Transient - GasTurb

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This is an example for the transient operation of a single spool turbojet. First the engine is decelerated, then there is a stabilization period followed by an acceleration.

The first picture gives an overview with the power lever angle = f(time) as input. The second picture shows the compresoor operating line; it looks like expected. Did you know how the transient operating line looks in the turbine map ?

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