.ThermoPower.Gas.GTunit_ISO

Information

This model adds the performance characteristics to the GTunit_base model, when only one performance curve is known at ISO conditions: 15 degC temperature and 1.013 bar pressure at the air inlet, and nominal rotational speed.

HI_ISO = f(ZLPout_ISO)
PR = g(ZLPout_ISO)
wia_ISO = h(ZLPout_ISO)

The performance maps are thus tabulated into the matrix tableData, whose columns contain:

ZLPout_ISO (zero loss power output in ISO conditions)
HI_ISO (heat input in ISO conditions)
PR (pressure ratio)
wia_ISO (inlet air flow rate in ISO conditions)

Modelling options

The following options are available to select how the table is defined:

Table = 0: the table is explicitly supplied as matrix parameter.
Table = 1: the table is read from a file; the string fileName contains the path to the files where tables are stored, either in ASCII or Matlab binary format.

Revisions

7 Jun 2005 by Francesco Casella:
Model restructured by inheritance.
19 Apr 2005 by Francesco Casella:
GT unit model restructured using inheritance.

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