modelTestTurboJetInertia
Extends from Modelica.Icons.Example (Icon for runnable examples).
Information
This is the full model of a turbojet-type engine at 11.000m [1].Simulate the model for 20s. At time t = 1 the fuel flow rate is reduced by 10%; the engine slows down accordingly.
References:
- P. P. Walsh, P. Fletcher: Gas Turbine Performance, 2nd ed., Oxford, Blackwell, 2004, pp. 646.
Parameters
| Type | Name | Default | Description |
|---|---|---|---|
| SI.SpecificEnthalpy | HH | Fuel lower heat value |
Components
| Type | Name | Default | Description |
|---|---|---|---|
| ThermoPower.Gas.Compressor | Compressor1 | ||
| ThermoPower.Gas.TurbineStodola | Turbine1 | ||
| ThermoPower.Gas.CombustionChamber | CombustionChamber1 | ||
| ThermoPower.Gas.SourcePressure | SourceP1 | ||
| ThermoPower.Gas.SinkPressure | SinkP1 | ||
| ThermoPower.Gas.SourceMassFlow | SourceW1 | ||
| Modelica.Mechanics.Rotational.Components.Inertia | Inertia1 | ||
| Gas.PressDrop | PressDrop1 | ||
| Gas.PressDrop | PressDrop2 | ||
| Gas.PressDrop | PressDrop3 | ||
| Modelica.Blocks.Sources.Step | Step1 | ||
| System | system |