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Thermo-dynamic cycle computation of a micro turbojet engine

Authors: Ladislav Fozo; Rudolf Andoga; Radovan Kovacs;

Thermo-dynamic cycle computation of a micro turbojet engine

Abstract

Thermodynamic models are a perfect tool to describe heat engines. But such thermodynamic model must be extended to reflect reality as accurately as possible. Micro turbo compressor engines are a specific type of heat engines that are derived from normal turbo compressor engines. To compute their thermodynamic parameters we need to know their dimensions and choose many coefficients, which describe them. With this model we can get the needed state variables, which describe the engine's operational mode, load, and degradation. In order to use the thermodynamic model as a diagnostic tool it has to be transformed into some kind of mathematic tool, like Matlab/Simulink to get comparative data at real time. In this paper will be introduced the JETCAT P80 micro turbo compressor engine and application of the analytical model on it. There will be presented also applicability of that model.

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Powered by OpenAIRE graph
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selected citations
These citations are derived from selected sources.
This is an alternative to the "Influence" indicator, which also reflects the overall/total impact of an article in the research community at large, based on the underlying citation network (diachronically).
BIP!Citations provided by BIP!
popularity
This indicator reflects the "current" impact/attention (the "hype") of an article in the research community at large, based on the underlying citation network.
BIP!Popularity provided by BIP!
influence
This indicator reflects the overall/total impact of an article in the research community at large, based on the underlying citation network (diachronically).
BIP!Influence provided by BIP!
impulse
This indicator reflects the initial momentum of an article directly after its publication, based on the underlying citation network.
BIP!Impulse provided by BIP!
14
Top 10%
Top 10%
Top 10%
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