.4457 0.01167 0.00373 -0.0240 0.2631 0.1961
2.000 0.4857 0.01121 0.00393 -0.0275 0.2487 0.4595
2.500 0.6855 0.01223 0.00617 -0.0613 0.2187 0.9762
2.750 0.7534 0.01278 0.00660 -0.0706 0.2086 0.9838
3.000 0.7725 0.01298 0.00678 -0.0689 0.2058 0.9847
3.250 0.8280 0.01307 0.00682 -0.0755 0.2008 0.9880
3.500 0.8553 0.01321 0.00692 -0.0758 0.1976 0.9889
3.750 0.8898 0.01339 0.00704 -0.0777 0.1934 0.9914
4.250 0.9718 0.01348 0.00709 -0.0844 0.1877 0.9975
4.500 1.0126 0.01344 0.00703 -0.0878 0.1852 0.9999
4.750 1.0335 0.01360 0.00717 -0.0867 0.1834 1.0000
5.000 1.0530 0.01379 0.00734 -0.0853 0.1808 1.0000
5.250 1.0721 0.01399 0.00753 -0.0838 0.1783 1.0000
5.500 1.0906 0.01422 0.00775 -0.0822 0.1754 1.0000
5.750 1.1103 0.01439 0.00793 -0.0809 0.1742 1.0000
6.000 1.1299 0.01458 0.00813 -0.0795 0.1736 1.0000
6.250 1.1495 0.01477 0.00833 -0.0782 0.1719 1.0000
6.500 1.1690 0.01498 0.00855 -0.0769 0.1712 1.0000
6.750 1.1883 0.01520 0.00877 -0.0756 0.1691 1.0000
7.000 1.2071 0.01543 0.00901 -0.0742 0.1680 1.0000
7.250 1.2254 0.01569 0.00927 -0.0728 0.1663 1.0000
7.500 1.2440 0.01595 0.00954 -0.0714 0.1651 1.0000
7.750 1.2623 0.01622 0.00983 -0.0700 0.1636 1.0000
8.000 1.2805 0.01651 0.01013 -0.0686 0.1622 1.0000
8.250 1.2981 0.01682 0.01046 -0.0671 0.1606 1.0000
8.500 1.3165 0.01709 0.01076 -0.0658 0.1600 1.0000
8.750 1.3347 0.01737 0.01108 -0.0645 0.1594 1.0000
9.000 1.3531 0.01765 0.01140 -0.0632 0.1590 1.0000
9.250 1.3714 0.01794 0.01172 -0.0620 0.1579 1.0000
9.500 1.3890 0.01826 0.01207 -0.0607 0.1566 1.0000
9.750 1.4065 0.01859 0.01240 -0.0594 0.1530 1.0000
10.000 1.4236 0.01895 0.01277 -0.0581 0.1511 1.0000
10.250 1.4393 0.01940 0.01321 -0.0565 0.1479 1.0000
10.500 1.4550 0.01982 0.01367 -0.0550 0.1464 1.0000
10.750 1.4732 0.02013 0.01401 -0.0540 0.1441 1.0000
11.000 1.4901 0.02051 0.01442 -0.0527 0.1409 1.0000
11.250 1.5065 0.02092 0.01489 -0.0514 0.1411 1.0000
11.500 1.5205 0.02146 0.01541 -0.0499 0.1359 1.0000
11.750 1.5361 0.02193 0.01592 -0.0485 0.1347 1.0000
12.000 1.5510 0.02245 0.01647 -0.0471 0.1330 1.0000
12.250 1.5662 0.02294 0.01699 -0.0458 0.1286 1.0000
12.500 1.5803 0.02351 0.01758 -0.0444 0.1257 1.0000
12.750 1.5933 0.02416 0.01824 -0.0429 0.1222 1.0000
13.000 1.6059 0.02483 0.01893 -0.0414 0.1169 1.0000
13.250 1.6150 0.02573 0.01979 -0.0395 0.1081 1.0000
13.500 1.6103 0.02754 0.02143 -0.0359 0.0860 1.0000
13.750 1.6206 0.02841 0.02235 -0.0343 0.0833 1.0000
14.000 1.6207 0.03000 0.02390 -0.0316 0.0726 1.0000
14.250 1.5785 0.03473 0.02836 -0.0246 0.0329 1.0000
14.500 1.5637 0.03772 0.03134 -0.0212 0.0197 1.0000
14.750 1.5655 0.03949 0.03316 -0.0195 0.0177 1.0000
15.000 1.5653 0.04150 0.03523 -0.0178 0.0158 1.0000
15.250 1.5601 0.04405 0.03783 -0.0160 0.0130 1.0000
15.500 1.5624 0.04599 0.03986 -0.0150 0.0127 1.0000
15.750 1.5618 0.04828 0.04223 -0.0138 0.0120 1.0000
16.000 1.5558 0.05124 0.04526 -0.0127 0.0109 1.0000
16.250 1.5547 0.05374 0.04785 -0.0121 0.0108 1.0000
16.500 1.5500 0.05679 0.05099 -0.0115 0.0103 0.9999
16.750 1.5446 0.06002 0.05432 -0.0112 0.0101 0.9999
17.000 1.5370 0.06367 0.05808 -0.0111 0.0098 0.9999
17.250 1.5264 0.06782 0.06233 -0.0113 0.0092 0.9999
17.500 1.5146 0.07225 0.06688 -0.0118 0.0091 0.9999
17.750 1.4945 0.07804 0.07279 -0.0128 0.0083 0.9998
18.000 1.4776 0.08361 0.07850 -0.0140 0.0084 0.9998
18.250 1.4602 0.08934 0.08438 -0.0154 0.0087 0.9998
18.500 1.4377 0.09584 0.09102 -0.0171 0.0088 0.9998
18.750 1.4090 0.10341 0.09874 -0.0192 0.0085 0.9998
19.000 1.3823 0.11077 0.10624 -0.0213 0.0085 0.9998
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