Aircraft engines. Lecture notes (first preliminary edition). Chapter 2. Basic considerations of thermodynamic processes

Please use this identifier to cite or link to this item: https://er.nau.edu.ua/handle/NAU/37939

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DC Field	Value	Language
dc.contributor.author	Goncharenko, Andriy Viktorovich	en
dc.date.accessioned	2019-03-01T16:15:15Z	-
dc.date.available	2019-03-01T16:15:15Z	-
dc.date.issued	2019-03-01	-
dc.identifier.uri	http://er.nau.edu.ua/handle/NAU/37939	-
dc.description	It is postulated in the thermodynamics, that an isolated system in the course of time always comes to the state of thermodynamic equilibrium and never can go out of it by itself (on its own).	en
dc.description.abstract	Under thermodynamic process it is understood a sequence of states (series, complex (the whole collection) of sequential states), through which a thermodynamic system undergoes at its interaction with the surrounding medium	en
dc.language.iso	en	en
dc.publisher	National Aviation University	en
dc.subject	aircraft	en
dc.subject	engine	en
dc.subject	piston type engine	en
dc.subject	gas turbine engine	en
dc.subject	thermodynamic cycle	en
dc.subject	thermodynamic process	en
dc.title	Aircraft engines. Lecture notes (first preliminary edition). Chapter 2. Basic considerations of thermodynamic processes	en
dc.type	Preprint	en
Appears in Collections:	Aircraft engines

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A_I_2.pdf	Chapter 2. Basic considerations of thermodynamic processes	97.01 kB	Adobe PDF	View/Open
References.pdf	References	255.57 kB	Adobe PDF	View/Open