davissm (davissm-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
|---|---|
|
Airfoil: davissm (davissm-il) Reynolds number: 1,000,000 Max Cl/Cd: 154.72 at α=2.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-davissm-il-1000000.txt Download as CSV file: xf-davissm-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: davissm
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 1.000 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-9.750 -0.3273 0.11739 0.11573 -0.0321 1.0000 0.0081
-9.500 -0.3234 0.11492 0.11328 -0.0322 1.0000 0.0082
-9.250 -0.3201 0.11253 0.11091 -0.0323 0.9998 0.0085
-9.000 -0.3057 0.10890 0.10727 -0.0358 0.9987 0.0089
-8.750 -0.2907 0.10514 0.10350 -0.0394 0.9967 0.0097
-8.500 -0.2778 0.10154 0.09991 -0.0429 0.9833 0.0104
-8.250 -0.2628 0.09775 0.09612 -0.0477 0.9772 0.0105
-8.000 -0.2461 0.09389 0.09225 -0.0526 0.9735 0.0105
-7.750 -0.2253 0.08971 0.08805 -0.0586 0.9703 0.0105
-7.500 -0.1987 0.08521 0.08353 -0.0660 0.9679 0.0105
-6.500 -0.1067 0.06984 0.06803 -0.0869 0.9428 0.0116
-6.250 -0.0845 0.06666 0.06480 -0.0916 0.9350 0.0120
-6.000 -0.0614 0.06340 0.06150 -0.0963 0.9273 0.0126
-5.500 0.0074 0.05510 0.05307 -0.1125 0.9137 0.0143
-5.250 0.0410 0.05078 0.04866 -0.1192 0.9080 0.0144
-5.000 0.0724 0.04497 0.04278 -0.1266 0.9021 0.0149
-4.750 0.0983 0.04287 0.04062 -0.1291 0.8967 0.0153
-4.500 0.1287 0.04049 0.03817 -0.1328 0.8916 0.0160
-4.250 0.1643 0.03760 0.03520 -0.1375 0.8863 0.0179
-4.000 0.2124 0.03361 0.03102 -0.1442 0.8817 0.0193
-3.750 0.2543 0.02890 0.02611 -0.1496 0.8770 0.0194
-3.500 0.2951 0.02273 0.01961 -0.1558 0.8721 0.0207
-3.250 0.3237 0.02172 0.01848 -0.1569 0.8667 0.0216
-3.000 0.3549 0.02029 0.01693 -0.1581 0.8609 0.0242
-2.750 0.3799 0.00407 0.00037 -0.1535 0.8420 0.0240
-2.500 0.4287 0.01205 0.00752 -0.1624 0.8511 0.0226
-2.250 0.4582 0.01095 0.00622 -0.1628 0.8452 0.0234
-2.000 0.4869 0.01026 0.00536 -0.1630 0.8393 0.0246
-1.750 0.5154 0.00981 0.00479 -0.1631 0.8330 0.0256
-1.500 0.5435 0.00954 0.00444 -0.1631 0.8260 0.0262
-1.250 0.5718 0.00882 0.00359 -0.1632 0.8193 0.0270
-1.000 0.5999 0.00817 0.00286 -0.1633 0.8121 0.0290
-0.750 0.6279 0.00805 0.00273 -0.1634 0.8051 0.0310
-0.500 0.6558 0.00789 0.00253 -0.1634 0.7974 0.0328
-0.250 0.6837 0.00776 0.00236 -0.1634 0.7896 0.0345
0.000 0.7114 0.00768 0.00225 -0.1633 0.7812 0.0357
0.250 0.7394 0.00747 0.00199 -0.1633 0.7722 0.0390
0.500 0.7670 0.00742 0.00192 -0.1633 0.7631 0.0434
0.750 0.7945 0.00739 0.00186 -0.1632 0.7530 0.0467
1.000 0.8222 0.00735 0.00180 -0.1631 0.7426 0.0543
1.250 0.8492 0.00726 0.00180 -0.1630 0.7271 0.1132
1.500 0.8753 0.00686 0.00198 -0.1630 0.7088 0.4377
1.750 0.9012 0.00587 0.00203 -0.1628 0.6947 1.0000
2.000 0.9282 0.00600 0.00209 -0.1627 0.6786 1.0000
2.250 0.9546 0.00617 0.00216 -0.1623 0.6562 1.0000
2.500 0.9807 0.00636 0.00224 -0.1620 0.6340 1.0000
2.750 1.0070 0.00655 0.00234 -0.1617 0.6127 1.0000
3.000 1.0330 0.00677 0.00247 -0.1614 0.5902 1.0000
3.250 1.0584 0.00704 0.00261 -0.1609 0.5604 1.0000
3.500 1.0831 0.00739 0.00279 -0.1603 0.5235 1.0000
3.750 1.1064 0.00788 0.00303 -0.1595 0.4702 1.0000
4.000 1.1294 0.00842 0.00332 -0.1587 0.4154 1.0000
4.250 1.1515 0.00907 0.00366 -0.1578 0.3530 1.0000
4.500 1.1702 0.01009 0.00418 -0.1563 0.2565 1.0000
4.750 1.1809 0.01205 0.00521 -0.1535 0.0811 1.0000
5.000 1.2049 0.01246 0.00555 -0.1529 0.0657 1.0000
5.250 1.2295 0.01278 0.00586 -0.1523 0.0571 1.0000
5.500 1.2538 0.01313 0.00617 -0.1518 0.0489 1.0000
5.750 1.2783 0.01342 0.00647 -0.1513 0.0426 1.0000
6.000 1.3019 0.01382 0.00681 -0.1506 0.0341 1.0000
6.250 1.3246 0.01430 0.00723 -0.1497 0.0259 1.0000
6.500 1.3482 0.01464 0.00760 -0.1490 0.0228 1.0000
6.750 1.3690 0.01530 0.00827 -0.1477 0.0184 1.0000
7.000 1.3919 0.01567 0.00868 -0.1469 0.0172 1.0000
7.250 1.4137 0.01613 0.00918 -0.1459 0.0158 1.0000
7.500 1.4342 0.01670 0.00977 -0.1446 0.0145 1.0000
7.750 1.4481 0.01783 0.01104 -0.1420 0.0128 1.0000
8.000 1.4690 0.01826 0.01150 -0.1408 0.0125 1.0000
8.250 1.4880 0.01881 0.01212 -0.1393 0.0119 1.0000
8.500 1.5056 0.01945 0.01282 -0.1375 0.0113 1.0000
8.750 1.5221 0.02011 0.01354 -0.1355 0.0108 1.0000
9.000 1.5384 0.02076 0.01424 -0.1336 0.0103 1.0000
9.250 1.5528 0.02149 0.01501 -0.1313 0.0098 1.0000
9.500 1.5587 0.02275 0.01636 -0.1275 0.0092 1.0000
9.750 1.5533 0.02467 0.01845 -0.1216 0.0087 1.0000
10.000 1.5663 0.02535 0.01921 -0.1192 0.0086 1.0000
10.250 1.5778 0.02620 0.02013 -0.1166 0.0084 1.0000
10.500 1.5882 0.02717 0.02119 -0.1140 0.0081 1.0000
10.750 1.5968 0.02835 0.02247 -0.1112 0.0078 1.0000
11.000 1.6056 0.02955 0.02378 -0.1086 0.0075 1.0000
11.250 1.6149 0.03072 0.02503 -0.1063 0.0072 1.0000
11.500 1.6237 0.03194 0.02632 -0.1040 0.0069 1.0000
11.750 1.6310 0.03334 0.02782 -0.1016 0.0067 1.0000
12.000 1.6374 0.03487 0.02943 -0.0992 0.0065 1.0000
12.250 1.6411 0.03669 0.03135 -0.0967 0.0063 1.0000
12.500 1.6385 0.03931 0.03413 -0.0935 0.0061 1.0000
12.750 1.6200 0.04423 0.03941 -0.0887 0.0058 1.0000
13.000 1.6272 0.04565 0.04092 -0.0872 0.0057 1.0000
13.250 1.6307 0.04763 0.04302 -0.0854 0.0056 1.0000
13.500 1.6336 0.04972 0.04525 -0.0838 0.0055 1.0000
13.750 1.6340 0.05215 0.04782 -0.0821 0.0054 1.0000
14.000 1.6317 0.05497 0.05080 -0.0805 0.0052 1.0000
14.250 1.6253 0.05843 0.05443 -0.0789 0.0051 1.0000
14.500 1.6192 0.06196 0.05812 -0.0777 0.0050 1.0000
14.750 1.6088 0.06619 0.06254 -0.0767 0.0050 1.0000
15.000 1.5988 0.07055 0.06707 -0.0762 0.0049 1.0000
15.250 1.5871 0.07539 0.07209 -0.0761 0.0048 1.0000
15.500 1.5738 0.08070 0.07757 -0.0765 0.0048 1.0000
15.750 1.5556 0.08705 0.08412 -0.0775 0.0047 1.0000
16.000 1.5392 0.09345 0.09070 -0.0791 0.0047 1.0000
16.250 1.5201 0.10071 0.09814 -0.0815 0.0047 1.0000
16.500 1.4992 0.10870 0.10632 -0.0847 0.0047 1.0000
16.750 1.4742 0.11794 0.11576 -0.0889 0.0047 1.0000
17.000 1.4462 0.12856 0.12658 -0.0945 0.0047 1.0000
17.250 1.4173 0.14025 0.13846 -0.1013 0.0048 1.0000
17.500 1.3812 0.15511 0.15354 -0.1107 0.0049 1.0000
|
Polar data table (+)
Polar graphs
<< Back to davissm (davissm-il)