AG27 Bubble Dancer DLG by Mark Drela (ag27-il) Xfoil prediction polar at RE=100,000 Ncrit=5
| Details | Polar file |
|---|---|
|
Airfoil: AG27 Bubble Dancer DLG by Mark Drela (ag27-il) Reynolds number: 100,000 Max Cl/Cd: 53 at α=4° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-ag27-il-100000-n5.txt Download as CSV file: xf-ag27-il-100000-n5.csv |
XFOIL Version 6.96
Calculated polar for: AG27 Bubble Dancer DLG by Mark Drela
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.100 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-8.000 -0.4813 0.09999 0.09518 0.0023 1.0000 0.0412
-7.750 -0.4759 0.09654 0.09176 0.0005 1.0000 0.0417
-7.250 -0.4653 0.08952 0.08480 -0.0039 1.0000 0.0425
-6.750 -0.3809 0.06420 0.05984 -0.0203 1.0000 0.0266
-6.500 -0.4259 0.07256 0.06785 -0.0235 1.0000 0.0249
-6.250 -0.4134 0.06838 0.06367 -0.0261 1.0000 0.0239
-6.000 -0.3963 0.06350 0.05877 -0.0308 1.0000 0.0230
-5.750 -0.3756 0.05804 0.05324 -0.0364 1.0000 0.0222
-5.500 -0.3519 0.05206 0.04712 -0.0423 1.0000 0.0214
-5.250 -0.3256 0.04582 0.04065 -0.0478 1.0000 0.0211
-5.000 -0.2983 0.04009 0.03458 -0.0521 1.0000 0.0218
-4.750 -0.2702 0.03494 0.02895 -0.0552 1.0000 0.0230
-4.500 -0.2421 0.03051 0.02395 -0.0571 1.0000 0.0237
-4.250 -0.2143 0.02682 0.01965 -0.0581 1.0000 0.0238
-4.000 -0.1866 0.02388 0.01614 -0.0584 1.0000 0.0243
-3.750 -0.1594 0.02162 0.01337 -0.0582 1.0000 0.0250
-3.500 -0.1327 0.01956 0.01094 -0.0580 1.0000 0.0263
-3.250 -0.1075 0.01841 0.00971 -0.0578 1.0000 0.0307
-3.000 -0.0813 0.01725 0.00835 -0.0573 1.0000 0.0348
-2.750 -0.0550 0.01602 0.00703 -0.0570 1.0000 0.0393
-2.500 -0.0290 0.01529 0.00625 -0.0567 1.0000 0.0505
-2.250 -0.0025 0.01451 0.00550 -0.0566 1.0000 0.0687
-2.000 0.0243 0.01378 0.00491 -0.0566 1.0000 0.1100
-1.750 0.0508 0.01311 0.00460 -0.0568 1.0000 0.1981
-1.500 0.0777 0.01259 0.00449 -0.0571 0.9994 0.3197
-1.250 0.1166 0.01201 0.00438 -0.0596 0.9901 0.4783
-1.000 0.1506 0.01110 0.00423 -0.0604 0.9812 0.7108
-0.750 0.1901 0.01064 0.00396 -0.0621 0.9667 1.0000
-0.500 0.2287 0.01069 0.00380 -0.0642 0.9524 1.0000
-0.250 0.2654 0.01073 0.00366 -0.0658 0.9363 1.0000
0.000 0.3007 0.01076 0.00356 -0.0671 0.9189 1.0000
0.250 0.3348 0.01080 0.00347 -0.0680 0.9007 1.0000
0.500 0.3658 0.01085 0.00341 -0.0682 0.8798 1.0000
0.750 0.3958 0.01090 0.00336 -0.0681 0.8584 1.0000
1.000 0.4236 0.01098 0.00334 -0.0675 0.8345 1.0000
1.250 0.4507 0.01107 0.00334 -0.0668 0.8097 1.0000
1.500 0.4775 0.01118 0.00337 -0.0660 0.7835 1.0000
1.750 0.5038 0.01131 0.00340 -0.0652 0.7556 1.0000
2.000 0.5299 0.01147 0.00345 -0.0643 0.7260 1.0000
2.250 0.5557 0.01165 0.00352 -0.0634 0.6949 1.0000
2.750 0.6071 0.01211 0.00379 -0.0617 0.6284 1.0000
3.000 0.6325 0.01239 0.00393 -0.0608 0.5933 1.0000
3.250 0.6580 0.01269 0.00412 -0.0601 0.5560 1.0000
3.500 0.6833 0.01303 0.00434 -0.0594 0.5175 1.0000
3.750 0.7085 0.01341 0.00464 -0.0587 0.4778 1.0000
4.000 0.7335 0.01384 0.00493 -0.0580 0.4366 1.0000
4.250 0.7584 0.01431 0.00527 -0.0574 0.3948 1.0000
4.500 0.7831 0.01483 0.00566 -0.0568 0.3522 1.0000
4.750 0.8077 0.01540 0.00610 -0.0563 0.3116 1.0000
5.000 0.8321 0.01603 0.00664 -0.0558 0.2730 1.0000
5.250 0.8565 0.01668 0.00721 -0.0553 0.2380 1.0000
5.500 0.8807 0.01738 0.00783 -0.0549 0.2076 1.0000
5.750 0.9048 0.01810 0.00851 -0.0544 0.1819 1.0000
6.000 0.9287 0.01886 0.00930 -0.0539 0.1597 1.0000
6.250 0.9525 0.01965 0.01012 -0.0533 0.1414 1.0000
6.500 0.9757 0.02051 0.01097 -0.0528 0.1245 1.0000
6.750 0.9988 0.02142 0.01191 -0.0522 0.1103 1.0000
7.000 1.0216 0.02234 0.01291 -0.0516 0.0966 1.0000
7.250 1.0440 0.02335 0.01399 -0.0509 0.0843 1.0000
7.500 1.0661 0.02439 0.01521 -0.0502 0.0727 1.0000
7.750 1.0878 0.02550 0.01648 -0.0495 0.0619 1.0000
8.000 1.1086 0.02680 0.01795 -0.0486 0.0523 1.0000
8.250 1.1280 0.02830 0.01958 -0.0477 0.0444 1.0000
8.500 1.1464 0.02982 0.02119 -0.0468 0.0373 1.0000
8.750 1.1646 0.03168 0.02336 -0.0456 0.0318 1.0000
9.000 1.1807 0.03354 0.02536 -0.0445 0.0279 1.0000
9.250 1.1954 0.03586 0.02799 -0.0432 0.0243 1.0000
9.500 1.2089 0.03831 0.03084 -0.0418 0.0218 1.0000
9.750 1.2198 0.04090 0.03370 -0.0404 0.0202 1.0000
10.000 1.2272 0.04369 0.03671 -0.0390 0.0189 1.0000
10.250 1.2282 0.04742 0.04076 -0.0374 0.0179 1.0000
10.500 1.2277 0.05080 0.04462 -0.0358 0.0169 1.0000
10.750 1.2201 0.05435 0.04854 -0.0340 0.0163 1.0000
11.000 1.2077 0.05824 0.05275 -0.0329 0.0159 1.0000
11.250 1.1922 0.06290 0.05769 -0.0335 0.0157 1.0000
11.500 1.1745 0.06859 0.06364 -0.0359 0.0157 1.0000
11.750 1.1547 0.07560 0.07088 -0.0402 0.0159 1.0000
12.000 1.1335 0.08395 0.07942 -0.0461 0.0163 1.0000
12.250 1.1117 0.09339 0.08899 -0.0528 0.0169 1.0000
12.500 1.0907 0.10314 0.09882 -0.0591 0.0176 1.0000
12.750 1.0708 0.11289 0.10860 -0.0649 0.0181 1.0000
|
Polar data table (+)
Polar graphs
<< Back to AG27 Bubble Dancer DLG by Mark Drela (ag27-il)