Please use this identifier to cite or link to this item: https://er.nau.edu.ua/handle/NAU/37944
Title: Aircraft engines. Lecture notes (first preliminary edition). Chapter 7. Heat and work consideration
Authors: Goncharenko, Andriy Viktorovich
Keywords: aircraft
engine
piston type engine
gas turbine engine
thermodynamic cycle
thermodynamic process
Issue Date: 1-Mar-2019
Publisher: National Aviation University
Abstract: Bodies in the thermodynamic process exchange energy between themselves. The energy of some bodies increases, the others, on the contrary, decreases instead. The transfer (transition, transmission) of the energy can be realised by two ways [113, pp. 23-24].
Description: The fist way of the energy transfer (transition, transmission) represents by itself the transition of the energy in the form of heat. The amount (quantity) of the energy transmitted in this way is called the amount (quantity) of heat. The second way of the energy transfer (transition, transmission) is called the transition of the energy in the form of work, and the amount (quantity) of the energy transmitted in this way is called the work. The energy transfer (transition, transmission) in this case realises by the displacement of either the entire (whole) body or its parts in space.
URI: http://er.nau.edu.ua/handle/NAU/37944
Appears in Collections:Aircraft engines

Files in This Item:
File Description SizeFormat 
A_II_7.pdfChapter 7. Heat and work consideration44.22 kBAdobe PDFView/Open
References.pdfReferences255.57 kBAdobe PDFView/Open


Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.