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(Created page with "== FGDirect == == FGNozzle == == FGPropeller == FGPropeller models a propeller given the tabular data for Ct and Cp, indexed by the advance ratio "J". === Configuration File For...") |
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== FGDirect == | == FGDirect == | ||
Thrust is computed directly by the engine, the direct thruster file is a stub. | |||
=== Configuration File Format === | |||
<syntaxhighlight lang="xml"> | |||
<?xml version="1.0"?> | |||
<direct name="Direct"> | |||
</direct> | |||
</syntaxhighlight> | |||
=== Notes === | |||
* The direct thruster creates a property called propulsion/engine[#]/reverser-angle-rad | |||
* "Reverser angle" as used here is a way to manipulate the thrust vector, along the thrust axis ONLY, during run time. This should not be confused with a thrust vectoring nozzle. The angle is defined in radians, and is used thus: Final_thrust = cosine( reverser_angle ) * unmodified_thrust. Therefore a reverser angle of 0 results in no change, and a reverser angle of 3.14 (pi) results in a completely reversed thrust vector. An angle of 1.57 (pi/2) results in no thrust at all | |||
== FGNozzle == | == FGNozzle == | ||
== FGPropeller == | == FGPropeller == | ||
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