.ThermoPower.Test.GasComponents.TestGasTurbine

Information

This model test the Turbine model with an inertial load. Boundary conditions and data refer to an turbojet engine at 11.000 m.

Simulate for 5 seconds.

Contents

NameDescription
 Medium
Generated at 2025-01-31T19:25:52Z by OpenModelicaOpenModelica 1.24.3 using GenerateDoc.mos