functionpartial_dp_tau
Compute dp and tau_st of a TurboComponent from the current state
Extends from Modelica.Icons.Function.
Information
This function computes the pressure differential and the moment needed for static operation of a partialTurboComponent in its current state.
By changing this function the partialTurboComponent implements different kinds of turbo components like fans, pumps, compressors, turbines, etc.
Inputs
| Type | Name | Default | Description |
|---|---|---|---|
| Medium.MassFlowRate | m_flow | Mass flow rate | |
| SI.AngularVelocity | omega | Angular velocity | |
| Medium.ThermodynamicState | state_in | Inlet state | |
| Medium.MassFlowRate | m_flow_norm | Normalization mass flow rate | |
| SI.AngularVelocity | omega_norm | Normalization angular velocity | |
| SI.Density | rho_min | Minimum density (relevant at p=0) |
Outputs
| Type | Name | Default | Description |
|---|---|---|---|
| SI.Pressure | dp | Pressure difference | |
| SI.Torque | tau_st | Steady state torque |
Contents
| Name | Description |
|---|---|
| Medium | Medium model |