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=== Starter speed === | |||
There is a somewhat complex relationship among the power coefficient, the maxrpm, and idlerpm. Both maxrpm and idlerpm are set in the engine xml file. | |||
The power of the starter motor is proportional to maxrpm. The minimum RPM needed to start the engine is 80% of the idlerpm. The greater the power coefficient (for J near 0), the more power the propeller will require to spin when starting the engine with the aircraft at rest. | |||
If your propeller will not spin fast enough to start, you can try some combination of: | |||
* Increase maxrpm (increases the power of the starter motor) | |||
* Decrease idlerpm (decreases the minimum RPM needed to start the engine) | |||
* Decrease the power coefficient in the C_POWER table, for values of J close to (or equal to) 0. This will reduce the amount of power it takes for the propeller to spin at a given RPM where J is close to 0 (which is the typical situation when starting the engine and the aircraft is at a dead stop). | |||
You can open the property tree and watch the value of J (/fdm/jsbsim/propulsion/engines/advance-ratio) to get an idea of which values you need to change in the C_POWER table. | |||
=== Notes === | === Notes === |
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