Aircraft engines. Lecture notes (first preliminary edition). Chapter 3. Theoretical dependencies for an ideal gas

Please use this identifier to cite or link to this item: https://er.nau.edu.ua/handle/NAU/37940

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DC Field	Value	Language
dc.contributor.author	Goncharenko, Andriy Viktorovich	en
dc.date.accessioned	2019-03-01T16:30:48Z	-
dc.date.available	2019-03-01T16:30:48Z	-
dc.date.issued	2019-03-01	-
dc.identifier.uri	http://er.nau.edu.ua/handle/NAU/37940	-
dc.description	The equation of (2.6) in space depicts (portrays, shows, represents, describes, illustrates, gives a picture of) a surface, which characterises all possible equilibrium states of a regular (uniform) thermodynamic system. This surface is called the thermodynamic surface or the surface of state. At the thermodynamic surface a certain point corresponds to each state of the system.	en
dc.description.abstract	An equation that establishes (sets up) the connection between pressure, temperature, and specific volume of a medium of a constant content (composition, compound) is called the thermodynamic equation of state	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 3. Theoretical dependencies for an ideal gas	en
dc.type	Preprint	en
Appears in Collections:	Aircraft engines

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A_I_3.pdf	Chapter 3. Theoretical dependencies for an ideal gas	132.83 kB	Adobe PDF	View/Open
References.pdf	References	255.57 kB	Adobe PDF	View/Open