Gas Turbine
This model extends the Turbine_Base model with the calculation of
the performance parameters, mass flowrate, pressure ratio and
efficiency.
This method is based on the Stodola's law, which calculates
PR as function of the inlet conditions, i.e. mass
flowrate, inlet temperature and pressure.
Modelling options
The following options are available to define Stodola's constant
K:
- NominalCondition = true: Stodola's constant K is
specified by the nominal operating point
(wnom,Tstart_in,pstart_in,pstart_out)
- NominalCondition = false: Stodola's constant K is used
directly.
The following options are available to define the efficiency
eta:
- fixedEta = true: the efficiency is explicitly supplied
as a parameter.
- fixedEta = false: the efficiency is a function of the
pressure ratio PR and of the referred speed N_T.
The function is defined by interpolation of the table
tableEta, where N_T represents the first row and
PR the first column of the table. The interpolation is
performed by a Modelica.Blocks.Tables.CombiTable2D
model.
The following options are available to select the way of
definition of the table:
- Table = 0: the table is explicitly supplied as a
matrix parameter.
- Table = 1: the table is read from a file; the string
fileName contains the path to the files where the table is
stored, either in ASCII or Matlab binary format.
- 13 Apr 2005 by Francesco Casella:
Turbine model restructured using inheritance.
First release.
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