### PropulsionSystem

Library for modeling of aircraft propulsion and power systems. Main contents are elements composing gas turbine, ex. compressor, turbine, combustors.

Interfaces and Media in components in this library are compatible with those of　Modlica Standard Library. If not, interfaces are provided with real in/out connectors or expandable connector. Please do not hesitate to build system model combining components in this library and those of Modelca Standard Library.

Please refer to "Examples" package first so as to learn how to use this library. There are lots of demo and test models.

#### Contents

#### |__ EngineSimEnvironments

components which stores system-wide global parameters, ex, p of Earth's standard atmohere at sea level. All components call this as "outer", so it must be instantiated in any model.

#### |__ Elements

contains elementary components of propulsion/power system, ex, compressors, turbines, and so on. Modelers mainly use contents here. It is divided into sub packages based on level of detail.

#### |__ Subelements

contains "sub" or internal parts of elements. For example, the compontent which calculates pressure ratio and adiabatic efficiency of compressor based on table data. The system modelers may NOT use components in this package unless developing new component having new calculation method.

#### |__ Sources

Do NOT use them. Components here are created and used in early development of this library.

#### |__ Interfaces

interface objects and frames, sets of interfaces for base of elements. The system modelers may NOT user components in this package unless developing new component.