Re: bum steer
Posted: Mon Jul 13, 2020 10:56 am
This is a simple outer wingtip airfoil.... and I've simplified it as I couldn't face re-identing everything to look inline.
the columns are beta and the row alpha
the columns are beta and the row alpha
Code: Select all
<fcs_function name="T4T/coefficients/wing_right/_7_Cn">
<function>
<product>
<property>T4T/coefficients/airfoil_efficiency</property>
<property>T4T/damage/wing_right_7</property>
<property>T4T/aero/Cn_mach_effect</property>
<table>
<independentVar lookup="row">T4T/aero/wing_right/_7_AoA-deg</independentVar>
<independentVar lookup="column">T4T/aero/wing_right/_7_beta-deg</independentVar>
<tableData>
-32 -16 -8 -4 -2 -1 0 1 2 4 8 16 32
-90 -1.280 -1.280 -1.280 -1.280 -1.280 -1.280 -1.280 -1.280 -1.280 -1.280 1.280 -1.280 -1.280
-32 -0.278 -0.326 -0.350 -0.362 -0.368 -0.371 -0.374 -0.368 -0.362 -0.352 -0.328 -0.282 -0.190
-16 -0.379 -0.434 -0.462 -0.476 -0.483 -0.486 -0.490 -0.482 -0.475 -0.461 -0.431 -0.373 -0.257
-8 -0.070 -0.069 -0.069 -0.069 -0.069 -0.069 -0.069 -0.069 -0.069 -0.069 -0.069 -0.070 -0.071
0 0.540 0.542 0.543 0.544 0.544 0.544 0.544 0.544 0.543 0.542 0.540 0.537 0.529
8 1.394 1.395 1.396 1.396 1.396 1.397 1.39 1.391 1.396 1.395 1.393 1.389 1.381
16 1.419 1.527 1.581 1.608 1.622 1.628 1.635 1.613 1.594 1.553 1.472 1.308 0.981
32 0.476 0.592 0.650 0.679 0.693 0.700 0.708 0.695 0.683 0.657 0.607 0.507 0.306
90 1.280 1.280 1.280 1.280 1.280 1.280 1.280 1.280 1.280 1.280 1.280 1.280 1.280
</tableData>
</table>
</product>
</function>
</fcs_function>