Marsden (marsden-il)
Marsden - Marsden airfoil
| Details | Dat file | Parser | |
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(marsden-il) Marsden Marsden airfoil Max thickness 27.9% at 31.6% chord. Max camber 7.7% at 37.6% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Selig format |
Marsden 1.00000 0.00000 .99901 .00262 .99606 .00626 .99114 .01056 .98429 .01524 .97553 .02053 .96489 .02626 .95241 .03240 .93815 .03892 .92216 .04579 .90451 .05299 .88526 .06051 .86448 .06833 .84227 .07646 .81871 .08488 .79389 .09359 .76791 .10259 .74088 .11186 .71289 .12139 .68406 .13119 .65451 .14124 .62434 .15152 .59369 .16202 .56267 .17271 .53140 .18354 .50000 .19447 .46860 .20538 .43733 .21603 .40631 .22583 .37565 .23224 .34549 .23476 .31594 .23466 .28711 .23203 .25912 .22740 .23209 .22110 .20611 .21336 .18129 .20435 .15773 .19425 .13552 .18319 .11474 .17131 .09549 .15877 .07784 .14569 .06185 .13222 .04759 .11851 .03511 .10471 .02447 .09098 .01571 .07745 .00886 .06441 .00394 .05181 .00099 .03930 0.00000 .02924 .00099 .01540 .00394 .00084 .00886 -.01272 .01571 -.02280 .02447 -.02967 .03511 -.03389 .04759 -.03701 .06185 -.03958 .07784 -.04184 .09549 -.04372 .11474 -.04519 .13552 -.04628 .15773 -.04701 .18129 -.04736 .20611 -.04734 .23209 -.04696 .25912 -.04628 .28711 -.04531 .31594 -.04409 .34549 -.04264 .37565 -.04095 .40631 -.03897 .43733 -.03662 .46860 -.03381 .50000 -.03043 .53140 -.02640 .56267 -.02167 .59369 -.01625 .62434 -.01022 .65451 -.00384 .68406 .00257 .71289 .00864 .74088 .01408 .76791 .01870 .79389 .02240 .81871 .02516 .84227 .02699 .86448 .02793 .88526 .02801 .90451 .02729 .92216 .02588 .93815 .02388 .95241 .02133 .96489 .01832 .97553 .01499 .98429 .01153 .99114 .00815 .99606 .00485 .99901 .00219 1.00000 0.00000 |
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Polars for Marsden (marsden-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| marsden-il | 50,000 | 9 | 3 at α=14.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| marsden-il | 50,000 | 5 | 3.5 at α=13.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| marsden-il | 100,000 | 9 | 3 at α=12.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| marsden-il | 100,000 | 5 | 4.7 at α=-10° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| marsden-il | 200,000 | 9 | 5.1 at α=-8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| marsden-il | 200,000 | 5 | 17 at α=-2.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| marsden-il | 500,000 | 9 | 28.7 at α=0° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| marsden-il | 500,000 | 5 | 59.1 at α=2° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| marsden-il | 1,000,000 | 9 | 70.2 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| marsden-il | 1,000,000 | 5 | 98 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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