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JSBSim Thrusters: Difference between revisions
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JSBSim uses thruster models to convert engine power into aerodynamic forces. The following table shows which engine-thruster combinations work. | '''[[JSBSim]]''' uses '''thruster''' models to convert engine power into aerodynamic forces. The following table shows which engine-thruster combinations work. | ||
{| class="wikitable" style="text-align:center;" | {| class="wikitable" style="text-align:center;" | ||
| | | | ||
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</tableData> | </tableData> | ||
</table> | </table> | ||
</propeller> | </propeller> | ||
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Or in metric units, kg * meters^2: | Or in metric units, kg * meters^2: | ||
<ixx unit="KG*M2"> | <ixx unit="KG*M2"> 12.14 </ixx> | ||
For a thin rod of mass m (kg) and diameter D (meters) spinning about its center, the formula is m*D^2/12. See the [http://en.wikipedia.org/wiki/List_of_moments_of_inertia Moments of inertia reference page] and [http://www.engineeringtoolbox.com/moment-inertia-torque-d_913.html list of conversion factors for different units for moment of inertia].) | For a thin rod of mass m (kg) and diameter D (meters) spinning about its center, the formula is m*D^2/12. See the [http://en.wikipedia.org/wiki/List_of_moments_of_inertia Moments of inertia reference page] and [http://www.engineeringtoolbox.com/moment-inertia-torque-d_913.html list of conversion factors for different units for moment of inertia].) | ||
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<table name="C_THRUST" type="internal"> | <table name="C_THRUST" type="internal"> | ||
<tableData> | <tableData> | ||
0.0 0.068 | |||
0.1 0.068 | |||
0.2 0.067 | |||
0.3 0.066 | |||
0.4 0.064 | |||
0.5 0.062 | |||
0.6 0.059 | |||
0.7 0.054 | |||
0.8 0.043 | |||
0.9 0.031 | |||
1.0 0.019 | |||
1.1 0.008 | |||
1.2 -0.001 | |||
1.3 -0.008 | |||
1.4 -0.019 | 1.4 -0.019 | ||
1.5 -0.029 | 1.5 -0.029 | ||